US1463498A - Armor for gasoline tanks of aeroplanes and for other purposes - Google Patents
Armor for gasoline tanks of aeroplanes and for other purposes Download PDFInfo
- Publication number
- US1463498A US1463498A US255518A US25551818A US1463498A US 1463498 A US1463498 A US 1463498A US 255518 A US255518 A US 255518A US 25551818 A US25551818 A US 25551818A US 1463498 A US1463498 A US 1463498A
- Authority
- US
- United States
- Prior art keywords
- armor
- balls
- plate
- layers
- aeroplanes
- 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.)
- Expired - Lifetime
Links
- 239000012858 resilient material Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000008933 bodily movement Effects 0.000 description 1
- 239000007799 cork Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0492—Layered armour containing hard elements, e.g. plates, spheres, rods, separated from each other, the elements being connected to a further flexible layer or being embedded in a plastics or an elastomer matrix
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/90—Rupture proof
Definitions
- My invention relates to bullet proof armor. It has for its object to produce a type of armor that is particularly adapted for the protection of gasoline tanks carried by aeroplanes though it is adapted for a wide "ariety of other uses.
- the armor is relatively light and is intended for a protection against the fire of machine guns and small arms.
- FIG. 1 1s a view of a gasoline tank provided with my invention.
- Fig. 2 is a detail sectional view of a piece of armor embodying my inventlon.
- A designates the article to be protected, such as a gasoline tank, and B, the armor covering it. In practice this will be manufactured in shapes best suited to resist gun fire and the tanks will be shaped to fit the armor.
- Fig. 2, 2 designates the outer shell of the armor, preferably formed of a plate of hard steel, curved so as to deflect a bullet strik ing it at an angle. This armor plate will be thin, preferably about of an inch in thickness.
- Another plate, 3 constitutes the inner shell or wall of the armor. This is adapted to lie against the surface of the tank or other article to be protected. It is preferably of hard steel and is curved so as to be concentric with the outer plate 2.
- a similar layer 5 lies just inside the metal plate 3.
- metal balls 6 There should be several layers of these, preferably three, as shown, and they should be packed in the space between said layers as closely as they will lie; the balls, however, although in contact with each other, being free to turn individually.
- the armor may be of any suitable hard metal, but when the armor is used as a protective covering for the gasoline tank of an aeroplane they are preferably made of aluminum in order to reduce the weight of the armor I as much as possible.
- the thickness of the layers 4 and 5 should be at least equal to the length of a bullet the armor is supposed to protect against. The reason for this is that the bullet shall not be supported and guided by the armor plate 2 that it may have pierced at the moment its end comes into engagement with one of the balls 6, but rather shall be free (the layer 4 ofl'ering little resistance to the bullet being deflected laterally) to be deflected by engagement with one of the balls 6.
- the two plates 2 and 3 having secured to them the layers of material 4 and 5, are placed at approximately the desired distance apart and the space between the layers is filled with the balls 6. The plates are then forced toward each other until the layers 4 and 5 bear forcibly upon the balls of the outer rows, which are thereby crowded together and held securely in place.
- the resilient nature of the layers 4 and 5 permits the action just described. After the plates have been forced toward each other to the desired degree they are united by any suitable means such as the bolts 7 and the armor is complete.
- the armor described is adapted to a great variety of uses.
- the dimensions of its several parts may be largely increased so that it may act as a dcjectiles that may strike it, only those making direct or approximately direct hits being able to puncture it.
- Those that do puncture will be so deflected and interfered with in their course by the resisting balls 6 that their force will be largely spent before reaching the inner plate 3.
- the deflection of the course of a projectile incident to its passage through the balls 6 will render it most improbable that it strike the plate 3 directly. Instead its angle of incidence will probably be such that it will be deflected and follow the surface of the plate on the inside, plowing through the layer 5, or being deflected back into the mass of balls 6.
- the deflecting balls 6 are relatively large, that is to say, the diameter is considerably greater than is the thickness of the armor shell 2, as well as bein greater than the diameter of the projectile which it is intended to deflect. This elementof size is important, else the balls will not operate to deflect and change the course of the projectile.
- a projectile-resisting armor comprising a thin outer armor plate and a series of relatively large balls free to rotate and deflect such projectiles as may pass through the outer plate and an inner wall cooperating with the outer armor plate to hold the balls in place.
- a projectile-resisting armor comprising individually rotate to deflect such projec-.
