US20050263359A1 - Customizable strut assemblies having variable stroke lengths and articles employing the same - Google Patents
Customizable strut assemblies having variable stroke lengths and articles employing the same Download PDFInfo
- Publication number
- US20050263359A1 US20050263359A1 US11/078,848 US7884805A US2005263359A1 US 20050263359 A1 US20050263359 A1 US 20050263359A1 US 7884805 A US7884805 A US 7884805A US 2005263359 A1 US2005263359 A1 US 2005263359A1
- Authority
- US
- United States
- Prior art keywords
- actuator
- piston
- housing
- strut assembly
- shape memory
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 230000000712 assembly Effects 0.000 title description 10
- 238000000429 assembly Methods 0.000 title description 10
- 230000008859 change Effects 0.000 claims abstract description 34
- 238000004891 communication Methods 0.000 claims abstract description 23
- 238000000034 method Methods 0.000 claims abstract description 15
- 230000003213 activating effect Effects 0.000 claims abstract description 6
- 239000000463 material Substances 0.000 claims description 35
- 229910001285 shape-memory alloy Inorganic materials 0.000 claims description 32
- 229920001971 elastomer Polymers 0.000 claims description 20
- 239000000806 elastomer Substances 0.000 claims description 20
- 229920001746 electroactive polymer Polymers 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 18
- 239000012781 shape memory material Substances 0.000 claims description 13
- 230000005291 magnetic effect Effects 0.000 claims description 11
- 241000256247 Spodoptera exigua Species 0.000 claims description 4
- 239000000126 substance Substances 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- -1 poly(aniline) Polymers 0.000 description 27
- 229920000642 polymer Polymers 0.000 description 20
- 239000011149 active material Substances 0.000 description 18
- 239000000956 alloy Substances 0.000 description 18
- 229920000431 shape-memory polymer Polymers 0.000 description 18
- 229910045601 alloy Inorganic materials 0.000 description 15
- 239000002131 composite material Substances 0.000 description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 13
- 239000002245 particle Substances 0.000 description 13
- 238000010438 heat treatment Methods 0.000 description 12
- 238000001994 activation Methods 0.000 description 10
- 230000004913 activation Effects 0.000 description 10
- 230000007246 mechanism Effects 0.000 description 10
- 238000006073 displacement reaction Methods 0.000 description 8
- 229910000734 martensite Inorganic materials 0.000 description 8
- 230000003446 memory effect Effects 0.000 description 8
- 239000012530 fluid Substances 0.000 description 7
- 230000007704 transition Effects 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 230000004044 response Effects 0.000 description 6
- 238000001816 cooling Methods 0.000 description 5
- 229920001577 copolymer Polymers 0.000 description 5
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N iron oxide Inorganic materials [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 5
- 239000011159 matrix material Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 238000007725 thermal activation Methods 0.000 description 5
- 229910001566 austenite Inorganic materials 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000013013 elastic material Substances 0.000 description 4
- SZVJSHCCFOBDDC-UHFFFAOYSA-N ferrosoferric oxide Chemical compound O=[Fe]O[Fe]O[Fe]=O SZVJSHCCFOBDDC-UHFFFAOYSA-N 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 239000000725 suspension Substances 0.000 description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 3
- 230000006399 behavior Effects 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 230000005294 ferromagnetic effect Effects 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 235000013980 iron oxide Nutrition 0.000 description 3
- 229920000767 polyaniline Polymers 0.000 description 3
- 229910052709 silver Inorganic materials 0.000 description 3
- 239000004332 silver Substances 0.000 description 3
- MIZLGWKEZAPEFJ-UHFFFAOYSA-N 1,1,2-trifluoroethene Chemical group FC=C(F)F MIZLGWKEZAPEFJ-UHFFFAOYSA-N 0.000 description 2
- BQCIDUSAKPWEOX-UHFFFAOYSA-N 1,1-Difluoroethene Chemical compound FC(F)=C BQCIDUSAKPWEOX-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 239000002033 PVDF binder Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- HZEWFHLRYVTOIW-UHFFFAOYSA-N [Ti].[Ni] Chemical compound [Ti].[Ni] HZEWFHLRYVTOIW-UHFFFAOYSA-N 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000004020 conductor Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910001000 nickel titanium Inorganic materials 0.000 description 2
- 230000005298 paramagnetic effect Effects 0.000 description 2
- 229920002239 polyacrylonitrile Polymers 0.000 description 2
- 229920013639 polyalphaolefin Polymers 0.000 description 2
- 229920001088 polycarbazole Polymers 0.000 description 2
- 229920001601 polyetherimide Polymers 0.000 description 2
- 229920000123 polythiophene Polymers 0.000 description 2
- 229920000915 polyvinyl chloride Polymers 0.000 description 2
- 239000004800 polyvinyl chloride Substances 0.000 description 2
- 229920002981 polyvinylidene fluoride Polymers 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 229910001316 Ag alloy Inorganic materials 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001020 Au alloy Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000976 Electrical steel Inorganic materials 0.000 description 1
- 229910001218 Gallium arsenide Inorganic materials 0.000 description 1
- 244000043261 Hevea brasiliensis Species 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 108010052285 Membrane Proteins Proteins 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- 229910003781 PbTiO3 Inorganic materials 0.000 description 1
- 229910001252 Pd alloy Inorganic materials 0.000 description 1
- 229920001609 Poly(3,4-ethylenedioxythiophene) Polymers 0.000 description 1
- 229920002845 Poly(methacrylic acid) Polymers 0.000 description 1
- 239000004642 Polyimide Substances 0.000 description 1
- 229920002396 Polyurea Polymers 0.000 description 1
- 229920001328 Polyvinylidene chloride Polymers 0.000 description 1
- 229910001260 Pt alloy Inorganic materials 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910001128 Sn alloy Inorganic materials 0.000 description 1
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 229910002370 SrTiO3 Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- TUDPMSCYVZIWFW-UHFFFAOYSA-N [Ti].[In] Chemical compound [Ti].[In] TUDPMSCYVZIWFW-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 229920000800 acrylic rubber Polymers 0.000 description 1
- JRBRVDCKNXZZGH-UHFFFAOYSA-N alumane;copper Chemical compound [AlH3].[Cu] JRBRVDCKNXZZGH-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 229910002113 barium titanate Inorganic materials 0.000 description 1
- 239000012620 biological material Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- WJCRZORJJRCRAW-UHFFFAOYSA-N cadmium gold Chemical compound [Cd].[Au] WJCRZORJJRCRAW-UHFFFAOYSA-N 0.000 description 1
- NCOPCFQNAZTAIV-UHFFFAOYSA-N cadmium indium Chemical compound [Cd].[In] NCOPCFQNAZTAIV-UHFFFAOYSA-N 0.000 description 1
- NSAODVHAXBZWGW-UHFFFAOYSA-N cadmium silver Chemical compound [Ag].[Cd] NSAODVHAXBZWGW-UHFFFAOYSA-N 0.000 description 1
- UHYPYGJEEGLRJD-UHFFFAOYSA-N cadmium(2+);selenium(2-) Chemical compound [Se-2].[Cd+2] UHYPYGJEEGLRJD-UHFFFAOYSA-N 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000002041 carbon nanotube Substances 0.000 description 1
- 229910021393 carbon nanotube Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 229910001567 cementite Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 229940090961 chromium dioxide Drugs 0.000 description 1
- IAQWMWUKBQPOIY-UHFFFAOYSA-N chromium(4+);oxygen(2-) Chemical compound [O-2].[O-2].[Cr+4] IAQWMWUKBQPOIY-UHFFFAOYSA-N 0.000 description 1
- AYTAKQFHWFYBMA-UHFFFAOYSA-N chromium(IV) oxide Inorganic materials O=[Cr]=O AYTAKQFHWFYBMA-UHFFFAOYSA-N 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 229920001940 conductive polymer Polymers 0.000 description 1
- 229920000547 conjugated polymer Polymers 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- QRJOYPHTNNOAOJ-UHFFFAOYSA-N copper gold Chemical compound [Cu].[Au] QRJOYPHTNNOAOJ-UHFFFAOYSA-N 0.000 description 1
- HPDFFVBPXCTEDN-UHFFFAOYSA-N copper manganese Chemical compound [Mn].[Cu] HPDFFVBPXCTEDN-UHFFFAOYSA-N 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000005684 electric field Effects 0.000 description 1
- 239000007772 electrode material Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 229910052733 gallium Inorganic materials 0.000 description 1
- 239000000499 gel Substances 0.000 description 1
- 230000009477 glass transition Effects 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229920001519 homopolymer Polymers 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 150000002484 inorganic compounds Chemical class 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 229910001337 iron nitride Inorganic materials 0.000 description 1
- SORXVYYPMXPIFD-UHFFFAOYSA-N iron palladium Chemical compound [Fe].[Pd] SORXVYYPMXPIFD-UHFFFAOYSA-N 0.000 description 1
- PWBYYTXZCUZPRD-UHFFFAOYSA-N iron platinum Chemical compound [Fe][Pt][Pt] PWBYYTXZCUZPRD-UHFFFAOYSA-N 0.000 description 1
- VBMVTYDPPZVILR-UHFFFAOYSA-N iron(2+);oxygen(2-) Chemical class [O-2].[Fe+2] VBMVTYDPPZVILR-UHFFFAOYSA-N 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 238000005224 laser annealing Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 150000002894 organic compounds Chemical class 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- KDLHZDBZIXYQEI-UHFFFAOYSA-N palladium Substances [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 1
- 239000010452 phosphate Substances 0.000 description 1
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Substances [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 229920001432 poly(L-lactide) Polymers 0.000 description 1
- 229920000191 poly(N-vinyl pyrrolidone) Polymers 0.000 description 1
- 229920000553 poly(phenylenevinylene) Polymers 0.000 description 1
- 229920001464 poly(sodium 4-styrenesulfonate) Polymers 0.000 description 1
- 229920001467 poly(styrenesulfonates) Polymers 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920006254 polymer film Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920002689 polyvinyl acetate Polymers 0.000 description 1
- 239000005033 polyvinylidene chloride Substances 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- SBIBMFFZSBJNJF-UHFFFAOYSA-N selenium;zinc Chemical compound [Se]=[Zn] SBIBMFFZSBJNJF-UHFFFAOYSA-N 0.000 description 1
- 238000005480 shot peening Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229920005573 silicon-containing polymer Polymers 0.000 description 1
- 239000010944 silver (metal) Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 238000000844 transformation Methods 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/56—Means for adjusting the length of, or for locking, the spring or damper, e.g. at the end of the stroke
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
- E05B47/0009—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with thermo-electric actuators, e.g. heated bimetals
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
- E05B47/0011—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with piezoelectric actuators
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B81/00—Power-actuated vehicle locks
- E05B81/12—Power-actuated vehicle locks characterised by the function or purpose of the powered actuators
- E05B81/20—Power-actuated vehicle locks characterised by the function or purpose of the powered actuators for assisting final closing or for initiating opening
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
- F15B15/20—Other details, e.g. assembly with regulating devices
- F15B15/204—Control means for piston speed or actuating force without external control, e.g. control valve inside the piston
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
- F15B15/20—Other details, e.g. assembly with regulating devices
- F15B15/26—Locking mechanisms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B21/00—Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
- F15B21/06—Use of special fluids, e.g. liquid metal; Special adaptations of fluid-pressure systems, or control of elements therefor, to the use of such fluids
- F15B21/065—Use of electro- or magnetosensitive fluids, e.g. electrorheological fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/005—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion using electro- or magnetostrictive actuation means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/36—Special sealings, including sealings or guides for piston-rods
- F16F9/368—Sealings in pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/44—Means on or in the damper for manual or non-automatic adjustment; such means combined with temperature correction
- F16F9/46—Means on or in the damper for manual or non-automatic adjustment; such means combined with temperature correction allowing control from a distance, i.e. location of means for control input being remote from site of valves, e.g. on damper external wall
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/44—Means on or in the damper for manual or non-automatic adjustment; such means combined with temperature correction
- F16F9/46—Means on or in the damper for manual or non-automatic adjustment; such means combined with temperature correction allowing control from a distance, i.e. location of means for control input being remote from site of valves, e.g. on damper external wall
- F16F9/466—Throttling control, i.e. regulation of flow passage geometry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/54—Arrangements for attachment
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B15/00—Other details of locks; Parts for engagement by bolts of fastening devices
- E05B15/04—Spring arrangements in locks
- E05B2015/0493—Overcenter springs
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B51/00—Operating or controlling locks or other fastening devices by other non-mechanical means
- E05B51/005—Operating or controlling locks or other fastening devices by other non-mechanical means by a bimetallic or memory-shape element
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2224/00—Materials; Material properties
- F16F2224/02—Materials; Material properties solids
- F16F2224/025—Elastomers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2224/00—Materials; Material properties
- F16F2224/02—Materials; Material properties solids
- F16F2224/0258—Shape-memory metals, e.g. Ni-Ti alloys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2224/00—Materials; Material properties
- F16F2224/02—Materials; Material properties solids
- F16F2224/0283—Materials; Material properties solids piezoelectric; electro- or magnetostrictive
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2224/00—Materials; Material properties
- F16F2224/04—Fluids
- F16F2224/045—Fluids magnetorheological
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T292/00—Closure fasteners
- Y10T292/08—Bolts
- Y10T292/1043—Swinging
- Y10T292/1075—Operating means
- Y10T292/1082—Motor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T292/00—Closure fasteners
- Y10T292/17—Bendable securers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T292/00—Closure fasteners
- Y10T292/68—Keepers
- Y10T292/696—With movable dog, catch or striker
- Y10T292/699—Motor controlled
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T70/00—Locks
- Y10T70/50—Special application
- Y10T70/5093—For closures
Definitions
- This disclosure relates to strut assemblies whose stroke lengths can be customized depending upon external conditions and upon user preferences.
- Strut assemblies are often used in automobiles to facilitate the opening, locking and positioning of doors, trunks, hoods, tail-gates, or the like. These assemblies have stroke lengths that are fixed during the design, manufacturing or assembly process. This can pose a problem for users of articles to which the strut assembly is attached. For example, a tailgate lift having a large stroke length can rise beyond the reach of smaller vehicle users.
- strut assemblies that offer opportunities for customizing stroke length after the strut assembly has been assembled or after the strut assembly has been installed into an article such as a vehicle.
- a strut assembly comprising a housing; a piston in slideable communication with the housing; an actuator in operative communication with the piston and/or the housing; wherein the actuator is adapted to change the location of the housing from a first position to a second position and/or change in a stroke length of the piston.
- a method for changing the strut length of a strut assembly comprising activating an actuator that is in operative communication with a housing or a piston of the strut assembly; and changing in the location of the housing from a first position to a second position and/or changing a stroke length of the piston.
- FIG. 1 is a schematic depiction of a strut assembly 10 comprising a housing 2 that is in slideable communication with a piston head 14 and a piston rod 12 ;
- FIG. 2 is a schematic representation of an exemplary embodiment of the improved customizable strut assembly 10 of this disclosure wherein the assembly 10 comprises an actuator 16 disposed outside the housing 2 ;
- FIG. 3 is a schematic representation of an exemplary embodiment of the improved customizable strut assembly 10 wherein the assembly 10 comprises an actuator 16 disposed inside the housing 2 ;
- FIG. 4 is a schematic representation of another exemplary embodiment of the improved customizable strut assembly 10 wherein the actuator 16 comprises an active element 20 manufactured from a magnetorheological elastomer disposed inside the housing 2 ; and
- FIG. 5 is a depiction of a schematic representation of strut assembly 10 that comprises a sleeve 30 that is disposed upon the outer surface of the housing 2 .
- the sleeve 30 can be positioned along the housing to adjust the effective stroke length.
- a mechanical stop 34 can also be used to adjust the effective stroke length.
- strut assemblies whose stroke lengths can be customized to provide the user with effective reach and control over articles that are in operative communication with the struts.
- the article may be any device that utilizes spatial positioning such as a door in an automobile or a residential building; the hood, trunk or tailgate of a automobile; the jaws of a vice or a press; the platens on machine tools such as injection molding machines, compression molding machines; arbors and chucks on lathes and drilling machines, or the like.
- the customizable strut assemblies disclosed herein differ from those that are currently commercially available in that they comprise active materials that permit some functional attributes of the assemblies to be adjusted after manufacture.
- a car owner can adjust the stroke length of the customizable strut assembly to suit his or her anthropometrics.
