BR112012017396A2 - sistema multifuncional de descongelamento / anticongelamento - Google Patents
sistema multifuncional de descongelamento / anticongelamentoInfo
- Publication number
- BR112012017396A2 BR112012017396A2 BR112012017396A BR112012017396A BR112012017396A2 BR 112012017396 A2 BR112012017396 A2 BR 112012017396A2 BR 112012017396 A BR112012017396 A BR 112012017396A BR 112012017396 A BR112012017396 A BR 112012017396A BR 112012017396 A2 BR112012017396 A2 BR 112012017396A2
- Authority
- BR
- Brazil
- Prior art keywords
- conductive
- defrost
- multifunction
- antifreeze system
- structures
- Prior art date
Links
- 230000002528 anti-freeze Effects 0.000 title abstract 3
- 239000002086 nanomaterial Substances 0.000 abstract 2
- 108010053481 Antifreeze Proteins Proteins 0.000 abstract 1
- 230000020169 heat generation Effects 0.000 abstract 1
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/10—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor
- H05B3/12—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material
- H05B3/14—Heating elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material the material being non-metallic
- H05B3/145—Carbon only, e.g. carbon black, graphite
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B2214/00—Aspects relating to resistive heating, induction heating and heating using microwaves, covered by groups H05B3/00, H05B6/00
- H05B2214/04—Heating means manufactured by using nanotechnology
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Surface Heating Bodies (AREA)
- Control Of Resistance Heating (AREA)
- Laminated Bodies (AREA)
- Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
Abstract
sistema multifuncional de descongelamento / anticongelamento. a invenção refere-se a um sistema de descongelamento / anticongelamento compreendendo pelo menos duas estruturas condutoras (3', 3'') embutidas em um artigo (2), que inclui uma superfície exterior (5) sendo projetada como uma superfície aerodinâmica, pelo menos, uma das estruturas condutoras (3 ', 3'') está disposta adjacente á superfície exterior (5) uma unidade de controle (39) está adaptada para controlar a alimentação de energia para as estruturas condutoras (3 ', 3'') para a geração de calor para a superfície exterior (5), uma estrutura condutora (3 ') que compreende uma primeira nanoestrutura condutora (19 '), a propriedade condutora da estrutura condutora (3') difere da propriedade condutora da outra estrutura condutora (3''), compreendendo uma segunda nanoestrutura condutora (19'').
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/SE2010/050028 WO2011087412A1 (en) | 2010-01-14 | 2010-01-14 | Multifunctional de-icing/anti-icing system |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112012017396A2 true BR112012017396A2 (pt) | 2016-04-19 |
Family
ID=44304483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012017396A BR112012017396A2 (pt) | 2010-01-14 | 2010-01-14 | sistema multifuncional de descongelamento / anticongelamento |
Country Status (5)
Country | Link |
---|---|
US (1) | US8931740B2 (pt) |
EP (1) | EP2523854B1 (pt) |
BR (1) | BR112012017396A2 (pt) |
CA (1) | CA2786838C (pt) |
WO (1) | WO2011087412A1 (pt) |
Families Citing this family (47)
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FR2932456B1 (fr) * | 2008-06-17 | 2010-05-28 | Airbus France | Systeme de drainage d'un courant de foudre genere par une decharge orageuse sur un aeronef |
WO2011094347A2 (en) | 2010-01-26 | 2011-08-04 | Metis Design Corporation | Multifunctional cnt-engineered structures |
DE12702329T1 (de) * | 2010-12-31 | 2015-03-26 | Battelle Memorial Institute | Antivereisungs-, Enteisungs- und Erhitzungskonfigurations-, Integrations- und Stromversorgungsverfahren für Flugzeuge sowie aerodynamische und komplexe Oberflächen |
DE102011119844A1 (de) * | 2011-05-26 | 2012-12-13 | Eads Deutschland Gmbh | Verbundstruktur mit Eisschutzvorrichtung sowie Herstellverfahren |
FR2984418B1 (fr) * | 2011-12-19 | 2014-01-24 | Valeol | Procede de degivrage de structures en materiaux composites, notamment de pales d'une eolienne, composition adaptee et dispositif adapte |
WO2014074034A1 (en) * | 2012-11-08 | 2014-05-15 | Saab Ab | De-icing arrangement and method for de-icing a structural element |
GB2512020A (en) * | 2012-12-11 | 2014-09-24 | Airbus Operations Ltd | A method of preventing the formation of ice on an aircraft |