- a projectile-resisting armor comprising a set of relatively large loose balls arranged in a plurality of layers, outer and inner layers of resilient material between which the balls are arranged, for holding them in place, a thin projectile-resisting armor shell outside the outer layer of resilient material and an inner wall inside the inner layer of resilient material.
- a projectile-resisting armor comprising a'set of relatively large loose balls arranged in a plurality of layers, outer and inner layers of resilient'material between which the balls are arranged, for holding them in place, and hard projectile-resisting armor plates respectively covering said layers of resilient material, the plates being united to cause the balls to be closely confined between the said resilient layers.
- a projectile-resisting armor comprising a thin outer plate of hard metal, a layer of resilient material inside the said plate, aseries of relatively large metal balls inside the said layer of resilient material, the balls being each free to individually rotate, the thickness of the resilient layer being greater than the thickness of the outer plate, and an inner wall co-operating with the outer plate to hold the intermediate parts of the armor in place.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
July 31, 1993 N. W. BURGESS ARMOR FOR GASOLINE TANKS OF AEROPLANES AND FOR OTHER PURPOSES Filed Sent. 24, 1918 Patented July 31, 1923.
UNITED STATES PATENT OFFICE.
NORMAN W. BURGESS, OF LEXINGTON, VIRGINIA.
ARMOR FOR GASOLINE TANKS 0F AEROPLANES AND FOR OTHER PURPOSES.
Application filed September 24, 1918. Serial No. 255,518.
To all whom it may concern:
Be it known that I, NORMAN W. BURGESS, a citizen of the United States, residing at Lexington, in the county of Rockbridge and State of Virginia, have invented certain new and useful Improvements in Armor for Gasoline Tanks of Aeroplanes and for Other Purposes, of which the following is a specification.
My invention relates to bullet proof armor. It has for its object to produce a type of armor that is particularly adapted for the protection of gasoline tanks carried by aeroplanes though it is adapted for a wide "ariety of other uses. The armor is relatively light and is intended for a protection against the fire of machine guns and small arms.
In the accompanying drawings Fig. 1 1s a view of a gasoline tank provided with my invention. Fig. 2 is a detail sectional view of a piece of armor embodying my inventlon.
In the drawings A designates the article to be protected, such as a gasoline tank, and B, the armor covering it. In practice this will be manufactured in shapes best suited to resist gun fire and the tanks will be shaped to fit the armor. Referring particularly to Fig. 2, 2 designates the outer shell of the armor, preferably formed of a plate of hard steel, curved so as to deflect a bullet strik ing it at an angle. This armor plate will be thin, preferably about of an inch in thickness. Another plate, 3, constitutes the inner shell or wall of the armor. This is adapted to lie against the surface of the tank or other article to be protected. It is preferably of hard steel and is curved so as to be concentric with the outer plate 2.
Just inside the plate 2 is a layer 4 of more or less resilient or yielding substance, such as comminuted cork, or unwoven fiber. A similar layer 5 lies just inside the metal plate 3. Between the layers of material, 4 and 5. are arranged metal balls 6. There should be several layers of these, preferably three, as shown, and they should be packed in the space between said layers as closely as they will lie; the balls, however, although in contact with each other, being free to turn individually.
They may be of any suitable hard metal, but when the armor is used as a protective covering for the gasoline tank of an aeroplane they are preferably made of aluminum in order to reduce the weight of the armor I as much as possible.
Should a bullet pierce the outer plate 2 and come into contact with one of the balls 6,-the chances are that the engagement will be at an angle. The balls are packed into the space between the layers 4 and 5 closely and are held in place so securely, that when one of them is struck by a bullet it will yield but little, but will rather rotate, deflecting the course of the bullet. Such deflection will cause the nose of the bullet to come into engagement with the adjacent ball which, rotating without much bodily movement, will again deflect the bullet; and this will proceed as the bullet comes into engagement with one ball after another, its speed and force being reduced and its course changed at each new contact, with the result that it may never reach the inner plate 3 at all, or if it does it will be with its speed and force so mu h reduced that it cannot penetrate the latter. Should the bullet strike one of the balls radially the ball might be broken, when the bullet would pass onto engage tangentially, or at an angle, with aball in the next row. to be thereby deflected, as has been described.