- a dealer can advantageously adjust the strut length of the strut assembly at the point of sale to customize certain characteristics of an otherwise mass produced vehicle to suit the desires of a specific buyer.
- an owner can adjust the swing of an automobile door to prevent damage to the exterior of surrounding vehicles when the owner has to park repeatedly in tight parking spaces.
- the stroke length can be adjusted either via hardware tuning or via software changes.
- a strut assembly 10 comprises a housing 2 that is in slideable communication with a piston 3 .
- the piston 3 comprises a piston head 14 and a piston rod 12 .
- the piston head 14 is fixedly attached to the piston rod 12 .
- the housing 2 contains a fluid 4 .
- the piston head 14 has disposed in it channels 8 that permit the passage of fluid through the piston head 14 as it moves forward and backward in the housing 2 .
- Seals 6 are circumferentially disposed upon the piston head 14 and seal the space between the piston head 14 and the cylinder 2 . Seals 6 can also be optionally disposed between the piston rod 12 and the housing 2 .
- the strut assembly 10 is in operative communication with a supporting body 50 (e.g., the body of the vehicle) and is also in operative communication with a suspended body 60 (e.g., a panel that swings back and forth such as a door).
- the supporting body 50 and the suspended body 60 are disposed at opposing ends of the strut assembly 10 .
- FIG. 1 depicts the suspended body 60 as being contacted by the housing 2 and the supporting body 50 as being contacted by the piston rod 12 , it is envisioned that the suspended body 60 can be contacted by the piston rod 12 while the supporting body can be contacted by the housing 2 .
- the strut stroke-length As the geometries of the different elements of the strut assembly displayed in the FIG. 1 are fixed at the time of design and manufacture of the strut assembly 10 , there is no opportunity to vary the strut stroke-length to suit varying anthropometrics of the consumer. For example, the swing of a car door that employs the strut assembly of FIG. 1 cannot be increased to accommodate a very large person entering or exiting the car. Similarly, the swing of the door cannot be decreased to prevent the door from opening beyond the reach of a small person.
- the stroke length is generally varied by the inclusion of an actuator in the strut assembly.
- the actuator may be disposed within the housing or external to the housing.
- the actuator generally comprises an active element that comprises a shape memory material (active material).
- the actuator can comprise one or more active elements that can be arranged in series or in parallel inside or outside the housing.
- the actuator can be in operative communication with either the housing and/or the piston.
- the actuator can cause a change in the stroke length of the strut assembly by changing the distance between the supporting body and the suspended body. This is accomplished by changing the location of the housing with respect to the supporting body and/or the suspended body. By changing the location of the housing from a first position to a second position, the supporting body is correspondingly moved from its first position to a second position. This change in the strut length brought on by changing the location of the housing can be manually controlled and effected or it can be computer controlled.
- the actuator can cause a change in the strut length of the strut assembly by changing the effective stroke length of the piston. Activating the actuator changes the length of travel of the piston in the housing.
- the mean position of travel of the piston is changed.
- the mean position of travel of the piston is the location of mid-point of travel of the piston in the housing. For example, f the piston travels back and forth between points A and B in the housing (i.e., A and B represents the extremities of travel of the piston) then the mean position of travel will be the sum of A and B divided by 2.
- the length of travel can be changed, while the mean position of travel remains the same.
- the length of travel of the piston is changed while the mean position of travel is also changed. This change in the strut length brought on by changing the effective length of travel of the piston, which can be manually controlled and effected or it can be computer controlled.
- the assembly 10 comprises an actuator 16 interposed between the suspended body 60 and the housing 2 .
- the actuator 16 is in operative communication with the housing 2 and the suspended body 60 .
- the actuator 16 comprises one or more active elements 20 that can be adjusted to effectively increase the stroke length in a direction parallel to the direction of travel of the piston rod 12 .
- the actuator 16 may be used to assist the displacement of the suspended body 60 away from and/or towards the supporting body 50 depending upon the desires of the user.
- the actuator 16 can be in operative communication with the housing 2 or the piston rod 12 .
- actuators 16 that employ active elements 20 that comprise active materials are electric stepper motors, inchworms, piezoelectric inchworms, ultrasonic motors, electrohydrostatic actuators, nanomotion piezoelectric motors, compact hybrid actuator devices (CHAD), that may be employed in the actuator 16 .
- These motors can be used in the customizable strut assemblies 10 external to the housing 2 as depicted in the FIG. 2 and can facilitate a change in distance between the suspended body 60 and the supporting body 50 .
- the active element 20 can involve a coil spring, a wire or other geometrical shape manufactured from an active material that can facilitate a change in distance between the suspended body 60 and the supporting body 50 .
- Shape memory materials generally refer to materials or compositions that have the ability to revert to a specified configuration (e.g. crystal structure, shape, or the like) in response to suitable external stimuli, e.g., an activation signal.
- exemplary shape memory materials suitable for use in the present disclosure include shape memory alloys, ferromagnetic shape memory alloys, shape memory polymers and composites of the foregoing shape memory materials with non-shape memory materials, and combinations comprising at least one of the foregoing shape memory materials.
- the class of active materials used in the customizable strut assembly 10 are those that change their shape in proportion to the strength of the applied field but then return to their original shape upon the discontinuation of the field.
- Exemplary active materials in this category are electroactive polymers (dielectric polymers), piezoelectrics, and piezoceramics.
- Activation signals can employ an electrical stimulus, a magnetic stimulus, a chemical stimulus, a mechanical stimulus, a thermal stimulus, or a combination comprising at least one of the foregoing stimuli.
- the return to the original shape is accomplished by the use of a restoring force such as, for example, a biasing spring.
- Exemplary materials that can employ a restoring force are shape memory alloys.
- Shape memory alloys generally refer to a group of metallic materials that demonstrate the ability to return to some previously defined shape or size when subjected to an appropriate thermal stimulus. Shape memory alloys are capable of undergoing phase transitions in which their elastic modulus, yield strength, and shape orientation are altered as a function of temperature. Generally, in the low temperature, or martensite phase, shape memory alloys can be plastically deformed and upon exposure to a specified higher temperature will transform to an austenite phase, or parent phase, attempting to return to their shape prior to the deformation. Materials that exhibit this shape memory effect only upon heating are referred to as having one-way shape memory. Those materials that also exhibit shape memory upon re-cooling are referred to as having two-way shape memory behavior.
- Shape memory alloys can exhibit a one-way shape memory effect, an intrinsic two-way effect, or an extrinsic two-way shape memory.
- Annealed shape memory alloys generally exhibit the one-way shape memory effect. Sufficient heating subsequent to low-temperature deformation of the shape memory material will induce the martensite to austenite type transition, and the material will recover the original, annealed shape. Hence, one-way shape memory effects are only observed upon heating.
- Intrinsic two-way shape memory alloys are characterized by a shape transition both upon heating from the martensite phase to the austenite phase, as well as an additional shape transition upon cooling from the austenite phase back to the martensite phase.
- active connector elements that exhibit the extrinsic two-way shape memory effects are composite or multi-component materials that combine a shape memory alloy composition that exhibits a one-way effect with another element that provides a restoring force to return the first plate another position or to its original position.
- Active elements that exhibit an intrinsic one-way shape memory effect are fabricated from a shape memory alloy composition that will cause the active elements to automatically reform themselves as a result of the above noted phase transformations.
- Intrinsic two-way shape memory behavior must be induced in the shape memory material through thermo-mechanical processing. Such procedures include extreme deformation of the material while in the martensite phase, heating-cooling under constraint or load, or surface modification such as laser annealing, polishing, or shot-peening. Once the material has been trained to exhibit the two-way shape memory effect, the shape change between the low and high temperature states is generally reversible and persists through a high number of thermal cycles.
- the temperature at which the shape memory alloy remembers its high temperature form when heated can be adjusted by slight changes in the composition of the alloy and through heat treatment. In nickel-titanium shape memory alloys, for instance, it can be changed from above about 100° C. to below about ⁇ 100° C.
- the shape recovery process occurs over a range ofjust a few degrees and the start or finish of the transformation can be controlled to within a few degrees depending on the alloy composition.
- Suitable shape memory alloy materials for fabricating the active elements include nickel-titanium based alloys, indium-titanium based alloys, nickel-aluminum based alloys, nickel-gallium based alloys, copper based alloys (e.g., copper-zinc alloys, copper-aluminum alloys, copper-gold, and copper-tin alloys), gold-cadmium based alloys, silver-cadmium based alloys, indium-cadmium based alloys, manganese-copper based alloys, iron-platinum based alloys, iron-palladium based alloys, or the like, or a combination comprising at least one of the foregoing shape memory alloys.
- the alloys can be binary, ternary, or any higher order so long as the alloy composition exhibits a shape memory effect, e.g., change in shape orientation, changes in yield strength, and/or flexural modulus properties, damping capacity, and the like.
- the thermal activation signal may be applied to the shape memory alloy in various ways. It is generally desirable for the thermal activation signal to promote a change in the temperature of the shape memory alloy to a temperature greater than or equal to its austenitic transition temperature. Suitable examples of such thermal activation signals that can promote a change in temperature are the use of steam, hot oil, resistive electrical heating, or the like, or a combination comprising at least one of the foregoing signals. A preferred thermal activation signal is one derived from resistive electrical heating.
- the active element 20 may also be an electrically active polymer. Electrically active polymers are also commonly known as electroactive polymers (EAP's). The key design feature of devices based on these materials is the use of compliant electrodes that enable polymer films to expand or contract in the in-plane directions in response to applied electric fields or mechanical stresses. When electroactive polymers are used as the active element 20 , strains of greater than or equal to about 100%, pressures greater than or equal to about 50 kilograms/square centimeter (kg/cm 2 ) can be developed in response to an applied voltage. The good electromechanical response of these materials, as well as other characteristics such as good environmental tolerance and long-term durability, make them suitable for use in active elements under a variety of manufacturing conditions. Electroactive polymers are suitable for use as an active element in many customizable strut assembly 10 configurations.
- Electroactive polymer actuator elements used in customizable strut assembly 10 may be selected based on one or more material properties such as a high electrical breakdown strength, a low modulus of elasticity-(for small deformations), a high dielectric constant, and the like.
- a polymer is selected such that is has an elastic modulus at most about 100 MPa.
- the polymer is selected such that is has a maximum actuation pressure between about 0.05 MPa and about 10 MPa, and preferably between about 0.3 MPa and about 3 MPa.
- the polymer is selected such that is has a dielectric constant between about 2 and about 20, and preferably between about 2.5 and about 12. The present disclosure is not intended to be limited to these ranges.
- electroactive polymers may be fabricated and implemented as thin films. Thicknesses suitable for these thin films may be below 50 micrometers.
- electrodes attached to the polymers should also deflect without compromising mechanical or electrical performance.
- electrodes suitable for use may be of any shape and material provided that they are able to supply a suitable voltage to, or receive a suitable voltage from, an Electroactive polymer. The voltage may be either constant or varying over time.
- the electrodes adhere to a surface of the polymer. Electrodes adhering to the polymer are preferably compliant and conform to the changing shape of the polymer.
- the present disclosure may include compliant electrodes that conform to the shape of an electroactive polymer to which they are attached. The electrodes may be only applied to a portion of an electroactive polymer and define an active area according to their geometry.
- Electrodes suitable for use with the present disclosure include structured electrodes comprising metal traces and charge distribution layers, textured electrodes comprising varying out of plane dimensions, conductive greases such as carbon greases or silver greases, colloidal suspensions, high aspect ratio conductive materials such as carbon fibrils and carbon nanotubes, and mixtures of ionically conductive materials.
- Suitable materials used in an electrode may include graphite, carbon black, colloidal suspensions, thin metals including silver and gold, silver filled and carbon filled gels and polymers, and ionically or electronically conductive polymers. It is understood that certain electrode materials may work well with particular polymers and may not work as well for others. By way of example, carbon fibrils work well with acrylic elastomer polymers while not as well with silicone polymers.
- electroactive polymers used herein are generally conjugated polymers. Suitable examples of electroactive polymers are poly(aniline), substituted poly(aniline)s, polycarbazoles, substituted polycarbazoles, polyindoles, poly(pyrrole)s, substituted poly(pyrrole)s, poly(thiophene)s, substituted poly(thiophene)s, poly(acetylene)s, poly(ethylene dioxythiophene)s, poly(ethylenedioxypyrrole)s, poly(p-phenylene vinylene)s, or the like, or combinations comprising at least one of the foregoing electroactive polymers. Blends or copolymers or composites of the foregoing electroactive polymers may also be used. Similarly blends or copolymers or composites of an electroactive polymers with an electroactive polymers precursor may also be used.
- the actuator element 20 used in the customizable strut assembly 10 may also comprise a piezoelectric material.
- the piezoelectric material may be configured for providing rapid deployment.
- piezoelectric is used to describe a material that mechanically deforms (changes shape and/or size) when a voltage potential is applied, or conversely, generates an electrical charge when mechanically deformed.
- a transmission e.g. a compliant mechanism
- a piezoelectric material is disposed on strips of a flexible metal sheet.
- the piezo actuators are coupled to the sheet in a manner that causes bending or unbending of the sheet when the actuators are activated.
- the ability of the bending mode of deformation in a flexible shell to amplify small axial strains into larger rotary displacements is used to advantage.
- the strips can be unimorph or bimorph.
- the strips are bimorph, because bimorphs generally exhibit more displacement than unimorphs.
- a bimorph device In contrast to the unimorph piezoelectric device, a bimorph device includes an intermediate flexible metal foil sandwiched between two piezoelectric elements. Bimorphs exhibit more displacement than unimorphs because under the applied voltage one ceramic element will contract while the other expands. Bimorphs can exhibit strains up to about 20%, but similar to unimorphs, generally cannot sustain high loads relative to the overall dimensions of the unimorph structure.
- Suitable piezoelectric materials include inorganic compounds, organic compounds, and metals.
- organic materials all of the polymeric materials with non-centrosymmetric structure and large dipole moment group(s) on the main chain or on the side-chain, or on both chains within the molecules, can be used as candidates for the piezoelectric film.
- suitable polymers include, for example, but are not limited to, poly(sodium 4-styrenesulfonate) (“PSS”), poly S- 119 (poly(vinylamine) backbone azo chromophore), and their derivatives; polyfluorocarbons, including polyvinylidene fluoride (“PVDF”), its co-polymer vinylidene fluoride (“VDF”), trifluoroethylene (TrFE), and their derivatives; polychlorocarbons, including poly(vinyl chloride) (“PVC”), polyvinylidene chloride (“PVC2”), and their derivatives; polyacrylonitriles (“PAN”), and their derivatives; polycarboxylic acids, including poly(methacrylic acid (“PMA”), and their derivatives; polyureas, and their derivatives; polyurethanes (“PUE”), and their derivatives; bio-polymer molecules such as poly-L-lactic acids and their derivatives, and membrane proteins, as well as
- piezoelectric materials can include Pt, Pd, Ni, Ti, Cr, Fe, Ag, Au, Cu, and metal alloys and mixtures thereof. These piezoelectric materials can also include, for example, metal oxide such as SiO 2 , Al 2 O 3 , ZrO 2 , TiO 2 , SrTiO 3 , PbTiO 3 , BaTiO 3 , FeO 3 , Fe 3 O 4 , ZnO, and mixtures thereof; and Group VIA and IIB compounds, such as CdSe, CdS, GaAs, AgCaSe 2 , ZnSe, GaP, InP, ZnS, and mixtures thereof.
- metal oxide such as SiO 2 , Al 2 O 3 , ZrO 2 , TiO 2 , SrTiO 3 , PbTiO 3 , BaTiO 3 , FeO 3 , Fe 3 O 4 , ZnO, and mixtures thereof.
- Group VIA and IIB compounds such as Cd
- the active element 20 can also comprise magnetorheological (MRE) elastomers.
- Magnetorheological elastomers are suspensions of micrometer-sized, magnetically polarizable particles in a polymeric elastomer. When a magnetorheological elastomer is exposed to a magnetic field, the normally randomly oriented particles form chains of particles in the direction of the magnetic field lines. The particle chains increase the effective stiffness of the elastomer. The change in the effective stiffness of the MRE is accomplished by changing the shear and compression/tension modulii of the magnetorheological elastomer by varying the strength of the applied magnetic field.
- the magnetorheological elastomers typically develop structure when exposed to a magnetic field in as little as a few milliseconds. Discontinuing the exposure of the magnetorheological elastomer to the magnetic field reverses the process and the elastomer returns to a lower viscosity state.