GB2511343B (en) | 2013-02-28 | 2015-07-22 | Gkn Aerospace Services Ltd | Ice protection system |
GB201306674D0 (en) * | 2013-04-12 | 2013-05-29 | Rolls Royce Plc | Rigid Raft for a Gas Turbine Engine |
US9868536B2 (en) * | 2013-10-30 | 2018-01-16 | Goodrich Corporation | Electrical interconnects for ice protection systems |
EP3130196A4 (en) * | 2014-04-10 | 2017-12-06 | Metis Design Corporation | Multifunctional assemblies |
US10368401B2 (en) * | 2014-06-03 | 2019-07-30 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
US10167550B2 (en) | 2014-06-03 | 2019-01-01 | Aurora Flight Sciences Corporation | Multi-functional composite structures |
US10285219B2 (en) | 2014-09-25 | 2019-05-07 | Aurora Flight Sciences Corporation | Electrical curing of composite structures |
FR3045567B1 (fr) * | 2015-12-21 | 2018-01-19 | Ratier Figeac | Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef |
US10273012B2 (en) * | 2016-09-08 | 2019-04-30 | Ge Aviation Systems Llc | Deicing module for an aircraft and method for deicing |
US10986699B2 (en) * | 2016-09-20 | 2021-04-20 | Goodrich Corporation | Thermally conductive, electrically insulating protection layer for de-icing heaters |
US10708979B2 (en) | 2016-10-07 | 2020-07-07 | De-Ice Technologies | Heating a bulk medium |
US10472977B2 (en) * | 2016-12-29 | 2019-11-12 | Goodrich Corporation | Erosion strip integrated with carbon allotrope-based deicing/ anti-icing elements |
US10494107B2 (en) * | 2017-01-03 | 2019-12-03 | Goodrich Corporation | Additive manufacturing of conformal deicing and boundary layer control surface for aircraft |
US10457404B2 (en) * | 2017-01-31 | 2019-10-29 | Wan Tony Chee | Carbon nanotube anti-icing and de-icing means for aircraft |
GB2561393B (en) * | 2017-04-13 | 2019-12-04 | Gkn Aerospace Services Ltd | Electrothermal heater |
US20190016466A1 (en) * | 2017-07-13 | 2019-01-17 | Goodrich Coporation | Redundant heating of surfaces of an aircraft skin for controlling ice accretion |
US10960983B2 (en) * | 2017-09-01 | 2021-03-30 | Textron Innovations Inc. | Tailored rotor-blade ice-protection system |
DK3456961T3 (da) * | 2017-09-14 | 2020-09-07 | Siemens Gamesa Renewable Energy As | Vindmøllevinge med afdækningsplade, der dækker varmluftudblæsning til afisning og/eller overisningsbeskyttelse |
US10183754B1 (en) * | 2017-12-20 | 2019-01-22 | The Florida International University Board Of Trustees | Three dimensional graphene foam reinforced composite coating and deicing systems therefrom |
US10669033B2 (en) * | 2017-12-21 | 2020-06-02 | The Boeing Company | Integrated lightning protection and electrical de-icing for aerodynamic structures |
US10822097B2 (en) * | 2018-02-15 | 2020-11-03 | Booz Allen Hamilton Inc. | Ice formation detection and removal system for an aerial vehicle and method |
US20190292420A1 (en) * | 2018-03-22 | 2019-09-26 | Goodrich Corporation | Installation of pneumatic de-icers with vertically aligned carbon nanotubes |
EP3546364A1 (en) * | 2018-03-28 | 2019-10-02 | Ratier-Figeac SAS | De-icing apparatus |
GB2574184B (en) * | 2018-03-29 | 2020-12-02 | Gkn Aerospace Services Ltd | Ice removal system |
DE102018002917A1 (de) * | 2018-04-10 | 2019-10-10 | Airbus Operations Gmbh | Beheizbare Fußbodenplatte und Fußbodenheizsystem für ein Flugzeug |
BR112020021755B1 (pt) * | 2018-04-24 | 2022-07-05 | Qarbon Aerospace (Foundation), Llc | Aeroestrutura aquecida |
KR20230028573A (ko) | 2018-05-03 | 2023-02-28 | 카본 에어로스페이스 (파운데이션), 엘엘씨 | 국부적인 절연 층을 갖는 열가소성 항공기 구조물 및 항공기 구조물을 형성하기 위한 방법 |
DE102018111703A1 (de) * | 2018-05-16 | 2019-11-21 | Airbus Defence and Space GmbH | Strukturbauteil für ein Flugzeug |
DE102018004814A1 (de) | 2018-06-19 | 2019-12-19 | Airbus Operations Gmbh | Beheizbare Vorderkantenvorrichtung, Vorderkantenheizsystem und Luftfahrzeug damit |
US11261787B2 (en) * | 2018-06-22 | 2022-03-01 | General Electric Company | Aircraft anti-icing system |
US11242150B2 (en) * | 2018-06-22 | 2022-02-08 | General Electric Company | Anti-icing system for an aircraft |
EP3844065B1 (en) | 2018-08-27 | 2023-05-10 | De-Ice Technologies, Inc. | De-icing systems |
GB201820301D0 (en) * | 2018-12-13 | 2019-01-30 | Rolls Royce Plc | Water and ice detection |
CN111698796A (zh) * | 2019-03-11 | 2020-09-22 | 南京银纳新材料科技有限公司 | 一种耐反复刮擦银纳米线薄膜加热器的制备方法 |
US11548648B2 (en) * | 2020-01-14 | 2023-01-10 | Goodrich Corporation | Robust power transmission |