The thickness of the layers 4 and 5 should be at least equal to the length of a bullet the armor is supposed to protect against. The reason for this is that the bullet shall not be supported and guided by the armor plate 2 that it may have pierced at the moment its end comes into engagement with one of the balls 6, but rather shall be free (the layer 4 ofl'ering little resistance to the bullet being deflected laterally) to be deflected by engagement with one of the balls 6. In the manufacture of the armor the two plates 2 and 3, having secured to them the layers of material 4 and 5, are placed at approximately the desired distance apart and the space between the layers is filled with the balls 6. The plates are then forced toward each other until the layers 4 and 5 bear forcibly upon the balls of the outer rows, which are thereby crowded together and held securely in place. The resilient nature of the layers 4 and 5 permits the action just described. After the plates have been forced toward each other to the desired degree they are united by any suitable means such as the bolts 7 and the armor is complete.
As has been intimated the armor described is adapted to a great variety of uses. The dimensions of its several parts may be largely increased so that it may act as a dcjectiles that may strike it, only those making direct or approximately direct hits being able to puncture it. Those that do puncture will be so deflected and interfered with in their course by the resisting balls 6 that their force will be largely spent before reaching the inner plate 3. The deflection of the course of a projectile incident to its passage through the balls 6 will render it most improbable that it strike the plate 3 directly. Instead its angle of incidence will probably be such that it will be deflected and follow the surface of the plate on the inside, plowing through the layer 5, or being deflected back into the mass of balls 6.
The deflecting balls 6 are relatively large, that is to say, the diameter is considerably greater than is the thickness of the armor shell 2, as well as bein greater than the diameter of the projectile which it is intended to deflect. This elementof size is important, else the balls will not operate to deflect and change the course of the projectile.
What I claim is:
1. A projectile-resisting armor comprising a thin outer armor plate and a series of relatively large balls free to rotate and deflect such projectiles as may pass through the outer plate and an inner wall cooperating with the outer armor plate to hold the balls in place.
2. A projectile-resisting armor comprising individually rotate to deflect such projec-.
tiles as may pass through the outer armor plate.
3. A projectile-resisting armor comprising a set of relatively large loose balls arranged in a plurality of layers, outer and inner layers of resilient material between which the balls are arranged, for holding them in place, a thin projectile-resisting armor shell outside the outer layer of resilient material and an inner wall inside the inner layer of resilient material. I
4. A projectile-resisting armor comprising a'set of relatively large loose balls arranged in a plurality of layers, outer and inner layers of resilient'material between which the balls are arranged, for holding them in place, and hard projectile-resisting armor plates respectively covering said layers of resilient material, the plates being united to cause the balls to be closely confined between the said resilient layers.
5. A projectile-resisting armor comprising a thin outer plate of hard metal, a layer of resilient material inside the said plate, aseries of relatively large metal balls inside the said layer of resilient material, the balls being each free to individually rotate, the thickness of the resilient layer being greater than the thickness of the outer plate, and an inner wall co-operating with the outer plate to hold the intermediate parts of the armor in place.
NORMAN W. BURGESS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US255518A US1463498A (en) | 1918-09-24 | 1918-09-24 | Armor for gasoline tanks of aeroplanes and for other purposes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US255518A US1463498A (en) | 1918-09-24 | 1918-09-24 | Armor for gasoline tanks of aeroplanes and for other purposes |