- Suitable magnetorheological elastomer materials include an elastic polymer matrix comprising a suspension of ferromagnetic or paramagnetic particles, wherein the particles are described above.
- Suitable polymer matrices include poly-alpha-olefins, copolymers of poly-alpha-olefins and natural rubber.
- Suitable ferromagnetic or paramagnetic include iron; iron alloys, such as those including aluminum, silicon, cobalt, nickel, vanadium, molybdenum, chromium, tungsten, manganese and/or copper; iron oxides, including Fe 2 O 3 and Fe 3 O 4 ; iron nitride; iron carbide; carbonyl iron; nickel and alloys of nickel; cobalt and alloys of cobalt; chromium dioxide; stainless steel; silicon steel; or the like, or a combination comprising at least one of the foregoing particles.
- suitable iron particles include straight iron powders, reduced iron powders, iron oxide powder/straight iron powder mixtures and iron oxide powder/reduced iron powder mixtures.
- a preferred magnetic-responsive particulate is carbonyl iron, preferably, reduced carbonyl iron.
- the particle size should be selected so that the particles exhibit multi-domain characteristics when subjected to a magnetic field. Diameter sizes for the particles can be less than or equal to about 1,000 micrometers, with less than or equal to about 500 micrometers preferred, and less than or equal to about 100 micrometers more preferred. Also preferred is a particle diameter of greater than or equal to about 0.1 micrometer, with greater than or equal to about 0.5 more preferred, and greater than or equal to about 10 micrometer especially preferred. The particles are preferably present in an amount between about 5.0 and about 50 percent by volume of the total composition.
- an external stimulus is applied to the active element 20 .
- a preferred external stimulus is one derived from thermal activation preferably one that is derived from resistive electrical heating.
- the active element 20 can be a composite of SMP, an elastic material and one or more active material based actuators (e.g. SMA or EAP); or a composite of SMP and an elastic material; or a sub-assembly comprising one or more active material based actuators that are mechanically coupled to elastic restoring elements; etc.
- the overall axial dimension of the active element can be changed in response to the activation signal to achieve the desired strut stroke adjustment. This change in length facilitates the displacement of the suspended body 60 with respect to the supporting body 50 , thereby changing the effective stroke length of the customizable strut assembly 10 .
- the magnitude of the change in length can be proportioned to the magnitude of the activation signal.
- FIGS. 3 and 4 depict exemplary embodiments of customizable strut assemblies that utilize active elements that are disposed inside the housing 2 .
- the customizable strut assembly 10 comprises plates 22 that are in operative communication with the active element 20 .
- the plates are perforated to allow easy passage for the fluid.
- the plates 22 and the active element 20 are disposed within the housing 2 .
- the active element 20 for purposed of this embodiment is a coil spring, though it can be varied in shape and size in other configurations.
- the plates 22 are disposed on opposing sides of the piston head 14 and are in operative communication with the piston head 14 .
- the perforations in the plate 22 allow for a smooth displacement of the fluid 4 within the housing 2 as the piston 3 slides back and forth in the housing 2 .
- the ends of the strut stroke are marked by (near) contact between the flat ends of the piston head and the respective cylinder ends.
- the end of stroke is marked by contact between the elements 22 and the respective ends of the cylinder. Therefore, it is clear that by changing the axial length and/or the stiffness of the active elements 20 , the effective stroke of the strut can be adjusted.
- the active element 20 can be a composite of a shape memory polymer, an elastic material and one or more active material based actuators (e.g., a shape memory alloy or and electroactive polymer); or a composite of shape memory polymer and an elastic material; or a sub-assembly comprising one or more active material based actuators that are mechanically coupled to elastic restoring elements; or the like.
- the overall axial dimension of the actuator can be changed in response to the activation signal to achieve the desired strut stroke adjustment.
- the change in the stroke may stay in effect until it is changed again, or the change may be made just-in-time for an operation and will remain in effect only for that operation.
- the active element 20 comprises a spring made of a shape memory alloy in its martensitic-phase over the operating temperature range for the strut.
- the actuator 16 generally comprises an active element 20 that comprises an active material.
- An active material generally refers to a group of materials that demonstrate an ability to return to some previously defined shape or size when subjected to an appropriate external stimulus. The active material, upon activation facilitates the displacement of the suspended body 60 towards and/or away from the supporting body 50 and also permits control over the magnitude of the displacement.
- the actuator 16 can also comprise a composite of an active material.
- the composite can comprise a shape memory alloy and a shape memory polymer.
- the composite can comprise a shape memory alloy and a material that is not an active material, i.e., a material that does not return to some previously defined shape or size when subjected to an appropriate external stimulus.
- the composite can comprise two or more active materials such as for example a shape memory alloy and a shape memory polymer in addition to and a material that is not an active material.
- an actuator can comprise a composite that comprises one or more elastic elements made from spring steel distributed within a shape memory polymer matrix together with one or more shape memory alloy elements.
- the shape memory polymer has a characteristic temperature known as its glass transition temperature (Tg), such that the elastic modulus of the material drops significantly e.g., a factor of about 30 to about 150 when it is heated above its Tg.
- Tg glass transition temperature
- the shape memory polymer is a soft and easily pliable polymer above the Tg, and it can be deformed significantly (up to 200% recoverable strain) by a relatively low force.
- the material On cooling the deformed shape memory polymer below its Tg, the material reverts back to its stiffer form, while retaining the deformed shape in a stress-free condition. If a specified limiting temperature is not exceeded during the heating process, the aforementioned procedure comprising heating, deforming and cooling can be repeated multiple times.
- the elastic elements in the above embodiment are mechanically coupled to the shape memory polymer matrix and, they determine the overall configuration (i.e. geometry, dimensions, etc) of the active element.
- the relative stiffnesses of the elastic elements and the shape memory polymer matrix are chosen such that, when the shape memory polymer is below the lower Tg, it is the dominant contributor to the overall stiffness of the actuator; whereas when the shape memory polymer is above the Tg, the elastic elements are the dominant contributors to the overall active element stiffness.
- they can either compress or elongate the elastic elements and thereby, control the overall configuration of the active element when the shape memory polymer is above the Tg.
- the use of the actuator can be illustrated by describing the process in which the actuator is reconfigured to tailor the strut-stroke.
- the shape memory polymer is softened by heating it to a temperature above its Tg.
- the shape memory alloy elements are then activated to change the overall configuration of the actuator while the shape memory polymer is soft.
- the desired configuration e.g. axial dimension
- the shape memory polymer is allowed to cool down to a temperature below its Tg, whereupon it regains its stiff form.
- the shape memory alloy elements are then powered off.
- the stiffness of the shape memory polymer matrix dominates that of the elastic elements, and hence the active element will retain the above configuration until it is heated above its Tg.
- the above reconfiguration process can then be repeated.
- the active elements 20 are compressed at one or both ends of the strut's stroke. If the stiffness of these active elements 20 is small, e.g., when the shape memory alloy is in its martensitic phase, they can be easily compressed between the piston 3 and the housing 2 . Hence, they will not affect the length of the stroke. However, if the stiffness of the active elements is high, e.g., when the shape memory alloy is in its austenitic phase, they resist relative motion between the piston 2 and the housing 2 with considerable force at the extremities of the strut's stroke. The amount of change in the stroke length is directly proportional to the length of the active element 20 and its stiffness. Thus a stiffening of the active element 20 upon activation will result in a reduction of the effective stroke length for the customizable strut assembly 10 .
- the length of the active element 20 can be varied, thereby varying the length of travel of the piston 3 in the housing 2 . This will alter the stroke length of the strut assembly 10 .
- the activation signal can be a thermal signal brought on by resistive heating of the spring.
- similar plates can also be connected to one or both ends of the housing 2 through active elements 20 , whose lengths and/or stiffnesses can be varied upon activation.
- varying the stiffness of the various active elements in the strut assembly can enable control over which part of the stroke is curtailed (e.g., the tailgate lift needs to be reduced for shorter owners; the tailgate may need to be held partially open when transporting over size cargo that extends partially out of the vehicle, in which case the tailgate closure needs to be restricted), and afford smoother operation of the customizable strut assembly 10 .
- the customizable strut assembly can be modified to function in various modes.
- the spring when the spring is in its martensitic phase over the temperature range of operation of the customizable strut assembly 10 , it has a low stiffness and hence a low spring constant than when it is in the austenitic form. Passage of an electric current through the spring can induce a martensitic to austenitic transition in the spring material, thereby increasing its stiffness e.g. three-fold.
- the dual-stiffness nature of the SMA spring can be used to vary the stroke of the strut as described above. Depending on the composition of the shape memory alloy material, the transition from soft to stiff can be sharp or gradual, thereby yielding greater control over the behavior of the strut at the extremities of its stroke.
- magnetorheological elastomers can be employed as the active element 20 .
- the piston 3 comprises an electromagnet 26 that is in mechanical and electrical communication with the magnetorheological elastomer of the active element 20 .
- the magnetorheological elastomer is in the form of a block that is disposed on opposing surfaces of the piston head 14 .
- the active element 20 has a size effective to vary the length of the stroke as its stiffness is increased.
- the stiffness of the magnetorheological elastomer can be varied by varying the strength of the magnetic field, the change in stiffness can be controlled by varying the electrical current passing through the electromagnet.
- the stiffness of the magnetorheological elastomer By changing the stiffness of the magnetorheological elastomer, the length of the stroke can be varied in a manner that is conceptually similar to that described above in the context of SMA springs. As the elastomer becomes less stiff, it can be easily compressed between the piston 3 and the inner surface of the housing 2 , thereby permitting a larger stroke length.
- the electrical current is varied to increase the stiffness of the elastomer, it cannot be easily deformed between the piston 3 and the inner surface of the housing 2 .
- the length of travel of the customizable strut assembly 10 can be adjusted.
- a biasing permanent magnet whose influence on the MRE can be counteracted by an electromagnet allows this concept to be extended to both: increase and decrease the effective strut stroke.
- the strut assembly 10 comprises a sleeve 30 that is disposed upon the outer surface of the housing 2 .
- the sleeve 30 is hollow and comprises a braking mechanism 32 that fixedly attaches it to the housing 2 depending upon the user's preference.
- the sleeve 30 can have any suitable cross-sectional geometry that permits slideable motion with the housing 2 , when the braking mechanism 32 is released.
- the braking mechanism is generally released when it is desirable to change the effective length of the strut assembly 10 after which it is reengaged to fixedly attach the sleeve 32 to the housing 2 .
- the braking mechanism 32 can be engaged or disengaged by a suitable stimulus to change the effective length of the strut assembly. Adjusting the position of the sleeve 32 controls the distance labeled DS 2 .
- a mechanical stop 34 is fixedly attached to the piston rod 12 at the user's discretion and can be used to adjust the effective stroke length by displacing the mechanical stop when desired.
- the location of the mechanical stop 34 determines the distance DS 1 as shown in the FIG. 5 .
- the mechanical stop 34 can be adjusted upon temporary removal of the sleeve 30 .
- the sleeve 30 can be freely positioned at any desirable point over the length of the housing 2 subject to mechanical interference constraints imposed by the cylinder dimensions.
- the effective-length of the strut assembly is controlled by the larger of the two distances, DS 1 and DS 2 .
- the motion of the suspended body 60 is governed by the smaller of the two distances DO 1 and DO 2 as shown in the FIG. 5 . These correspond to mechanical interference between the piston 3 and the end of the cylinder proximate to the supporting body 50 , and between the end of the cylinder proximate to the supporting body 50 and the mechanical stop 34 . Changing the position of the mechanical stop 34 allows the length DO 2 to be adjusted. This affords control over the motion of the suspended body 60 when it is to be opened completely.
- the position of the mechanical stop 34 can be adjusted using an optional biasing spring 36 as depicted in the FIG. 5 .
- the bias spring can be of a length effective to keep the mechanical stop in communication with the end of the sleeve 30 proximate to the supporting body 50 .
- the spring force i.e., the spring constant
- the spring 36 does not affect the position of the mechanical stop 32 , when the brake is engaged.
- the mechanical stop 34 is disengaged and the braking mechanism 32 is engaged thereby permitting the swing panel to be displaced into the desired fully-open position. At this point the mechanical stop 34 is engaged locking in the range of desired motion for the strut assembly 10 .
- the sleeve 30 moves with the suspended body 60 during its motion and the mechanical stop 34 moves with the spring 36 to its new location.
- the desired fully-shut position can be set in a similar way.
- the braking mechanism 32 is disengaged and the suspended body 60 is moved to the desired fully-shut position before the braking mechanism 32 is engaged again.
- the piston rod 3 can be used to displace the sleeve 30 to the desired position.
- a soft bias spring (not shown) can be used to keep the sleeve 30 flush against the end of the piston rod that is proximate to the supporting body 50 .
- the ability to customize the length of travel of a customizable strut assembly 10 can be advantageously used in automobiles, aircraft, ships, in machine tools, or the like, to improve usability.
- the length of travel can be adjusted at any time during the life cycle of an article that employs the customizable strut assembly.
- the length of travel can also be adjusted to accommodate ambient weather conditions, consumer anthropometrics or to offset the deleterious effects of component wear.
- the length of travel can be adjusted manually or by computer as desired.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Fluid-Damping Devices (AREA)
- Springs (AREA)
- Infusion, Injection, And Reservoir Apparatuses (AREA)
- Actuator (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Prostheses (AREA)
- Lock And Its Accessories (AREA)
- Chairs Characterized By Structure (AREA)
- Orthopedics, Nursing, And Contraception (AREA)
- Sealing Devices (AREA)
- General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
Abstract
Description
- This application claims the benefit of U.S. Provisional Application Ser. No. 60/552,791 filed Mar. 12, 2004, the entire contents of which are hereby incorporated by reference.
- This disclosure relates to strut assemblies whose stroke lengths can be customized depending upon external conditions and upon user preferences.
- Strut assemblies are often used in automobiles to facilitate the opening, locking and positioning of doors, trunks, hoods, tail-gates, or the like. These assemblies have stroke lengths that are fixed during the design, manufacturing or assembly process. This can pose a problem for users of articles to which the strut assembly is attached. For example, a tailgate lift having a large stroke length can rise beyond the reach of smaller vehicle users.
- It is therefore desirable to use strut assemblies that offer opportunities for customizing stroke length after the strut assembly has been assembled or after the strut assembly has been installed into an article such as a vehicle.
- Disclosed herein is a strut assembly comprising a housing; a piston in slideable communication with the housing; an actuator in operative communication with the piston and/or the housing; wherein the actuator is adapted to change the location of the housing from a first position to a second position and/or change in a stroke length of the piston.
- Disclosed herein too is a method for changing the strut length of a strut assembly comprising activating an actuator that is in operative communication with a housing or a piston of the strut assembly; and changing in the location of the housing from a first position to a second position and/or changing a stroke length of the piston.
-
FIG. 1 is a schematic depiction of astrut assembly 10 comprising ahousing 2 that is in slideable communication with apiston head 14 and apiston rod 12; -
FIG. 2 is a schematic representation of an exemplary embodiment of the improvedcustomizable strut assembly 10 of this disclosure wherein theassembly 10 comprises anactuator 16 disposed outside thehousing 2; -
FIG. 3 is a schematic representation of an exemplary embodiment of the improvedcustomizable strut assembly 10 wherein theassembly 10 comprises anactuator 16 disposed inside thehousing 2; -
FIG. 4 is a schematic representation of another exemplary embodiment of the improvedcustomizable strut assembly 10 wherein theactuator 16 comprises anactive element 20 manufactured from a magnetorheological elastomer disposed inside thehousing 2; and -
FIG. 5 is a depiction of a schematic representation ofstrut assembly 10 that comprises asleeve 30 that is disposed upon the outer surface of thehousing 2. Thesleeve 30 can be positioned along the housing to adjust the effective stroke length. Amechanical stop 34 can also be used to adjust the effective stroke length. - Disclosed herein are strut assemblies whose stroke lengths can be customized to provide the user with effective reach and control over articles that are in operative communication with the struts. The article may be any device that utilizes spatial positioning such as a door in an automobile or a residential building; the hood, trunk or tailgate of a automobile; the jaws of a vice or a press; the platens on machine tools such as injection molding machines, compression molding machines; arbors and chucks on lathes and drilling machines, or the like.