US20210231592A1 (en) * | 2020-01-24 | 2021-07-29 | Goodrich Corporation | Multi-layered ice detector apparatus |
US20220022286A1 (en) * | 2020-07-20 | 2022-01-20 | Goodrich Corporation | Metallized carbon nanotube elements for electrothermal ice protection |
EP4074603A1 (en) * | 2021-04-15 | 2022-10-19 | Airbus Defence and Space GmbH | De-icing system, airfoil and aircraft having such a system, and de-icing method |
EP4137696A1 (en) * | 2021-08-16 | 2023-02-22 | General Electric Renovables España S.L. | A system comprising a structure being prone to lightning strikes and icing, a method for operating the system and a wind turbine comprising the system |
US20240262515A1 (en) * | 2023-02-02 | 2024-08-08 | Raytheon Technologies Corporation | Hybrid electric engine and nacelle system |
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FR2779314B1 (fr) * | 1998-05-27 | 2000-08-04 | Eurocopter France | Dispositif de chauffage a elements resistifs d'un profil aerodynamique |
DE10016259C2 (de) | 2000-04-03 | 2002-06-20 | Karlsruhe Forschzent | Kompakte millimeterwellentechnische Einrichtung zum Enteisen und/oder Vorbeugeneiner Vereisung |
JP2001316502A (ja) * | 2000-04-28 | 2001-11-16 | Jsr Corp | 伝熱性シートおよびそれを用いた加熱構造、放熱構造、電気的検査方法および装置。 |
JP2003174127A (ja) * | 2001-12-04 | 2003-06-20 | Polymatech Co Ltd | 異方性伝熱シートおよびその製造方法 |
US6965513B2 (en) * | 2001-12-20 | 2005-11-15 | Intel Corporation | Carbon nanotube thermal interface structures |
FR2863586B1 (fr) | 2003-12-12 | 2007-01-19 | Eurocopter France | Dispositif de degivrage/antigivrage modulaire d'une surface aerodynamique. |
US7278610B2 (en) * | 2004-03-03 | 2007-10-09 | Goodrich Corporation | Aircraft wing with electrothermal deicing and/or anti-icing device |
US7281318B2 (en) * | 2004-05-19 | 2007-10-16 | The Boeing Company | Method of manufacturing a composite structural member having an integrated electrical circuit |
ATE430091T1 (de) * | 2005-02-09 | 2009-05-15 | Qinetiq Ltd | Elektrothermische heizvorrichtung zum schutz von aerodynamischen oberflächen vor eis und ihre herstellungsverfahren |
US7291815B2 (en) * | 2006-02-24 | 2007-11-06 | Goodrich Corporation | Composite ice protection heater and method of producing same |
EP1873060B1 (en) | 2006-06-26 | 2010-04-07 | Honeywell International Inc. | Hybrid electrical ice protection system and method including an energy saving mode |
US20080166563A1 (en) * | 2007-01-04 | 2008-07-10 | Goodrich Corporation | Electrothermal heater made from thermally conducting electrically insulating polymer material |
US8388795B2 (en) * | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
US8146861B2 (en) * | 2007-11-29 | 2012-04-03 | Airbus Deutschland Gmbh | Component with carbon nanotubes |
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US9004407B2 (en) * | 2008-12-24 | 2015-04-14 | Middle River Aircraft Systems | Anti-icing system and method for preventing ice accumulation |
US8549832B2 (en) * | 2009-12-30 | 2013-10-08 | MRA Systems Inc. | Turbomachine nacelle and anti-icing system and method therefor |
ES2640189T3 (es) * | 2010-01-14 | 2017-11-02 | Saab Ab | Artículo con una función de descongelación / anticongelación |
DE12702329T1 (de) * | 2010-12-31 | 2015-03-26 | Battelle Memorial Institute | Antivereisungs-, Enteisungs- und Erhitzungskonfigurations-, Integrations- und Stromversorgungsverfahren für Flugzeuge sowie aerodynamische und komplexe Oberflächen |
-
2010
- 2010-01-14 BR BR112012017396A patent/BR112012017396A2/pt active Search and Examination
- 2010-01-14 US US13/522,368 patent/US8931740B2/en active Active
- 2010-01-14 CA CA2786838A patent/CA2786838C/en active Active
- 2010-01-14 WO PCT/SE2010/050028 patent/WO2011087412A1/en active Application Filing
- 2010-01-14 EP EP10702174.3A patent/EP2523854B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2523854B1 (en) | 2015-12-16 |
CA2786838A1 (en) | 2011-07-21 |
CA2786838C (en) | 2017-01-10 |
EP2523854A1 (en) | 2012-11-21 |
EP2523854A4 (en) | 2015-01-21 |
US20130043342A1 (en) | 2013-02-21 |
WO2011087412A1 (en) | 2011-07-21 |
US8931740B2 (en) | 2015-01-13 |
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Legal Events
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B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B11D | Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time |