Publications (1)
Publication Number | Publication Date |
---|---|
US1463498A true US1463498A (en) | 1923-07-31 |
Family
ID=22968690
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US255518A Expired - Lifetime US1463498A (en) | 1918-09-24 | 1918-09-24 | Armor for gasoline tanks of aeroplanes and for other purposes |
Country Status (1)
Country | Link |
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US (1) | US1463498A (en) |
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500158A (en) * | 1943-06-23 | 1950-03-14 | Celanese Corp | Self-sealing fuel container having a sealing layer composed of a textile fabric coated with a mixed cellulose ester |
US2503537A (en) * | 1947-08-09 | 1950-04-11 | James A Youngblood | Sawproof grating bar |
US2916179A (en) * | 1958-01-13 | 1959-12-08 | British Oxygen Co Ltd | Thermally insulated storage vessels |
US2928529A (en) * | 1958-02-13 | 1960-03-15 | Res Inst Of Temple University | Storage of explosive gases |
US2994452A (en) * | 1954-08-02 | 1961-08-01 | Conch Int Methane Ltd | Insulated tank for liquefied hydrocarbons and the like with loose membranous lining therefor |
US3431818A (en) * | 1965-04-26 | 1969-03-11 | Aerojet General Co | Lightweight protective armor plate |
US3523057A (en) * | 1965-10-24 | 1970-08-04 | Schjeldahl Co G T | Ball and plastic armour plate |
US3638589A (en) * | 1970-02-02 | 1972-02-01 | Diebold Inc | Protective door structure |
US3705558A (en) * | 1963-04-24 | 1972-12-12 | Gen Motors Corp | Armor |
US4561362A (en) * | 1980-06-18 | 1985-12-31 | Wildermuth Wallace P | Mobile-immobile safe |
US5500037A (en) * | 1988-12-06 | 1996-03-19 | Alhamad; Shaikh G. M. Y. | Impact Absorber |
US5866839A (en) * | 1994-03-21 | 1999-02-02 | Ohayon; Shalom | High performance armor protection system for tank crews and fighting vehicles |
US6408734B1 (en) * | 1998-04-14 | 2002-06-25 | Michael Cohen | Composite armor panel |
US6575075B2 (en) * | 2000-10-05 | 2003-06-10 | Michael Cohen | Composite armor panel |
US6581504B2 (en) * | 2000-12-15 | 2003-06-24 | Paul Caron | Passive armor for protection against shaped charges |
WO2006087699A2 (en) * | 2005-02-21 | 2006-08-24 | Arie Israeli | Armor assembly |
US20070017359A1 (en) * | 2005-06-21 | 2007-01-25 | Gamache Raymond M | Composite armor panel and method of manufacturing same |
US20080006146A1 (en) * | 2004-12-20 | 2008-01-10 | Bjorn Magnusson | Light Ballistic Protection As Building Elements |
US20090293711A1 (en) * | 2008-06-03 | 2009-12-03 | Triton Systems, Inc. | Armor repair kit and methods related thereto |
US8096223B1 (en) * | 2008-01-03 | 2012-01-17 | Andrews Mark D | Multi-layer composite armor and method |
US20120055937A1 (en) * | 2010-09-04 | 2012-03-08 | High Impact Technology, Llc | Differentially armored fuel tank structure and associated fabrication methodology |
US20120174759A1 (en) * | 2008-08-19 | 2012-07-12 | Gallo Michael J | Encapsulated ballistic protection system |
US20150336680A1 (en) * | 2014-05-23 | 2015-11-26 | Airbus Operations Gmbh | Tank System For The Cryogenic Storage Of Hydrogen, And Aircraft With A Tank System For The Cryogenic Storage Of Hydrogen |
US9347746B1 (en) | 2008-01-03 | 2016-05-24 | Great Lakes Armor Systems, Inc. | Armored energy-dispersion objects and method of making and using |
US9370674B2 (en) | 2011-12-05 | 2016-06-21 | High Impact Technology, Llc | Plural layer, plural-action protective coating for liquid fuel container |
US9733049B1 (en) * | 2004-12-08 | 2017-08-15 | Armordynamics, Inc. | Reactive armor system and method |
US9809109B2 (en) | 2015-09-02 | 2017-11-07 | The Boeing Company | Ballooning self-sealing bladders |
US9925863B2 (en) * | 2015-09-02 | 2018-03-27 | The Boeing Company | Self-sealing liquid bladders |
US9950613B2 (en) | 2015-09-02 | 2018-04-24 | The Boeing Company | Use of flaps in fuel bladders to seal punctures |
US10124664B2 (en) | 2015-09-02 | 2018-11-13 | The Boeing Company | Self-sealing liquid bladders |
US10457138B2 (en) | 2015-09-02 | 2019-10-29 | The Boeing Company | Self-sealing liquid bladders |
-
1918
- 1918-09-24 US US255518A patent/US1463498A/en not_active Expired - Lifetime
Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500158A (en) * | 1943-06-23 | 1950-03-14 | Celanese Corp | Self-sealing fuel container having a sealing layer composed of a textile fabric coated with a mixed cellulose ester |
US2503537A (en) * | 1947-08-09 | 1950-04-11 | James A Youngblood | Sawproof grating bar |
US2994452A (en) * | 1954-08-02 | 1961-08-01 | Conch Int Methane Ltd | Insulated tank for liquefied hydrocarbons and the like with loose membranous lining therefor |
US2916179A (en) * | 1958-01-13 | 1959-12-08 | British Oxygen Co Ltd | Thermally insulated storage vessels |
US2928529A (en) * | 1958-02-13 | 1960-03-15 | Res Inst Of Temple University | Storage of explosive gases |
US3705558A (en) * | 1963-04-24 | 1972-12-12 | Gen Motors Corp | Armor |
US3431818A (en) * | 1965-04-26 | 1969-03-11 | Aerojet General Co | Lightweight protective armor plate |
US3523057A (en) * | 1965-10-24 | 1970-08-04 | Schjeldahl Co G T | Ball and plastic armour plate |
US3638589A (en) * | 1970-02-02 | 1972-02-01 | Diebold Inc | Protective door structure |
US4561362A (en) * | 1980-06-18 | 1985-12-31 | Wildermuth Wallace P | Mobile-immobile safe |
US5500037A (en) * | 1988-12-06 | 1996-03-19 | Alhamad; Shaikh G. M. Y. | Impact Absorber |
US5866839A (en) * | 1994-03-21 | 1999-02-02 | Ohayon; Shalom | High performance armor protection system for tank crews and fighting vehicles |
US6408734B1 (en) * | 1998-04-14 | 2002-06-25 | Michael Cohen | Composite armor panel |
US6575075B2 (en) * | 2000-10-05 | 2003-06-10 | Michael Cohen | Composite armor panel |
US6581504B2 (en) * | 2000-12-15 | 2003-06-24 | Paul Caron | Passive armor for protection against shaped charges |
US9733049B1 (en) * | 2004-12-08 | 2017-08-15 | Armordynamics, Inc. | Reactive armor system and method |
US20080006146A1 (en) * | 2004-12-20 | 2008-01-10 | Bjorn Magnusson | Light Ballistic Protection As Building Elements |
US7827897B2 (en) * | 2004-12-20 | 2010-11-09 | Protaurius Aktiebolag | Light ballistic protection as building elements |
WO2006087699A2 (en) * | 2005-02-21 | 2006-08-24 | Arie Israeli | Armor assembly |
WO2006087699A3 (en) * | 2005-02-21 | 2007-05-03 | Arie Israeli | Armor assembly |
US20070017359A1 (en) * | 2005-06-21 | 2007-01-25 | Gamache Raymond M | Composite armor panel and method of manufacturing same |
US8220378B2 (en) * | 2005-06-21 | 2012-07-17 | Specialty Products, Inc. | Composite armor panel and method of manufacturing same |
US8096223B1 (en) * | 2008-01-03 | 2012-01-17 | Andrews Mark D | Multi-layer composite armor and method |
US9835419B2 (en) | 2008-01-03 | 2017-12-05 | Great Lakes Armor Systems, Inc. | Method and system for armored energy-dispersion objects |
US9347746B1 (en) | 2008-01-03 | 2016-05-24 | Great Lakes Armor Systems, Inc. | Armored energy-dispersion objects and method of making and using |
US20090293711A1 (en) * | 2008-06-03 | 2009-12-03 | Triton Systems, Inc. | Armor repair kit and methods related thereto |
US8322267B2 (en) | 2008-06-03 | 2012-12-04 | Triton Systems, Inc. | Armor repair kit and methods related thereto |
US20120174759A1 (en) * | 2008-08-19 | 2012-07-12 | Gallo Michael J | Encapsulated ballistic protection system |
US8616113B2 (en) * | 2008-08-19 | 2013-12-31 | Kelly Space & Technology, Inc. | Encapsulated ballistic protection system |
US20120055937A1 (en) * | 2010-09-04 | 2012-03-08 | High Impact Technology, Llc | Differentially armored fuel tank structure and associated fabrication methodology |
US9370674B2 (en) | 2011-12-05 | 2016-06-21 | High Impact Technology, Llc | Plural layer, plural-action protective coating for liquid fuel container |
US20150336680A1 (en) * | 2014-05-23 | 2015-11-26 | Airbus Operations Gmbh | Tank System For The Cryogenic Storage Of Hydrogen, And Aircraft With A Tank System For The Cryogenic Storage Of Hydrogen |
US9809109B2 (en) | 2015-09-02 | 2017-11-07 | The Boeing Company | Ballooning self-sealing bladders |
US9925863B2 (en) * | 2015-09-02 | 2018-03-27 | The Boeing Company | Self-sealing liquid bladders |
US9950613B2 (en) | 2015-09-02 | 2018-04-24 | The Boeing Company | Use of flaps in fuel bladders to seal punctures |
US10124664B2 (en) | 2015-09-02 | 2018-11-13 | The Boeing Company | Self-sealing liquid bladders |
US10457138B2 (en) | 2015-09-02 | 2019-10-29 | The Boeing Company | Self-sealing liquid bladders |
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