- The customizable strut assemblies disclosed herein differ from those that are currently commercially available in that they comprise active materials that permit some functional attributes of the assemblies to be adjusted after manufacture. In one example, a car owner can adjust the stroke length of the customizable strut assembly to suit his or her anthropometrics. In another example, a dealer can advantageously adjust the strut length of the strut assembly at the point of sale to customize certain characteristics of an otherwise mass produced vehicle to suit the desires of a specific buyer. In another embodiment, an owner can adjust the swing of an automobile door to prevent damage to the exterior of surrounding vehicles when the owner has to park repeatedly in tight parking spaces. In an exemplary embodiment, the stroke length can be adjusted either via hardware tuning or via software changes.
- With reference to the
FIG. 1 , which represents the prior art, astrut assembly 10 comprises ahousing 2 that is in slideable communication with apiston 3. Thepiston 3 comprises apiston head 14 and apiston rod 12. Thepiston head 14 is fixedly attached to thepiston rod 12. Thehousing 2 contains afluid 4. Thepiston head 14 has disposed in itchannels 8 that permit the passage of fluid through thepiston head 14 as it moves forward and backward in thehousing 2.Seals 6 are circumferentially disposed upon thepiston head 14 and seal the space between thepiston head 14 and thecylinder 2.Seals 6 can also be optionally disposed between thepiston rod 12 and thehousing 2. Thestrut assembly 10 is in operative communication with a supporting body 50 (e.g., the body of the vehicle) and is also in operative communication with a suspended body 60 (e.g., a panel that swings back and forth such as a door). The supportingbody 50 and the suspendedbody 60 are disposed at opposing ends of thestrut assembly 10. - While the
FIG. 1 depicts the suspendedbody 60 as being contacted by thehousing 2 and the supportingbody 50 as being contacted by thepiston rod 12, it is envisioned that the suspendedbody 60 can be contacted by thepiston rod 12 while the supporting body can be contacted by thehousing 2. - As the
piston rod 12 slides back and forth in thehousing 2 during the expansion or contraction of the strut assembly, thefluid 4 is forced to flow through thechannels 8 in thepiston head 14. This flow is restricted by thechannels 8 and the restricted flow gives rise to two forces that resist relative motion between the piston and the cylinder, an elastic force arising out of the compression of the fluid column that the piston head is pushing against, and a hydrodynamic force arising from the resistance to fluid flow through thechannels 8 in thepiston head 14. Friction brought on by the presence of theseal 6 between thepiston head 14 and the inner wall of thehousing 2, or between thepiston rod 12 and thehousing 2, also resists relative motion between the piston head and the cylinder. - As the geometries of the different elements of the strut assembly displayed in the
FIG. 1 are fixed at the time of design and manufacture of thestrut assembly 10, there is no opportunity to vary the strut stroke-length to suit varying anthropometrics of the consumer. For example, the swing of a car door that employs the strut assembly ofFIG. 1 cannot be increased to accommodate a very large person entering or exiting the car. Similarly, the swing of the door cannot be decreased to prevent the door from opening beyond the reach of a small person. - By being able to vary the stroke length of the
strut assembly 10, the distance between the suspendedbody 60 and the supportingbody 50 can be adjusted accordingly as desired. The stroke length is generally varied by the inclusion of an actuator in the strut assembly. The actuator may be disposed within the housing or external to the housing. The actuator generally comprises an active element that comprises a shape memory material (active material). The actuator can comprise one or more active elements that can be arranged in series or in parallel inside or outside the housing. - The actuator can be in operative communication with either the housing and/or the piston. In one embodiment, the actuator can cause a change in the stroke length of the strut assembly by changing the distance between the supporting body and the suspended body. This is accomplished by changing the location of the housing with respect to the supporting body and/or the suspended body. By changing the location of the housing from a first position to a second position, the supporting body is correspondingly moved from its first position to a second position. This change in the strut length brought on by changing the location of the housing can be manually controlled and effected or it can be computer controlled.
- In another embodiment, the actuator can cause a change in the strut length of the strut assembly by changing the effective stroke length of the piston. Activating the actuator changes the length of travel of the piston in the housing. In one embodiment, upon changing the length of travel of the piston in the housing, the mean position of travel of the piston is changed. The mean position of travel of the piston is the location of mid-point of travel of the piston in the housing. For example, f the piston travels back and forth between points A and B in the housing (i.e., A and B represents the extremities of travel of the piston) then the mean position of travel will be the sum of A and B divided by 2. Thus in one embodiment, upon actuating the actuator, the length of travel can be changed, while the mean position of travel remains the same. In another embodiment, the length of travel of the piston is changed while the mean position of travel is also changed. This change in the strut length brought on by changing the effective length of travel of the piston, which can be manually controlled and effected or it can be computer controlled.
- With reference now to the
FIG. 2 , which represents an embodiment of the improvedcustomizable strut assembly 10 of this disclosure, theassembly 10 comprises anactuator 16 interposed between the suspendedbody 60 and thehousing 2. Theactuator 16 is in operative communication with thehousing 2 and the suspendedbody 60. Theactuator 16 comprises one or moreactive elements 20 that can be adjusted to effectively increase the stroke length in a direction parallel to the direction of travel of thepiston rod 12. Theactuator 16 may be used to assist the displacement of the suspendedbody 60 away from and/or towards the supportingbody 50 depending upon the desires of the user. As noted above, theactuator 16 can be in operative communication with thehousing 2 or thepiston rod 12. - In one embodiment, a suitable example of
actuators 16 that employactive elements 20 that comprise active materials are electric stepper motors, inchworms, piezoelectric inchworms, ultrasonic motors, electrohydrostatic actuators, nanomotion piezoelectric motors, compact hybrid actuator devices (CHAD), that may be employed in theactuator 16. These motors can be used in thecustomizable strut assemblies 10 external to thehousing 2 as depicted in theFIG. 2 and can facilitate a change in distance between the suspendedbody 60 and the supportingbody 50. In another embodiment, theactive element 20 can involve a coil spring, a wire or other geometrical shape manufactured from an active material that can facilitate a change in distance between the suspendedbody 60 and the supportingbody 50. - Shape memory materials generally refer to materials or compositions that have the ability to revert to a specified configuration (e.g. crystal structure, shape, or the like) in response to suitable external stimuli, e.g., an activation signal. Exemplary shape memory materials suitable for use in the present disclosure include shape memory alloys, ferromagnetic shape memory alloys, shape memory polymers and composites of the foregoing shape memory materials with non-shape memory materials, and combinations comprising at least one of the foregoing shape memory materials. In another embodiment, the class of active materials used in the
customizable strut assembly 10 are those that change their shape in proportion to the strength of the applied field but then return to their original shape upon the discontinuation of the field. Exemplary active materials in this category are electroactive polymers (dielectric polymers), piezoelectrics, and piezoceramics. Activation signals can employ an electrical stimulus, a magnetic stimulus, a chemical stimulus, a mechanical stimulus, a thermal stimulus, or a combination comprising at least one of the foregoing stimuli. In one embodiment, the return to the original shape is accomplished by the use of a restoring force such as, for example, a biasing spring. Exemplary materials that can employ a restoring force are shape memory alloys. - For convenience and by way of example, reference herein will be made to shape memory alloys. Shape memory alloys (SMA's) generally refer to a group of metallic materials that demonstrate the ability to return to some previously defined shape or size when subjected to an appropriate thermal stimulus. Shape memory alloys are capable of undergoing phase transitions in which their elastic modulus, yield strength, and shape orientation are altered as a function of temperature. Generally, in the low temperature, or martensite phase, shape memory alloys can be plastically deformed and upon exposure to a specified higher temperature will transform to an austenite phase, or parent phase, attempting to return to their shape prior to the deformation. Materials that exhibit this shape memory effect only upon heating are referred to as having one-way shape memory. Those materials that also exhibit shape memory upon re-cooling are referred to as having two-way shape memory behavior.
- Shape memory alloys can exhibit a one-way shape memory effect, an intrinsic two-way effect, or an extrinsic two-way shape memory. Annealed shape memory alloys generally exhibit the one-way shape memory effect. Sufficient heating subsequent to low-temperature deformation of the shape memory material will induce the martensite to austenite type transition, and the material will recover the original, annealed shape. Hence, one-way shape memory effects are only observed upon heating.
- Intrinsic two-way shape memory alloys are characterized by a shape transition both upon heating from the martensite phase to the austenite phase, as well as an additional shape transition upon cooling from the austenite phase back to the martensite phase. In contrast, active connector elements that exhibit the extrinsic two-way shape memory effects are composite or multi-component materials that combine a shape memory alloy composition that exhibits a one-way effect with another element that provides a restoring force to return the first plate another position or to its original position. Active elements that exhibit an intrinsic one-way shape memory effect are fabricated from a shape memory alloy composition that will cause the active elements to automatically reform themselves as a result of the above noted phase transformations. Intrinsic two-way shape memory behavior must be induced in the shape memory material through thermo-mechanical processing. Such procedures include extreme deformation of the material while in the martensite phase, heating-cooling under constraint or load, or surface modification such as laser annealing, polishing, or shot-peening. Once the material has been trained to exhibit the two-way shape memory effect, the shape change between the low and high temperature states is generally reversible and persists through a high number of thermal cycles.
- The temperature at which the shape memory alloy remembers its high temperature form when heated can be adjusted by slight changes in the composition of the alloy and through heat treatment. In nickel-titanium shape memory alloys, for instance, it can be changed from above about 100° C. to below about −100° C. The shape recovery process occurs over a range ofjust a few degrees and the start or finish of the transformation can be controlled to within a few degrees depending on the alloy composition.
- Suitable shape memory alloy materials for fabricating the active elements include nickel-titanium based alloys, indium-titanium based alloys, nickel-aluminum based alloys, nickel-gallium based alloys, copper based alloys (e.g., copper-zinc alloys, copper-aluminum alloys, copper-gold, and copper-tin alloys), gold-cadmium based alloys, silver-cadmium based alloys, indium-cadmium based alloys, manganese-copper based alloys, iron-platinum based alloys, iron-palladium based alloys, or the like, or a combination comprising at least one of the foregoing shape memory alloys. The alloys can be binary, ternary, or any higher order so long as the alloy composition exhibits a shape memory effect, e.g., change in shape orientation, changes in yield strength, and/or flexural modulus properties, damping capacity, and the like.
- The thermal activation signal may be applied to the shape memory alloy in various ways. It is generally desirable for the thermal activation signal to promote a change in the temperature of the shape memory alloy to a temperature greater than or equal to its austenitic transition temperature. Suitable examples of such thermal activation signals that can promote a change in temperature are the use of steam, hot oil, resistive electrical heating, or the like, or a combination comprising at least one of the foregoing signals. A preferred thermal activation signal is one derived from resistive electrical heating.
- The
active element 20 may also be an electrically active polymer. Electrically active polymers are also commonly known as electroactive polymers (EAP's). The key design feature of devices based on these materials is the use of compliant electrodes that enable polymer films to expand or contract in the in-plane directions in response to applied electric fields or mechanical stresses. When electroactive polymers are used as theactive element 20, strains of greater than or equal to about 100%, pressures greater than or equal to about 50 kilograms/square centimeter (kg/cm2) can be developed in response to an applied voltage. The good electromechanical response of these materials, as well as other characteristics such as good environmental tolerance and long-term durability, make them suitable for use in active elements under a variety of manufacturing conditions. Electroactive polymers are suitable for use as an active element in manycustomizable strut assembly 10 configurations. - Electroactive polymer actuator elements used in
customizable strut assembly 10 may be selected based on one or more material properties such as a high electrical breakdown strength, a low modulus of elasticity-(for small deformations), a high dielectric constant, and the like. In one embodiment, a polymer is selected such that is has an elastic modulus at most about 100 MPa. In another embodiment, the polymer is selected such that is has a maximum actuation pressure between about 0.05 MPa and about 10 MPa, and preferably between about 0.3 MPa and about 3 MPa. In another embodiment, the polymer is selected such that is has a dielectric constant between about 2 and about 20, and preferably between about 2.5 and about 12. The present disclosure is not intended to be limited to these ranges. Ideally, materials with a higher dielectric constant than the ranges given above would be desirable if the materials had both a high dielectric constant and a high dielectric strength. In many cases, electroactive polymers may be fabricated and implemented as thin films. Thicknesses suitable for these thin films may be below 50 micrometers. - As electroactive polymers may deflect at high strains, electrodes attached to the polymers should also deflect without compromising mechanical or electrical performance. Generally, electrodes suitable for use may be of any shape and material provided that they are able to supply a suitable voltage to, or receive a suitable voltage from, an Electroactive polymer. The voltage may be either constant or varying over time. In one embodiment, the electrodes adhere to a surface of the polymer. Electrodes adhering to the polymer are preferably compliant and conform to the changing shape of the polymer. Correspondingly, the present disclosure may include compliant electrodes that conform to the shape of an electroactive polymer to which they are attached. The electrodes may be only applied to a portion of an electroactive polymer and define an active area according to their geometry. Various types of electrodes suitable for use with the present disclosure include structured electrodes comprising metal traces and charge distribution layers, textured electrodes comprising varying out of plane dimensions, conductive greases such as carbon greases or silver greases, colloidal suspensions, high aspect ratio conductive materials such as carbon fibrils and carbon nanotubes, and mixtures of ionically conductive materials.
- Materials used for electrodes may vary. Suitable materials used in an electrode may include graphite, carbon black, colloidal suspensions, thin metals including silver and gold, silver filled and carbon filled gels and polymers, and ionically or electronically conductive polymers. It is understood that certain electrode materials may work well with particular polymers and may not work as well for others. By way of example, carbon fibrils work well with acrylic elastomer polymers while not as well with silicone polymers.
- The electroactive polymers used herein are generally conjugated polymers. Suitable examples of electroactive polymers are poly(aniline), substituted poly(aniline)s, polycarbazoles, substituted polycarbazoles, polyindoles, poly(pyrrole)s, substituted poly(pyrrole)s, poly(thiophene)s, substituted poly(thiophene)s, poly(acetylene)s, poly(ethylene dioxythiophene)s, poly(ethylenedioxypyrrole)s, poly(p-phenylene vinylene)s, or the like, or combinations comprising at least one of the foregoing electroactive polymers. Blends or copolymers or composites of the foregoing electroactive polymers may also be used. Similarly blends or copolymers or composites of an electroactive polymers with an electroactive polymers precursor may also be used.
- The
actuator element 20 used in thecustomizable strut assembly 10 may also comprise a piezoelectric material. Also, in certain embodiments, the piezoelectric material may be configured for providing rapid deployment. As used herein, the term “piezoelectric” is used to describe a material that mechanically deforms (changes shape and/or size) when a voltage potential is applied, or conversely, generates an electrical charge when mechanically deformed. As piezoelectric actuators have a small output stroke, they are usually coupled with a transmission (e.g. a compliant mechanism) that serves to amplify the output stroke at the expense of a reduction in the output force. As an example, a piezoelectric material is disposed on strips of a flexible metal sheet. The piezo actuators are coupled to the sheet in a manner that causes bending or unbending of the sheet when the actuators are activated. The ability of the bending mode of deformation in a flexible shell to amplify small axial strains into larger rotary displacements is used to advantage. The strips can be unimorph or bimorph. Preferably, the strips are bimorph, because bimorphs generally exhibit more displacement than unimorphs. - In contrast to the unimorph piezoelectric device, a bimorph device includes an intermediate flexible metal foil sandwiched between two piezoelectric elements. Bimorphs exhibit more displacement than unimorphs because under the applied voltage one ceramic element will contract while the other expands. Bimorphs can exhibit strains up to about 20%, but similar to unimorphs, generally cannot sustain high loads relative to the overall dimensions of the unimorph structure.
- Suitable piezoelectric materials include inorganic compounds, organic compounds, and metals. With regard to organic materials, all of the polymeric materials with non-centrosymmetric structure and large dipole moment group(s) on the main chain or on the side-chain, or on both chains within the molecules, can be used as candidates for the piezoelectric film. Examples of suitable polymers include, for example, but are not limited to, poly(sodium 4-styrenesulfonate) (“PSS”), poly S-119 (poly(vinylamine) backbone azo chromophore), and their derivatives; polyfluorocarbons, including polyvinylidene fluoride (“PVDF”), its co-polymer vinylidene fluoride (“VDF”), trifluoroethylene (TrFE), and their derivatives; polychlorocarbons, including poly(vinyl chloride) (“PVC”), polyvinylidene chloride (“PVC2”), and their derivatives; polyacrylonitriles (“PAN”), and their derivatives; polycarboxylic acids, including poly(methacrylic acid (“PMA”), and their derivatives; polyureas, and their derivatives; polyurethanes (“PUE”), and their derivatives; bio-polymer molecules such as poly-L-lactic acids and their derivatives, and membrane proteins, as well as phosphate bio-molecules; polyanilines and their derivatives, and all of the derivatives of tetramines; polyimides, polyetherimides (“PEI”), and their derivatives; all of the membrane polymers; poly(N-vinyl pyrrolidone) (“PVP”) homopolymer, and its derivatives, and random PVP-co-vinyl acetate (“PVAc”) copolymers; and all of the aromatic polymers with dipole moment groups in the main-chain or side-chains, or in both the main-chain and the side-chains, and mixtures thereof.
- Further, piezoelectric materials can include Pt, Pd, Ni, Ti, Cr, Fe, Ag, Au, Cu, and metal alloys and mixtures thereof. These piezoelectric materials can also include, for example, metal oxide such as SiO2, Al2O3, ZrO2, TiO2, SrTiO3, PbTiO3, BaTiO3, FeO3, Fe3O4, ZnO, and mixtures thereof; and Group VIA and IIB compounds, such as CdSe, CdS, GaAs,
AgCaSe 2, ZnSe, GaP, InP, ZnS, and mixtures thereof. - The
active element 20 can also comprise magnetorheological (MRE) elastomers. Magnetorheological elastomers (MRE) are suspensions of micrometer-sized, magnetically polarizable particles in a polymeric elastomer. When a magnetorheological elastomer is exposed to a magnetic field, the normally randomly oriented particles form chains of particles in the direction of the magnetic field lines. The particle chains increase the effective stiffness of the elastomer. The change in the effective stiffness of the MRE is accomplished by changing the shear and compression/tension modulii of the magnetorheological elastomer by varying the strength of the applied magnetic field. The magnetorheological elastomers typically develop structure when exposed to a magnetic field in as little as a few milliseconds. Discontinuing the exposure of the magnetorheological elastomer to the magnetic field reverses the process and the elastomer returns to a lower viscosity state. - Suitable magnetorheological elastomer materials include an elastic polymer matrix comprising a suspension of ferromagnetic or paramagnetic particles, wherein the particles are described above. Suitable polymer matrices include poly-alpha-olefins, copolymers of poly-alpha-olefins and natural rubber.
- Suitable ferromagnetic or paramagnetic include iron; iron alloys, such as those including aluminum, silicon, cobalt, nickel, vanadium, molybdenum, chromium, tungsten, manganese and/or copper; iron oxides, including Fe2O3 and Fe3O4; iron nitride; iron carbide; carbonyl iron; nickel and alloys of nickel; cobalt and alloys of cobalt; chromium dioxide; stainless steel; silicon steel; or the like, or a combination comprising at least one of the foregoing particles. Examples of suitable iron particles include straight iron powders, reduced iron powders, iron oxide powder/straight iron powder mixtures and iron oxide powder/reduced iron powder mixtures. A preferred magnetic-responsive particulate is carbonyl iron, preferably, reduced carbonyl iron.
- The particle size should be selected so that the particles exhibit multi-domain characteristics when subjected to a magnetic field. Diameter sizes for the particles can be less than or equal to about 1,000 micrometers, with less than or equal to about 500 micrometers preferred, and less than or equal to about 100 micrometers more preferred. Also preferred is a particle diameter of greater than or equal to about 0.1 micrometer, with greater than or equal to about 0.5 more preferred, and greater than or equal to about 10 micrometer especially preferred. The particles are preferably present in an amount between about 5.0 and about 50 percent by volume of the total composition.
- With reference now again to the
FIG. 2 , in one embodiment, in one manner of operating thecustomizable strut assembly 10 in order to vary its stroke length, an external stimulus is applied to theactive element 20. A preferred external stimulus is one derived from thermal activation preferably one that is derived from resistive electrical heating. As described earlier, theactive element 20 can be a composite of SMP, an elastic material and one or more active material based actuators (e.g. SMA or EAP); or a composite of SMP and an elastic material; or a sub-assembly comprising one or more active material based actuators that are mechanically coupled to elastic restoring elements; etc. In each case, the overall axial dimension of the active element can be changed in response to the activation signal to achieve the desired strut stroke adjustment. This change in length facilitates the displacement of the suspendedbody 60 with respect to the supportingbody 50, thereby changing the effective stroke length of thecustomizable strut assembly 10. The magnitude of the change in length can be proportioned to the magnitude of the activation signal. -
FIGS. 3 and 4 depict exemplary embodiments of customizable strut assemblies that utilize active elements that are disposed inside thehousing 2. With reference now to theFIG. 3 , thecustomizable strut assembly 10 comprisesplates 22 that are in operative communication with theactive element 20. The plates are perforated to allow easy passage for the fluid. Theplates 22 and theactive element 20 are disposed within thehousing 2. Theactive element 20 for purposed of this embodiment is a coil spring, though it can be varied in shape and size in other configurations. Theplates 22 are disposed on opposing sides of thepiston head 14 and are in operative communication with thepiston head 14. The perforations in theplate 22 allow for a smooth displacement of thefluid 4 within thehousing 2 as thepiston 3 slides back and forth in thehousing 2. - In the prior art strut assembly (e.g., as shown in
FIG. 1 ), the ends of the strut stroke are marked by (near) contact between the flat ends of the piston head and the respective cylinder ends. In the adjustable strut assembly shown in theFIGS. 3 and 4 , the end of stroke is marked by contact between theelements 22 and the respective ends of the cylinder. Therefore, it is clear that by changing the axial length and/or the stiffness of theactive elements 20, the effective stroke of the strut can be adjusted. - In one embodiment, the
active element 20 can be a composite of a shape memory polymer, an elastic material and one or more active material based actuators (e.g., a shape memory alloy or and electroactive polymer); or a composite of shape memory polymer and an elastic material; or a sub-assembly comprising one or more active material based actuators that are mechanically coupled to elastic restoring elements; or the like. In each case, the overall axial dimension of the actuator can be changed in response to the activation signal to achieve the desired strut stroke adjustment. Depending on the active materials and the configuration in which they are used, the change in the stroke may stay in effect until it is changed again, or the change may be made just-in-time for an operation and will remain in effect only for that operation. In another embodiment, theactive element 20 comprises a spring made of a shape memory alloy in its martensitic-phase over the operating temperature range for the strut. - As noted above, the
actuator 16 generally comprises anactive element 20 that comprises an active material. An active material generally refers to a group of materials that demonstrate an ability to return to some previously defined shape or size when subjected to an appropriate external stimulus. The active material, upon activation facilitates the displacement of the suspendedbody 60 towards and/or away from the supportingbody 50 and also permits control over the magnitude of the displacement. - In another embodiment, the
actuator 16 can also comprise a composite of an active material. In one embodiment, the composite can comprise a shape memory alloy and a shape memory polymer. In another embodiment, the composite can comprise a shape memory alloy and a material that is not an active material, i.e., a material that does not return to some previously defined shape or size when subjected to an appropriate external stimulus. In yet another embodiment, the composite can comprise two or more active materials such as for example a shape memory alloy and a shape memory polymer in addition to and a material that is not an active material. - For example, an actuator can comprise a composite that comprises one or more elastic elements made from spring steel distributed within a shape memory polymer matrix together with one or more shape memory alloy elements. The shape memory polymer has a characteristic temperature known as its glass transition temperature (Tg), such that the elastic modulus of the material drops significantly e.g., a factor of about 30 to about 150 when it is heated above its Tg. The shape memory polymer is a soft and easily pliable polymer above the Tg, and it can be deformed significantly (up to 200% recoverable strain) by a relatively low force. On cooling the deformed shape memory polymer below its Tg, the material reverts back to its stiffer form, while retaining the deformed shape in a stress-free condition. If a specified limiting temperature is not exceeded during the heating process, the aforementioned procedure comprising heating, deforming and cooling can be repeated multiple times.
- The elastic elements in the above embodiment are mechanically coupled to the shape memory polymer matrix and, they determine the overall configuration (i.e. geometry, dimensions, etc) of the active element. The relative stiffnesses of the elastic elements and the shape memory polymer matrix are chosen such that, when the shape memory polymer is below the lower Tg, it is the dominant contributor to the overall stiffness of the actuator; whereas when the shape memory polymer is above the Tg, the elastic elements are the dominant contributors to the overall active element stiffness. Depending on the manner in which the shape memory elements are activated, they can either compress or elongate the elastic elements and thereby, control the overall configuration of the active element when the shape memory polymer is above the Tg.
- The use of the actuator can be illustrated by describing the process in which the actuator is reconfigured to tailor the strut-stroke. The shape memory polymer is softened by heating it to a temperature above its Tg. The shape memory alloy elements are then activated to change the overall configuration of the actuator while the shape memory polymer is soft. Once the actuator achieves the desired configuration (e.g. axial dimension), the shape memory polymer is allowed to cool down to a temperature below its Tg, whereupon it regains its stiff form. The shape memory alloy elements are then powered off. As described earlier, the stiffness of the shape memory polymer matrix dominates that of the elastic elements, and hence the active element will retain the above configuration until it is heated above its Tg. The above reconfiguration process can then be repeated.
- As the
piston 3 slides within thehousing 2, theactive elements 20 are compressed at one or both ends of the strut's stroke. If the stiffness of theseactive elements 20 is small, e.g., when the shape memory alloy is in its martensitic phase, they can be easily compressed between thepiston 3 and thehousing 2. Hence, they will not affect the length of the stroke. However, if the stiffness of the active elements is high, e.g., when the shape memory alloy is in its austenitic phase, they resist relative motion between thepiston 2 and thehousing 2 with considerable force at the extremities of the strut's stroke. The amount of change in the stroke length is directly proportional to the length of theactive element 20 and its stiffness. Thus a stiffening of theactive element 20 upon activation will result in a reduction of the effective stroke length for thecustomizable strut assembly 10. - In one embodiment, by activating the
active element 20, the length of theactive element 20 can be varied, thereby varying the length of travel of thepiston 3 in thehousing 2. This will alter the stroke length of thestrut assembly 10. The activation signal can be a thermal signal brought on by resistive heating of the spring. Depending on the range of stroke variation required, similar plates can also be connected to one or both ends of thehousing 2 throughactive elements 20, whose lengths and/or stiffnesses can be varied upon activation. - In addition to changing the stroke of the
strut assembly 10, varying the stiffness of the various active elements in the strut assembly can enable control over which part of the stroke is curtailed (e.g., the tailgate lift needs to be reduced for shorter owners; the tailgate may need to be held partially open when transporting over size cargo that extends partially out of the vehicle, in which case the tailgate closure needs to be restricted), and afford smoother operation of thecustomizable strut assembly 10. - When the
active element 20 in theFIG. 3 is a coil spring made from a shape memory alloy material, the customizable strut assembly can be modified to function in various modes. In one mode, when the spring is in its martensitic phase over the temperature range of operation of thecustomizable strut assembly 10, it has a low stiffness and hence a low spring constant than when it is in the austenitic form. Passage of an electric current through the spring can induce a martensitic to austenitic transition in the spring material, thereby increasing its stiffness e.g. three-fold. The dual-stiffness nature of the SMA spring can be used to vary the stroke of the strut as described above. Depending on the composition of the shape memory alloy material, the transition from soft to stiff can be sharp or gradual, thereby yielding greater control over the behavior of the strut at the extremities of its stroke. - In yet another embodiment, depicted in the
FIG. 4 , magnetorheological elastomers can be employed as theactive element 20. In this embodiment, thepiston 3 comprises anelectromagnet 26 that is in mechanical and electrical communication with the magnetorheological elastomer of theactive element 20. The magnetorheological elastomer is in the form of a block that is disposed on opposing surfaces of thepiston head 14. Theactive element 20 has a size effective to vary the length of the stroke as its stiffness is increased. When an electrical current is passed through theelectromagnet 26, a magnetic field is set up inside the magnetorheological elastomer. Since the stiffness of the magnetorheological elastomer can be varied by varying the strength of the magnetic field, the change in stiffness can be controlled by varying the electrical current passing through the electromagnet. By changing the stiffness of the magnetorheological elastomer, the length of the stroke can be varied in a manner that is conceptually similar to that described above in the context of SMA springs. As the elastomer becomes less stiff, it can be easily compressed between thepiston 3 and the inner surface of thehousing 2, thereby permitting a larger stroke length. As the electrical current is varied to increase the stiffness of the elastomer, it cannot be easily deformed between thepiston 3 and the inner surface of thehousing 2. Thus by varying the magnitude of the activation signal to theactive element 20, the length of travel of thecustomizable strut assembly 10 can be adjusted. The use of a biasing permanent magnet, whose influence on the MRE can be counteracted by an electromagnet allows this concept to be extended to both: increase and decrease the effective strut stroke. - In yet another exemplary embodiment, depicted in the
FIG. 5 , thestrut assembly 10 comprises asleeve 30 that is disposed upon the outer surface of thehousing 2. Thesleeve 30 is hollow and comprises abraking mechanism 32 that fixedly attaches it to thehousing 2 depending upon the user's preference. Thesleeve 30 can have any suitable cross-sectional geometry that permits slideable motion with thehousing 2, when thebraking mechanism 32 is released. The braking mechanism is generally released when it is desirable to change the effective length of thestrut assembly 10 after which it is reengaged to fixedly attach thesleeve 32 to thehousing 2. Thebraking mechanism 32 can be engaged or disengaged by a suitable stimulus to change the effective length of the strut assembly. Adjusting the position of thesleeve 32 controls the distance labeled DS2. - A
mechanical stop 34 is fixedly attached to thepiston rod 12 at the user's discretion and can be used to adjust the effective stroke length by displacing the mechanical stop when desired. The location of themechanical stop 34 determines the distance DS1 as shown in theFIG. 5 . Themechanical stop 34 can be adjusted upon temporary removal of thesleeve 30. When thebraking mechanism 32 is disengaged, thesleeve 30 can be freely positioned at any desirable point over the length of thehousing 2 subject to mechanical interference constraints imposed by the cylinder dimensions. When thebraking mechanism 32 is engaged and thesleeve 30 is mechanically coupled to thehousing 2, the effective-length of the strut assembly is controlled by the larger of the two distances, DS1 and DS2. - Once the position of the
mechanical stop 34 is fixed relative to thepiston rod 12, the motion of the suspendedbody 60 is governed by the smaller of the two distances DO1 and DO2 as shown in theFIG. 5 . These correspond to mechanical interference between thepiston 3 and the end of the cylinder proximate to the supportingbody 50, and between the end of the cylinder proximate to the supportingbody 50 and themechanical stop 34. Changing the position of themechanical stop 34 allows the length DO2 to be adjusted. This affords control over the motion of the suspendedbody 60 when it is to be opened completely. - In an alternative embodiment, the position of the
mechanical stop 34 can be adjusted using anoptional biasing spring 36 as depicted in theFIG. 5 . The bias spring can be of a length effective to keep the mechanical stop in communication with the end of thesleeve 30 proximate to the supportingbody 50. The spring force (i.e., the spring constant) is negligible compared to the braking resistance produced when themechanical stop 32 is engaged. Therefore, thespring 36 does not affect the position of themechanical stop 32, when the brake is engaged. In one embodiment, in one method of determining the fully open position of the suspendedbody 60, themechanical stop 34 is disengaged and thebraking mechanism 32 is engaged thereby permitting the swing panel to be displaced into the desired fully-open position. At this point themechanical stop 34 is engaged locking in the range of desired motion for thestrut assembly 10. Thesleeve 30 moves with the suspendedbody 60 during its motion and themechanical stop 34 moves with thespring 36 to its new location. - The desired fully-shut position can be set in a similar way. Here the
braking mechanism 32 is disengaged and the suspendedbody 60 is moved to the desired fully-shut position before thebraking mechanism 32 is engaged again. Thepiston rod 3 can be used to displace thesleeve 30 to the desired position. Again, a soft bias spring (not shown) can be used to keep thesleeve 30 flush against the end of the piston rod that is proximate to the supportingbody 50. - The ability to customize the length of travel of a
customizable strut assembly 10 can be advantageously used in automobiles, aircraft, ships, in machine tools, or the like, to improve usability. The length of travel can be adjusted at any time during the life cycle of an article that employs the customizable strut assembly. The length of travel can also be adjusted to accommodate ambient weather conditions, consumer anthropometrics or to offset the deleterious effects of component wear. The length of travel can be adjusted manually or by computer as desired. - While the disclosure has been described with reference to an exemplary embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the disclosure without departing from the essential scope thereof. Therefore, it is intended that the disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this disclosure, but that the disclosure will include all embodiments falling within the scope of the appended claims.
Claims (20)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/078,848 US20050263359A1 (en) | 2004-03-12 | 2005-03-11 | Customizable strut assemblies having variable stroke lengths and articles employing the same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US55279104P | 2004-03-12 | 2004-03-12 | |
US11/078,848 US20050263359A1 (en) | 2004-03-12 | 2005-03-11 | Customizable strut assemblies having variable stroke lengths and articles employing the same |
Publications (1)
Publication Number | Publication Date |
---|---|
US20050263359A1 true US20050263359A1 (en) | 2005-12-01 |
Family
ID=34994178
Family Applications (8)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/077,496 Expired - Fee Related US8261892B2 (en) | 2004-03-12 | 2005-03-10 | Customizable strut assemblies and articles that employ the same |
US11/077,179 Abandoned US20050205364A1 (en) | 2004-03-12 | 2005-03-10 | Variable resistance strut assemblies and articles containing the same |
US11/078,847 Abandoned US20050230195A1 (en) | 2004-03-12 | 2005-03-11 | Devices for holding intermediate positions and articles that contain the same |
US11/078,848 Abandoned US20050263359A1 (en) | 2004-03-12 | 2005-03-11 | Customizable strut assemblies having variable stroke lengths and articles employing the same |
US11/078,823 Expired - Fee Related US7478845B2 (en) | 2004-03-12 | 2005-03-11 | Active materials based approaches to latch snug down and articles containing the same |
US12/040,377 Abandoned US20080141736A1 (en) | 2004-03-12 | 2008-02-29 | Devices for holding intermediate positions and articles that contain the same |
US12/210,674 Abandoned US20090008844A1 (en) | 2004-03-12 | 2008-09-15 | Variable Resistance Strut Assemblies and Articles Containing the Same |
US12/788,831 Expired - Fee Related US8069963B2 (en) | 2004-03-12 | 2010-05-27 | Variable resistance strut assemblies and articles containing the same |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/077,496 Expired - Fee Related US8261892B2 (en) | 2004-03-12 | 2005-03-10 | Customizable strut assemblies and articles that employ the same |
US11/077,179 Abandoned US20050205364A1 (en) | 2004-03-12 | 2005-03-10 | Variable resistance strut assemblies and articles containing the same |
US11/078,847 Abandoned US20050230195A1 (en) | 2004-03-12 | 2005-03-11 | Devices for holding intermediate positions and articles that contain the same |
Family Applications After (4)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/078,823 Expired - Fee Related US7478845B2 (en) | 2004-03-12 | 2005-03-11 | Active materials based approaches to latch snug down and articles containing the same |
US12/040,377 Abandoned US20080141736A1 (en) | 2004-03-12 | 2008-02-29 | Devices for holding intermediate positions and articles that contain the same |
US12/210,674 Abandoned US20090008844A1 (en) | 2004-03-12 | 2008-09-15 | Variable Resistance Strut Assemblies and Articles Containing the Same |
US12/788,831 Expired - Fee Related US8069963B2 (en) | 2004-03-12 | 2010-05-27 | Variable resistance strut assemblies and articles containing the same |
Country Status (2)
Country | Link |
---|---|
US (8) | US8261892B2 (en) |
WO (2) | WO2005089168A2 (en) |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050199455A1 (en) * | 2004-03-12 | 2005-09-15 | Browne Alan L. | Customizable strut assemblies and articles that employ the same |
US20060056993A1 (en) * | 2004-09-14 | 2006-03-16 | Moshe Gombinsky | Magnetic spring actuator device |
US20070205853A1 (en) * | 2003-02-27 | 2007-09-06 | University Of Washington | Design of membrane actuator based on ferromagnetic shape memory alloy composite for sythentic jet actuator |
US20070289301A1 (en) * | 2003-02-27 | 2007-12-20 | University Of Washington | Torque actuator incorporating shape memory alloy composites |
US20080230330A1 (en) * | 2007-03-20 | 2008-09-25 | Siemens Aktiengesellschaft | Braking device having a wedge mechanism |
US20090038126A1 (en) * | 2007-08-08 | 2009-02-12 | Key Safety Systems, Inc. | Seat belt buckle |
US20090058130A1 (en) * | 2007-08-31 | 2009-03-05 | Gm Global Technology Operations, Inc. | Active material based concealment devices for seams |
US20090115284A1 (en) * | 2003-02-27 | 2009-05-07 | University Of Washington | Inchworm actuator based on shape memory alloy composite diaphragm |
US20090130391A1 (en) * | 2007-11-02 | 2009-05-21 | University Of Washington | Design of shape memory alloy fibers and shape memory polymer fibers and films and their composites for reversible shape changes |
WO2009089221A1 (en) * | 2008-01-07 | 2009-07-16 | Bio-Rad Laboratories, Inc. | Piston position detection for preparative chromatography column |
US20090278342A1 (en) * | 2008-05-06 | 2009-11-12 | Gm Global Technology Operations, Inc. | Vehicle roll bar apparatus with active material actuation |
US7648589B2 (en) | 2004-09-08 | 2010-01-19 | University Of Washington | Energy absorbent material |
US7688168B2 (en) | 2003-02-27 | 2010-03-30 | University Of Washington | Actuators based on ferromagnetic shape memory alloy composites |
US20100229610A1 (en) * | 2006-06-23 | 2010-09-16 | Cornerstone Research Group, Inc. | Locking Device Using Shape Memory Materials |
US20100314842A1 (en) * | 2009-06-16 | 2010-12-16 | Toyota Motor Engineering & Manufacturing North America, Inc. | Active Magneto-Rheological Spring Assemblies and Vehicle Suspension Systems Incorporating the Same |
US20120018962A1 (en) * | 2010-07-22 | 2012-01-26 | Gm Global Technology Operations, Inc. | Stiffness control using smart actuators |
US20140042756A1 (en) * | 2012-08-13 | 2014-02-13 | GM Global Technology Operations LLC | Latchable or lockable device |
US20140376837A1 (en) * | 2013-06-24 | 2014-12-25 | The Regents Of The University Of California | Semi-active insolators based on magnetorheological nanocomposites |
US20160152108A1 (en) * | 2013-07-24 | 2016-06-02 | Kyb Corporation | Shock absorber mounting device |
US9859834B2 (en) | 2016-02-05 | 2018-01-02 | GM Global Technology Operations LLC | Slack compensator |
US10208823B2 (en) * | 2017-01-10 | 2019-02-19 | Toyota Motor Engineering & Manufacturing North America, Inc. | Variable rate bound stoppers and variable rate suspension systems containing variable rate bound stoppers |
US10597917B2 (en) | 2017-10-09 | 2020-03-24 | GM Global Technology Operations LLC | Stretchable adjustable-stiffness assemblies |
US10604201B2 (en) | 2018-03-29 | 2020-03-31 | Shimano Inc. | Telescopic apparatus |
Families Citing this family (90)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7413063B1 (en) * | 2003-02-24 | 2008-08-19 | Davis Family Irrevocable Trust | Compressible fluid magnetorheological suspension strut |
US20050077691A1 (en) * | 2003-10-14 | 2005-04-14 | Witters Allen L. | Suspension structure with internal height sensor assembly |
US7556117B2 (en) * | 2004-06-09 | 2009-07-07 | Gm Global Technology Operations, Inc. | Hood lift mechanisms utilizing active materials and methods of use |
CN101170966A (en) * | 2005-04-01 | 2008-04-30 | 科罗拉多州立大学董事会 | A graft fixation device and method |
ITBO20060090A1 (en) * | 2006-02-10 | 2007-08-11 | Ferrari Spa | SEAT FOR A SPORTS VEHICLE WITH LATERAL CONTAINMENT. |
CN101466714B (en) * | 2006-06-23 | 2013-02-06 | 英赛特股份有限公司 | Purinone derivatives as HM74A agonists |
US20080042368A1 (en) * | 2006-08-07 | 2008-02-21 | Gm Global Technology Operations, Inc. | Piston ring assembly including a self accommodating smart piston ring |
US7677639B2 (en) * | 2007-02-23 | 2010-03-16 | Gm Global Technology Operations, Inc. | Active material based closure hinge and alignment process |
US20080217927A1 (en) * | 2007-03-07 | 2008-09-11 | Gm Global Technology Operations, Inc. | Cable systems having at least one section formed of an active material |
US8110050B2 (en) * | 2007-05-16 | 2012-02-07 | Thyssenkrupp Elevator Capital Corporation | Actively damped tension member |
US8104823B2 (en) * | 2007-06-15 | 2012-01-31 | Ford Global Technologies | Automotive door with hydraulically locking repositionable immobilizer |
AT504333B8 (en) * | 2007-06-19 | 2008-09-15 | Evva Werke | DEVICE FOR LOCKING A LOCK |
US10153121B2 (en) * | 2007-11-30 | 2018-12-11 | Hubbell Incorporated | GFCI with miswire protection having unitary receptacle and load conductors after proper installation |
US20090278363A1 (en) * | 2008-05-08 | 2009-11-12 | Gm Global Technology Operations, Inc. | Active Materials Based Impact Management Systems |
US20100170760A1 (en) | 2009-01-07 | 2010-07-08 | John Marking | Remotely Operated Bypass for a Suspension Damper |
US11306798B2 (en) | 2008-05-09 | 2022-04-19 | Fox Factory, Inc. | Position sensitive suspension damping with an active valve |
US8627932B2 (en) | 2009-01-07 | 2014-01-14 | Fox Factory, Inc. | Bypass for a suspension damper |
US9033122B2 (en) | 2009-01-07 | 2015-05-19 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US10060499B2 (en) | 2009-01-07 | 2018-08-28 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US9452654B2 (en) | 2009-01-07 | 2016-09-27 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US10047817B2 (en) | 2009-01-07 | 2018-08-14 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US8857580B2 (en) | 2009-01-07 | 2014-10-14 | Fox Factory, Inc. | Remotely operated bypass for a suspension damper |
US8430933B2 (en) * | 2008-07-24 | 2013-04-30 | MedShape Inc. | Method and apparatus for deploying a shape memory polymer |
US8069858B2 (en) * | 2008-07-24 | 2011-12-06 | Medshape Solutions, Inc. | Method and apparatus for deploying a shape memory polymer |
US20100170521A1 (en) * | 2008-07-24 | 2010-07-08 | Medshape Solutions, Inc. | Method and apparatus for deploying a shape memory polymer |
US8393446B2 (en) | 2008-08-25 | 2013-03-12 | David M Haugen | Methods and apparatus for suspension lock out and signal generation |
US9004242B2 (en) * | 2008-09-09 | 2015-04-14 | Darel E. Hodgson | Apparatus for absorbing shocks |
US8540297B2 (en) * | 2008-09-15 | 2013-09-24 | GM Global Technology Operations LLC | Manipulating center console components utilizing active material actuation |
US9022682B2 (en) * | 2008-10-13 | 2015-05-05 | GM Global Technology Operations LLC | Active material wire actuators having reinforced structural connectors |
US9422018B2 (en) | 2008-11-25 | 2016-08-23 | Fox Factory, Inc. | Seat post |
US10036443B2 (en) | 2009-03-19 | 2018-07-31 | Fox Factory, Inc. | Methods and apparatus for suspension adjustment |
US9140325B2 (en) | 2009-03-19 | 2015-09-22 | Fox Factory, Inc. | Methods and apparatus for selective spring pre-load adjustment |
US8301272B2 (en) * | 2008-12-03 | 2012-10-30 | GM Global Technology Operations LLC | Active materials-based compliant mechanisms |
US10821795B2 (en) | 2009-01-07 | 2020-11-03 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US9038791B2 (en) | 2009-01-07 | 2015-05-26 | Fox Factory, Inc. | Compression isolator for a suspension damper |
US11299233B2 (en) | 2009-01-07 | 2022-04-12 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
US12122205B2 (en) | 2009-01-07 | 2024-10-22 | Fox Factory, Inc. | Active valve for an internal bypass |
US8936139B2 (en) | 2009-03-19 | 2015-01-20 | Fox Factory, Inc. | Methods and apparatus for suspension adjustment |
US9074612B2 (en) * | 2009-04-27 | 2015-07-07 | Norgren Gmbh | Fluid operated actuator including a bleed port |
US8176958B2 (en) * | 2009-06-16 | 2012-05-15 | Toyota Motor Engineering & Manufacturing North America, Inc. | Magneto-rheological elastomer wheel assemblies with dynamic tire pressure control |
US8955653B2 (en) | 2009-10-13 | 2015-02-17 | Fox Factory, Incorporated | Methods and apparatus for controlling a fluid damper |
US8672106B2 (en) | 2009-10-13 | 2014-03-18 | Fox Factory, Inc. | Self-regulating suspension |
US8683798B2 (en) * | 2010-01-15 | 2014-04-01 | Syracuse University | Stimuli-responsive product |
US10697514B2 (en) | 2010-01-20 | 2020-06-30 | Fox Factory, Inc. | Remotely operated bypass for a suspension damper |
EP2402239B1 (en) | 2010-07-02 | 2020-09-02 | Fox Factory, Inc. | Adjustable seat post |
US8815145B2 (en) | 2010-11-11 | 2014-08-26 | Spirit Aerosystems, Inc. | Methods and systems for fabricating composite stiffeners with a rigid/malleable SMP apparatus |
US8951375B2 (en) | 2010-11-11 | 2015-02-10 | Spirit Aerosystems, Inc. | Methods and systems for co-bonding or co-curing composite parts using a rigid/malleable SMP apparatus |
US8734703B2 (en) | 2010-11-11 | 2014-05-27 | Spirit Aerosystems, Inc. | Methods and systems for fabricating composite parts using a SMP apparatus as a rigid lay-up tool and bladder |
US8974217B2 (en) | 2010-11-11 | 2015-03-10 | Spirit Aerosystems, Inc. | Reconfigurable shape memory polymer tooling supports |
US9427493B2 (en) | 2011-03-07 | 2016-08-30 | The Regents Of The University Of Colorado | Shape memory polymer intraocular lenses |
DE102011001900B4 (en) * | 2011-04-08 | 2015-01-22 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Hydraulic damper with compensation of the viscosity reduction with temperature increase |
EP3636953B1 (en) | 2011-05-31 | 2023-09-27 | Fox Factory, Inc. | Apparatus for position sensitive and/or adjustable suspension damping |
US9003956B2 (en) * | 2011-06-21 | 2015-04-14 | Honda Motor Co., Ltd. | Fluid cylinder mechanism |
US8689771B2 (en) * | 2011-06-30 | 2014-04-08 | GM Global Technology Operations LLC | Shape memory alloy-based device for controlling or monitoring pressure in a system |
US8522930B1 (en) * | 2011-08-08 | 2013-09-03 | Lockheed Martin Corporation | Clamping assembly employing a shape memory alloy actuating apparatus |
EP3929459A1 (en) | 2011-09-12 | 2021-12-29 | Fox Factory, Inc. | Methods and apparatus for suspension set up |
US11279199B2 (en) | 2012-01-25 | 2022-03-22 | Fox Factory, Inc. | Suspension damper with by-pass valves |
US8819912B2 (en) * | 2012-03-08 | 2014-09-02 | GM Global Technology Operations LLC | Method of assembling workpieces utilizing shape memory polymer activation to facilitate alignment and retention |
JP6006965B2 (en) * | 2012-04-13 | 2016-10-12 | 本田技研工業株式会社 | Power transmission device |
US10330171B2 (en) | 2012-05-10 | 2019-06-25 | Fox Factory, Inc. | Method and apparatus for an adjustable damper |
KR101338137B1 (en) * | 2012-07-05 | 2013-12-06 | 한국과학기술연구원 | Actuator using shape memory alloy |
WO2014009965A1 (en) * | 2012-07-09 | 2014-01-16 | Amrish Chopra | Fail-safe actuating system |
US9140243B2 (en) | 2012-11-12 | 2015-09-22 | Toyota Motor Engineering & Manufacturing North America, Inc. | Shape memory alloy latch with stable on-off position |
CN102926324B (en) * | 2012-11-23 | 2014-08-27 | 杨丽茹 | Multifunctional rigidity adjustable speed locking force transmission devices |
DE112014003306T5 (en) * | 2013-07-17 | 2016-05-12 | Magna Closures Inc. | Double motor unit with application in force-tightening and lock mechanism |
CN104612042B (en) * | 2013-12-05 | 2018-06-26 | 深圳市市政设计研究院有限公司 | A kind of anticollision attachment device for bridge |
US10315767B2 (en) * | 2014-04-02 | 2019-06-11 | B/E Aerospace, Inc. | Vacuum powered actuation mechanism for a vertically stowable aircraft storage unit |
US9435360B2 (en) * | 2014-04-02 | 2016-09-06 | B/E Aerospace, Inc. | Vacuum powered lifting mechanism |
US9422745B2 (en) * | 2014-05-09 | 2016-08-23 | Leslie Ho Leung Chow | Safe with nitinol wire locking mechanism |
DE102014216949A1 (en) * | 2014-08-26 | 2016-03-03 | Continental Teves Ag & Co. Ohg | steamers |
US10323443B2 (en) * | 2015-04-20 | 2019-06-18 | GM Global Technolgy Operations LLC. | Closure system for a vehicle |
CN104895982A (en) * | 2015-06-18 | 2015-09-09 | 无锡众扬金属制品有限公司 | Hydraulic spring |
DE102015119505B4 (en) * | 2015-07-21 | 2022-12-08 | Inventus Engineering Gmbh | Door component with a controllable damper device |
CN105346489B (en) * | 2015-12-14 | 2017-08-01 | 吉林大学 | A kind of marmem automobile intelligent endergonic structure and its control method |
US10737546B2 (en) | 2016-04-08 | 2020-08-11 | Fox Factory, Inc. | Electronic compression and rebound control |
DE102016212654A1 (en) * | 2016-07-12 | 2018-01-18 | Stabilus Gmbh | A rail brake damper |
US10801593B2 (en) | 2017-04-26 | 2020-10-13 | Paratech, Incorporated | Strut extender mechanism |
DE102017120131A1 (en) | 2017-09-01 | 2019-03-07 | Bürkert Werke GmbH & Co. KG | Foil converter and valve |
US20190157012A1 (en) * | 2017-11-03 | 2019-05-23 | Battelle Memorial Institute | Compositions and methods for polarization-switched, solid-state molecular pumping |
JP7019476B2 (en) * | 2018-03-26 | 2022-02-15 | 日立Astemo株式会社 | Damper device |
CN109404477A (en) * | 2018-11-21 | 2019-03-01 | 沈阳建筑大学 | A kind of SMA spring-STF viscous damper |
US11434972B2 (en) * | 2019-02-20 | 2022-09-06 | The Boeing Company | Passive lockable strut |
US11098463B2 (en) * | 2019-11-11 | 2021-08-24 | Caterpillar Inc. | Electrically activated polymer based locking system for earth moving equipment and method |
CN111207175B (en) * | 2020-03-13 | 2021-07-16 | 义乌市丹航科技有限公司 | Oil-gas damper for undercarriage |
US11725421B1 (en) * | 2021-04-07 | 2023-08-15 | Norshield Security Products, LLC | Attack, ballistic and blast resistant self-locking door |
GB2606525B (en) * | 2021-05-10 | 2024-06-26 | Safran Landing Systems Uk Ltd | Mechanically locking actuator |
CN113639004B (en) * | 2021-08-24 | 2022-05-27 | 上海大学 | Squeeze-mode giant electrorheological fluid damper |
US11624376B2 (en) | 2021-09-14 | 2023-04-11 | Toyota Motor Engineering & Manufacturing North America, Inc. | Hybrid actuation devices with electrostatic clutches |
US11592037B1 (en) | 2021-12-08 | 2023-02-28 | Toyota Motor Engineering & Manufacturing North America, Inc. | Hybrid actuation devices including alignment aids |
US12064156B2 (en) | 2023-01-09 | 2024-08-20 | John F. Krumme | Dynamic compression fixation devices |
Citations (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2811136A (en) * | 1955-10-27 | 1957-10-29 | Cleveland Pneumatic Tool Co | Lock mechanism for fluid motors |
US2856200A (en) * | 1956-03-19 | 1958-10-14 | Dominic M Conflitti | Vehicle shock absorber brake dive arrester |
US2973969A (en) * | 1955-05-11 | 1961-03-07 | Earle S Thall | Electrical shock absorbing system |
US3695144A (en) * | 1969-08-07 | 1972-10-03 | Charmilles Sa Ateliers | Servo feed system for machine tool provided with locking mechanism |
US4351515A (en) * | 1979-07-02 | 1982-09-28 | Toyota Jidosha Kogyo Kabushiki Kaisha | Feedback control type shock absorbing suspension system |
US4655629A (en) * | 1985-02-19 | 1987-04-07 | Westinghouse Electric Corp. | Flexural pivot device and method for assembling same |
US4773680A (en) * | 1984-09-04 | 1988-09-27 | Beta Phase, Inc. | Pipe couplers |
US4828237A (en) * | 1988-03-01 | 1989-05-09 | Trw Inc. | Reduced length MacPherson strut |
US5018606A (en) * | 1990-01-10 | 1991-05-28 | Lord Corporation | Electrophoretic fluid damper |
US5070697A (en) * | 1988-04-12 | 1991-12-10 | Koni | Actuator with memory metal and a shock absorber provided with this actuator |
US5095595A (en) * | 1990-05-16 | 1992-03-17 | Contraves Italiana | Actuator for restraint/release (r/r) devices, particularly for space applications |
US5277281A (en) * | 1992-06-18 | 1994-01-11 | Lord Corporation | Magnetorheological fluid dampers |
US5315565A (en) * | 1989-11-09 | 1994-05-24 | Brosow Joergen | Resonance oscillator |
US5396769A (en) * | 1993-10-12 | 1995-03-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Rotary actuator |
US5398916A (en) * | 1992-08-29 | 1995-03-21 | Mercedes-Benz Ag | Shape-memory metallic alloy damping body |
US5468042A (en) * | 1992-07-22 | 1995-11-21 | Stabilus Gmbh | Compartment confining construction with an opening, a closure unit for the opening and a positioning unit for the closure unit |
US5492312A (en) * | 1995-04-17 | 1996-02-20 | Lord Corporation | Multi-degree of freedom magnetorheological devices and system for using same |
US5592780A (en) * | 1995-06-07 | 1997-01-14 | Checkovich; Peter | Door position controlling apparatus |
US5657969A (en) * | 1994-12-29 | 1997-08-19 | Illinois Tool Works Inc. | Snap-in push-push latch mechanism |
US5687958A (en) * | 1991-08-28 | 1997-11-18 | Mercedes-Benz Ag | Metallic damping body |
US5727391A (en) * | 1995-10-16 | 1998-03-17 | Mcgill University | Deformable structural arrangement |
US5741007A (en) * | 1995-06-19 | 1998-04-21 | Illinois Tool Works Inc. | Damper rotational latch |
US5839719A (en) * | 1995-12-21 | 1998-11-24 | Stabilus Gmbh | Pneumatic strut for a motor vehicle with an adjustable limit position |
US5967268A (en) * | 1997-03-17 | 1999-10-19 | Tenneco Automotive Inc. | Temperature responsive damper |
US6008992A (en) * | 1998-02-05 | 1999-12-28 | Nec Corporation | Locking device |
US6126371A (en) * | 1999-04-05 | 2000-10-03 | Lockheed Martin Corporation | Shape memory metal alloy preload attenuation device |
US6138596A (en) * | 1999-09-22 | 2000-10-31 | Brunswick Corporation | Damped steering mechanism for a watercraft |
US6371463B1 (en) * | 2000-04-21 | 2002-04-16 | Dpd, Inc. | Constant-force pseudoelastic springs and applications thereof |
US6382602B1 (en) * | 2001-01-16 | 2002-05-07 | Joe Morrow | Apparatus for retrofitting height and load adjustable air spring to coil spring based Mac Pherson strut |
US6384518B1 (en) * | 2000-09-18 | 2002-05-07 | Jean A. Van Poppel | Piezoelectric coupler for variably coupling two bodies and joint incorporating the coupler |
US20020074742A1 (en) * | 2000-12-20 | 2002-06-20 | Quoiani Roberto L. | Metallic seal components |
US6427813B1 (en) * | 1997-08-04 | 2002-08-06 | Lord Corporation | Magnetorheological fluid devices exhibiting settling stability |
US6491291B1 (en) * | 2000-05-08 | 2002-12-10 | Meritor Light Vehicle Systems, Inc. | Suspension characteristic control using shape memory alloy materials |
US20020185347A1 (en) * | 1997-04-26 | 2002-12-12 | Andreas Pohl | Spring/mass vibratory force coupler |
US6508437B1 (en) * | 2002-01-15 | 2003-01-21 | Honeywell International Inc. | Launch lock for spacecraft payloads |
US6615449B1 (en) * | 2002-02-06 | 2003-09-09 | Arthur Alvarez | Releasable locking assembly for a door control cylinder |
US6715591B2 (en) * | 2002-01-08 | 2004-04-06 | Honeywell International Inc. | Spacecraft isolator launch restraint |
US20040194970A1 (en) * | 2003-04-07 | 2004-10-07 | Eatwell William Donald | Expandable seal member with shape memory alloy |
US20040231933A1 (en) * | 2003-03-24 | 2004-11-25 | Buchele Paul D. | Remotely releasable support strut |
US6832539B2 (en) * | 2002-07-15 | 2004-12-21 | Delaware Capital Formation, Inc. | Cylinder lock |
US6848727B1 (en) * | 1999-02-18 | 2005-02-01 | Atoma International Corp | Power door latch assembly |
US6871519B2 (en) * | 2001-03-27 | 2005-03-29 | C.R.F. Societa Consortile Per Azioni | Lock for doors |
US20050072579A1 (en) * | 2003-10-03 | 2005-04-07 | Philippe Gambier | Well packer having an energized sealing element and associated method |
US6886837B2 (en) * | 2000-03-30 | 2005-05-03 | Gibbs Technologies Limited | Hydraulic suspension strut for an amphibious vehicle |
US20050199455A1 (en) * | 2004-03-12 | 2005-09-15 | Browne Alan L. | Customizable strut assemblies and articles that employ the same |
US20050206095A1 (en) * | 2004-03-12 | 2005-09-22 | Keefe Andrew C | Discrete active seal assemblies |
US7029044B2 (en) * | 2003-11-18 | 2006-04-18 | General Motors Corporation | Tunable, healable vehicle impact devices |
US7111359B1 (en) * | 2003-02-03 | 2006-09-26 | Valentin Luca | Rod gripper |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4027479A (en) * | 1976-05-06 | 1977-06-07 | Cory John S | Variable density heat engine |
FR2594510B1 (en) * | 1986-02-18 | 1988-06-24 | Bourcier Carbon Christian | HYDRAULIC SHOCK ABSORBER WITH CONTROLLED DAMPING |
JPS6350678A (en) | 1986-08-14 | 1988-03-03 | Sumitomo Electric Ind Ltd | Shape memory alloy cylinder |
FR2607890B1 (en) * | 1986-12-09 | 1989-04-21 | Renault | SHOCK ABSORBER COMPRISING SHAPE MEMORY MATERIALS |
NL8800945A (en) * | 1988-04-12 | 1989-11-01 | Koni Bv | SHOCK ABSORBER. |
DE68917370T2 (en) * | 1988-05-13 | 1995-03-30 | Toa Nenryo Kogyo Kk | Damping device for a rotating shaft. |
JPH01288646A (en) * | 1988-05-13 | 1989-11-20 | Fuji Rubber Co Ltd | Shock absorber using shape memory alloy |
JPH034047A (en) * | 1989-05-31 | 1991-01-10 | Tonen Corp | Suspension device for vehicle |
NL193462C (en) * | 1993-03-10 | 1999-11-02 | Petrus Antonius Besselink | Door closer with locking device and temperature-sensitive release mechanism. |
JPH10318429A (en) * | 1997-05-20 | 1998-12-04 | Denso Corp | Flow control valve |
US6175989B1 (en) * | 1998-05-26 | 2001-01-23 | Lockheed Corp | Shape memory alloy controllable hinge apparatus |
US6666483B2 (en) * | 2000-01-14 | 2003-12-23 | Atoma International Corp | Hood latch with self-retracting secondary latch release arm |
DE10100010B4 (en) * | 2001-01-02 | 2005-05-12 | Brose Schließsysteme GmbH & Co.KG | Motor vehicle door lock, designed as an electric lock, and method for assembling a motor vehicle door lock designed as an electric lock |
US6374608B1 (en) * | 2001-03-06 | 2002-04-23 | Charles James Corris | Shape memory alloy wire actuator |
US6772479B2 (en) * | 2001-06-21 | 2004-08-10 | The Aerospace Corporation | Conductive shape memory metal deployment latch hinge |
WO2004001170A1 (en) | 2002-06-24 | 2003-12-31 | Intier Automotive Closures Inc. | Door control system for stepless holding of vehicle doors by means of a field force |
US7958979B2 (en) * | 2007-01-05 | 2011-06-14 | Honda Motor Co., Ltd. | Variable damper |
-
2005
- 2005-03-10 US US11/077,496 patent/US8261892B2/en not_active Expired - Fee Related
- 2005-03-10 WO PCT/US2005/007787 patent/WO2005089168A2/en active Application Filing
- 2005-03-10 WO PCT/US2005/007995 patent/WO2005089188A2/en active Application Filing
- 2005-03-10 US US11/077,179 patent/US20050205364A1/en not_active Abandoned
- 2005-03-11 US US11/078,847 patent/US20050230195A1/en not_active Abandoned
- 2005-03-11 US US11/078,848 patent/US20050263359A1/en not_active Abandoned
- 2005-03-11 US US11/078,823 patent/US7478845B2/en not_active Expired - Fee Related
-
2008
- 2008-02-29 US US12/040,377 patent/US20080141736A1/en not_active Abandoned
- 2008-09-15 US US12/210,674 patent/US20090008844A1/en not_active Abandoned
-
2010
- 2010-05-27 US US12/788,831 patent/US8069963B2/en not_active Expired - Fee Related
Patent Citations (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2973969A (en) * | 1955-05-11 | 1961-03-07 | Earle S Thall | Electrical shock absorbing system |
US2811136A (en) * | 1955-10-27 | 1957-10-29 | Cleveland Pneumatic Tool Co | Lock mechanism for fluid motors |
US2856200A (en) * | 1956-03-19 | 1958-10-14 | Dominic M Conflitti | Vehicle shock absorber brake dive arrester |
US3695144A (en) * | 1969-08-07 | 1972-10-03 | Charmilles Sa Ateliers | Servo feed system for machine tool provided with locking mechanism |
US4351515A (en) * | 1979-07-02 | 1982-09-28 | Toyota Jidosha Kogyo Kabushiki Kaisha | Feedback control type shock absorbing suspension system |
US4773680A (en) * | 1984-09-04 | 1988-09-27 | Beta Phase, Inc. | Pipe couplers |
US4655629A (en) * | 1985-02-19 | 1987-04-07 | Westinghouse Electric Corp. | Flexural pivot device and method for assembling same |
US4828237A (en) * | 1988-03-01 | 1989-05-09 | Trw Inc. | Reduced length MacPherson strut |
US5070697A (en) * | 1988-04-12 | 1991-12-10 | Koni | Actuator with memory metal and a shock absorber provided with this actuator |
US5315565A (en) * | 1989-11-09 | 1994-05-24 | Brosow Joergen | Resonance oscillator |
US5018606A (en) * | 1990-01-10 | 1991-05-28 | Lord Corporation | Electrophoretic fluid damper |
US5095595A (en) * | 1990-05-16 | 1992-03-17 | Contraves Italiana | Actuator for restraint/release (r/r) devices, particularly for space applications |
US5687958A (en) * | 1991-08-28 | 1997-11-18 | Mercedes-Benz Ag | Metallic damping body |
US5277281A (en) * | 1992-06-18 | 1994-01-11 | Lord Corporation | Magnetorheological fluid dampers |
US5468042A (en) * | 1992-07-22 | 1995-11-21 | Stabilus Gmbh | Compartment confining construction with an opening, a closure unit for the opening and a positioning unit for the closure unit |
US5398916A (en) * | 1992-08-29 | 1995-03-21 | Mercedes-Benz Ag | Shape-memory metallic alloy damping body |
US5396769A (en) * | 1993-10-12 | 1995-03-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Rotary actuator |
US5657969A (en) * | 1994-12-29 | 1997-08-19 | Illinois Tool Works Inc. | Snap-in push-push latch mechanism |
US5492312A (en) * | 1995-04-17 | 1996-02-20 | Lord Corporation | Multi-degree of freedom magnetorheological devices and system for using same |
US5592780A (en) * | 1995-06-07 | 1997-01-14 | Checkovich; Peter | Door position controlling apparatus |
US5741007A (en) * | 1995-06-19 | 1998-04-21 | Illinois Tool Works Inc. | Damper rotational latch |
US5727391A (en) * | 1995-10-16 | 1998-03-17 | Mcgill University | Deformable structural arrangement |
US5839719A (en) * | 1995-12-21 | 1998-11-24 | Stabilus Gmbh | Pneumatic strut for a motor vehicle with an adjustable limit position |
US5967268A (en) * | 1997-03-17 | 1999-10-19 | Tenneco Automotive Inc. | Temperature responsive damper |
US20020185347A1 (en) * | 1997-04-26 | 2002-12-12 | Andreas Pohl | Spring/mass vibratory force coupler |
US6427813B1 (en) * | 1997-08-04 | 2002-08-06 | Lord Corporation | Magnetorheological fluid devices exhibiting settling stability |
US6008992A (en) * | 1998-02-05 | 1999-12-28 | Nec Corporation | Locking device |
US6848727B1 (en) * | 1999-02-18 | 2005-02-01 | Atoma International Corp | Power door latch assembly |
US6126371A (en) * | 1999-04-05 | 2000-10-03 | Lockheed Martin Corporation | Shape memory metal alloy preload attenuation device |
US6138596A (en) * | 1999-09-22 | 2000-10-31 | Brunswick Corporation | Damped steering mechanism for a watercraft |
US6886837B2 (en) * | 2000-03-30 | 2005-05-03 | Gibbs Technologies Limited | Hydraulic suspension strut for an amphibious vehicle |
US6371463B1 (en) * | 2000-04-21 | 2002-04-16 | Dpd, Inc. | Constant-force pseudoelastic springs and applications thereof |
US6491291B1 (en) * | 2000-05-08 | 2002-12-10 | Meritor Light Vehicle Systems, Inc. | Suspension characteristic control using shape memory alloy materials |
US6384518B1 (en) * | 2000-09-18 | 2002-05-07 | Jean A. Van Poppel | Piezoelectric coupler for variably coupling two bodies and joint incorporating the coupler |
US20020074742A1 (en) * | 2000-12-20 | 2002-06-20 | Quoiani Roberto L. | Metallic seal components |
US6382602B1 (en) * | 2001-01-16 | 2002-05-07 | Joe Morrow | Apparatus for retrofitting height and load adjustable air spring to coil spring based Mac Pherson strut |
US6871519B2 (en) * | 2001-03-27 | 2005-03-29 | C.R.F. Societa Consortile Per Azioni | Lock for doors |
US6715591B2 (en) * | 2002-01-08 | 2004-04-06 | Honeywell International Inc. | Spacecraft isolator launch restraint |
US6508437B1 (en) * | 2002-01-15 | 2003-01-21 | Honeywell International Inc. | Launch lock for spacecraft payloads |
US6615449B1 (en) * | 2002-02-06 | 2003-09-09 | Arthur Alvarez | Releasable locking assembly for a door control cylinder |
US6832539B2 (en) * | 2002-07-15 | 2004-12-21 | Delaware Capital Formation, Inc. | Cylinder lock |
US7111359B1 (en) * | 2003-02-03 | 2006-09-26 | Valentin Luca | Rod gripper |
US20040231933A1 (en) * | 2003-03-24 | 2004-11-25 | Buchele Paul D. | Remotely releasable support strut |
US6920966B2 (en) * | 2003-03-24 | 2005-07-26 | Honeywell International Inc. | Remotely releasable support strut |
US20040194970A1 (en) * | 2003-04-07 | 2004-10-07 | Eatwell William Donald | Expandable seal member with shape memory alloy |
US20050072579A1 (en) * | 2003-10-03 | 2005-04-07 | Philippe Gambier | Well packer having an energized sealing element and associated method |
US7029044B2 (en) * | 2003-11-18 | 2006-04-18 | General Motors Corporation | Tunable, healable vehicle impact devices |
US20050199455A1 (en) * | 2004-03-12 | 2005-09-15 | Browne Alan L. | Customizable strut assemblies and articles that employ the same |
US20050206095A1 (en) * | 2004-03-12 | 2005-09-22 | Keefe Andrew C | Discrete active seal assemblies |
US20050205364A1 (en) * | 2004-03-12 | 2005-09-22 | Browne Alan L | Variable resistance strut assemblies and articles containing the same |
US20050206175A1 (en) * | 2004-03-12 | 2005-09-22 | Browne Alan L | Active materials based approaches to latch snug down and articles containing the same |
US20050230195A1 (en) * | 2004-03-12 | 2005-10-20 | Jones Gary L | Devices for holding intermediate positions and articles that contain the same |
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090115284A1 (en) * | 2003-02-27 | 2009-05-07 | University Of Washington | Inchworm actuator based on shape memory alloy composite diaphragm |
US8072302B2 (en) | 2003-02-27 | 2011-12-06 | University Of Washington Through Its Center For Commercialization | Inchworm actuator based on shape memory alloy composite diaphragm |
US7810326B2 (en) | 2003-02-27 | 2010-10-12 | University Of Washington Through Its Center For Commercialization | Torque actuator incorporating shape memory alloy composites |
US7688168B2 (en) | 2003-02-27 | 2010-03-30 | University Of Washington | Actuators based on ferromagnetic shape memory alloy composites |
US20070205853A1 (en) * | 2003-02-27 | 2007-09-06 | University Of Washington | Design of membrane actuator based on ferromagnetic shape memory alloy composite for sythentic jet actuator |
US7280016B2 (en) * | 2003-02-27 | 2007-10-09 | University Of Washington | Design of membrane actuator based on ferromagnetic shape memory alloy composite for synthetic jet actuator |
US20070289301A1 (en) * | 2003-02-27 | 2007-12-20 | University Of Washington | Torque actuator incorporating shape memory alloy composites |
US7667560B2 (en) | 2003-02-27 | 2010-02-23 | University Of Washington | Membrane actuator based on ferromagnetic shape memory alloy composite for synthetic jet actuator |
US20080197208A1 (en) * | 2003-02-27 | 2008-08-21 | University Of Washington | Membrane actuator based on ferromagnetic shape memory alloy composite for synthetic jet actuator |
US7478845B2 (en) | 2004-03-12 | 2009-01-20 | Gm Global Technology Operations, Inc. | Active materials based approaches to latch snug down and articles containing the same |
US20050199455A1 (en) * | 2004-03-12 | 2005-09-15 | Browne Alan L. | Customizable strut assemblies and articles that employ the same |
US8261892B2 (en) | 2004-03-12 | 2012-09-11 | GM Global Technology Operations LLC | Customizable strut assemblies and articles that employ the same |
US20050206175A1 (en) * | 2004-03-12 | 2005-09-22 | Browne Alan L | Active materials based approaches to latch snug down and articles containing the same |
US20050230195A1 (en) * | 2004-03-12 | 2005-10-20 | Jones Gary L | Devices for holding intermediate positions and articles that contain the same |
US20080141736A1 (en) * | 2004-03-12 | 2008-06-19 | Jones Gary L | Devices for holding intermediate positions and articles that contain the same |
US7648589B2 (en) | 2004-09-08 | 2010-01-19 | University Of Washington | Energy absorbent material |
US20060056993A1 (en) * | 2004-09-14 | 2006-03-16 | Moshe Gombinsky | Magnetic spring actuator device |
US20100229610A1 (en) * | 2006-06-23 | 2010-09-16 | Cornerstone Research Group, Inc. | Locking Device Using Shape Memory Materials |
US20080230330A1 (en) * | 2007-03-20 | 2008-09-25 | Siemens Aktiengesellschaft | Braking device having a wedge mechanism |
US20090038126A1 (en) * | 2007-08-08 | 2009-02-12 | Key Safety Systems, Inc. | Seat belt buckle |
US20120198665A1 (en) * | 2007-08-08 | 2012-08-09 | Key Safety Systems, Inc. | Seat belt buckle |
US7905538B2 (en) * | 2007-08-31 | 2011-03-15 | Gm Global Technology Operations, Inc. | Active material based concealment devices for seams |
US20090058130A1 (en) * | 2007-08-31 | 2009-03-05 | Gm Global Technology Operations, Inc. | Active material based concealment devices for seams |
US20090130391A1 (en) * | 2007-11-02 | 2009-05-21 | University Of Washington | Design of shape memory alloy fibers and shape memory polymer fibers and films and their composites for reversible shape changes |
US8586176B2 (en) | 2007-11-02 | 2013-11-19 | University Of Washington | Shape memory alloy fibers and shape memory polymer fibers and films and their composites for reversible shape changes |
US20100305777A1 (en) * | 2008-01-07 | 2010-12-02 | Bio-Rad Laboratories, Inc. | Piston position detection for preparative chromatography column |
WO2009089221A1 (en) * | 2008-01-07 | 2009-07-16 | Bio-Rad Laboratories, Inc. | Piston position detection for preparative chromatography column |
US20090230060A1 (en) * | 2008-01-07 | 2009-09-17 | Bio-Rad Laboratories, Inc. | Piston position detection for preparative chromatography column |
US20090278342A1 (en) * | 2008-05-06 | 2009-11-12 | Gm Global Technology Operations, Inc. | Vehicle roll bar apparatus with active material actuation |
US8210547B2 (en) * | 2009-06-16 | 2012-07-03 | Toyota Motor Engineering & Manufacturing North America, Inc. | Active magneto-rheological spring assemblies and vehicle suspension systems incorporating the same |
US20100314842A1 (en) * | 2009-06-16 | 2010-12-16 | Toyota Motor Engineering & Manufacturing North America, Inc. | Active Magneto-Rheological Spring Assemblies and Vehicle Suspension Systems Incorporating the Same |
US8313108B2 (en) * | 2010-07-22 | 2012-11-20 | GM Global Technology Operations LLC | Stiffness control using smart actuators |
US20120018962A1 (en) * | 2010-07-22 | 2012-01-26 | Gm Global Technology Operations, Inc. | Stiffness control using smart actuators |
US20140042756A1 (en) * | 2012-08-13 | 2014-02-13 | GM Global Technology Operations LLC | Latchable or lockable device |
US9004551B2 (en) * | 2012-08-13 | 2015-04-14 | GM Global Technology Operations LLC | Latchable or lockable device |
US9581214B2 (en) * | 2013-06-24 | 2017-02-28 | The Regents Of The University Of California | Semi-active isolators based on magnetorheological nanocomposites |
US20140376837A1 (en) * | 2013-06-24 | 2014-12-25 | The Regents Of The University Of California | Semi-active insolators based on magnetorheological nanocomposites |
US20160152108A1 (en) * | 2013-07-24 | 2016-06-02 | Kyb Corporation | Shock absorber mounting device |
US9616727B2 (en) * | 2013-07-24 | 2017-04-11 | Kyb Corporation | Shock absorber mounting device |
US9859834B2 (en) | 2016-02-05 | 2018-01-02 | GM Global Technology Operations LLC | Slack compensator |
US10208823B2 (en) * | 2017-01-10 | 2019-02-19 | Toyota Motor Engineering & Manufacturing North America, Inc. | Variable rate bound stoppers and variable rate suspension systems containing variable rate bound stoppers |
US10597917B2 (en) | 2017-10-09 | 2020-03-24 | GM Global Technology Operations LLC | Stretchable adjustable-stiffness assemblies |
US10604201B2 (en) | 2018-03-29 | 2020-03-31 | Shimano Inc. | Telescopic apparatus |
Also Published As
Publication number | Publication date |
---|---|
US20080141736A1 (en) | 2008-06-19 |
US8261892B2 (en) | 2012-09-11 |
US20050205364A1 (en) | 2005-09-22 |
US20050230195A1 (en) | 2005-10-20 |
US20090008844A1 (en) | 2009-01-08 |
WO2005089188A3 (en) | 2009-04-16 |
WO2005089188A2 (en) | 2005-09-29 |
US7478845B2 (en) | 2009-01-20 |
WO2005089168A3 (en) | 2009-04-02 |
US20050206175A1 (en) | 2005-09-22 |
US20100236881A1 (en) | 2010-09-23 |
WO2005089168A2 (en) | 2005-09-29 |
US20050199455A1 (en) | 2005-09-15 |
US8069963B2 (en) | 2011-12-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20050263359A1 (en) | Customizable strut assemblies having variable stroke lengths and articles employing the same | |
US7845709B2 (en) | Active material actuated flow trips | |
US7905538B2 (en) | Active material based concealment devices for seams | |
US7548010B2 (en) | Active material based actuators for large displacements and rotations | |
US7455147B2 (en) | Hood lift mechanisms utilizing active materials and methods of use | |
US7607717B2 (en) | Reversibly deployable spoiler | |
US7258347B2 (en) | Discrete active seal assemblies | |
US7686120B2 (en) | Hood lift mechanisms utilizing active materials and methods of use | |
US7703839B2 (en) | Airflow control devices based on active materials | |
US7669918B2 (en) | Tunable vehicle structural members and methods for selectively changing the mechanical properties thereto | |
US7971393B2 (en) | Door actuation systems | |
US8505987B2 (en) | Electrically-activated hood latch and release mechanism | |
US7331616B2 (en) | Hood latch assemblies utilizing active materials and methods of use | |
US7556117B2 (en) | Hood lift mechanisms utilizing active materials and methods of use | |
US7823682B2 (en) | Hood lift mechanisms utilizing active materials and methods of use | |
US20090278342A1 (en) | Vehicle roll bar apparatus with active material actuation | |
US8267216B2 (en) | Hood lift mechanisms utilizing active materials and methods of use |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC., MICHIGAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MANKAME, NILESH D.;STEVENSON, ROBIN;BROWNE, ALAN L.;AND OTHERS;REEL/FRAME:016640/0088;SIGNING DATES FROM 20050502 TO 20050802 |
|
AS | Assignment |
Owner name: UNITED STATES DEPARTMENT OF THE TREASURY, DISTRICT Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:022201/0405 Effective date: 20081231 Owner name: UNITED STATES DEPARTMENT OF THE TREASURY,DISTRICT Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:022201/0405 Effective date: 20081231 |
|
AS | Assignment |
Owner name: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECU Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:022553/0446 Effective date: 20090409 Owner name: CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SEC Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:022553/0446 Effective date: 20090409 |
|
AS | Assignment |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC., MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:UNITED STATES DEPARTMENT OF THE TREASURY;REEL/FRAME:023124/0429 Effective date: 20090709 Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC.,MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:UNITED STATES DEPARTMENT OF THE TREASURY;REEL/FRAME:023124/0429 Effective date: 20090709 |
|
AS | Assignment |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC., MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNORS:CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES;CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES;REEL/FRAME:023127/0468 Effective date: 20090814 Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC.,MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNORS:CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES;CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES;REEL/FRAME:023127/0468 Effective date: 20090814 |
|
AS | Assignment |
Owner name: UNITED STATES DEPARTMENT OF THE TREASURY, DISTRICT Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:023156/0052 Effective date: 20090710 Owner name: UNITED STATES DEPARTMENT OF THE TREASURY,DISTRICT Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:023156/0052 Effective date: 20090710 |
|
AS | Assignment |
Owner name: UAW RETIREE MEDICAL BENEFITS TRUST, MICHIGAN Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:023162/0001 Effective date: 20090710 Owner name: UAW RETIREE MEDICAL BENEFITS TRUST,MICHIGAN Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:023162/0001 Effective date: 20090710 |
|
AS | Assignment |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC., MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:UNITED STATES DEPARTMENT OF THE TREASURY;REEL/FRAME:025245/0442 Effective date: 20100420 Owner name: GM GLOBAL TECHNOLOGY OPERATIONS, INC., MICHIGAN Free format text: RELEASE BY SECURED PARTY;ASSIGNOR:UAW RETIREE MEDICAL BENEFITS TRUST;REEL/FRAME:025311/0770 Effective date: 20101026 |
|
AS | Assignment |
Owner name: WILMINGTON TRUST COMPANY, DELAWARE Free format text: SECURITY AGREEMENT;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:025327/0001 Effective date: 20101027 |
|
AS | Assignment |
Owner name: GM GLOBAL TECHNOLOGY OPERATIONS LLC, MICHIGAN Free format text: CHANGE OF NAME;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:025780/0936 Effective date: 20101202 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |