ATE318755T1 - Schutzsystem gegen blitzeinschlag für flugzeugbrennstofftanks aus compositematerial mit geringer elektrischer leitfähigkeit - Google Patents
Schutzsystem gegen blitzeinschlag für flugzeugbrennstofftanks aus compositematerial mit geringer elektrischer leitfähigkeitInfo
- Publication number
- ATE318755T1 ATE318755T1 AT03380301T AT03380301T ATE318755T1 AT E318755 T1 ATE318755 T1 AT E318755T1 AT 03380301 T AT03380301 T AT 03380301T AT 03380301 T AT03380301 T AT 03380301T AT E318755 T1 ATE318755 T1 AT E318755T1
- Authority
- AT
- Austria
- Prior art keywords
- metallic
- electrical conductivity
- outer skin
- protection system
- low electrical
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title abstract 3
- 239000002828 fuel tank Substances 0.000 title 1
- 239000000463 material Substances 0.000 abstract 2
- 239000011152 fibreglass Substances 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 239000007769 metal material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
- B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
-
- 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
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/20—Inserts
- B29K2105/206—Meshes, lattices or nets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
- B29K2705/08—Transition metals
- B29K2705/10—Copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
- B29K2707/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2709/00—Use of inorganic materials not provided for in groups B29K2703/00 - B29K2707/00, for preformed parts, e.g. for inserts
- B29K2709/08—Glass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
- Elimination Of Static Electricity (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200301351A ES2264299B1 (es) | 2003-06-06 | 2003-06-06 | Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica. |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE318755T1 true ATE318755T1 (de) | 2006-03-15 |
Family
ID=33155461
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03380301T ATE318755T1 (de) | 2003-06-06 | 2003-12-19 | Schutzsystem gegen blitzeinschlag für flugzeugbrennstofftanks aus compositematerial mit geringer elektrischer leitfähigkeit |
Country Status (5)
Country | Link |
---|---|
US (1) | US7307825B2 (de) |
EP (1) | EP1484245B1 (de) |
AT (1) | ATE318755T1 (de) |
DE (1) | DE60303783T2 (de) |
ES (1) | ES2264299B1 (de) |
Families Citing this family (71)
Publication number | Priority date | Publication date | Assignee | Title |
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ES2279664B1 (es) * | 2004-12-30 | 2008-08-01 | Airbus España S.L. | Dispositivo de proteccion contra descargas electricas en aeronaves. |
WO2007039650A1 (es) * | 2005-09-29 | 2007-04-12 | Airbus España, S.L. | Método de protección de depósitos de combustible fabricados con materiales compuestos contra descargas eléctricas |
US7886439B2 (en) * | 2005-12-15 | 2011-02-15 | The Boeing Company | Ground stud installation on composite structures for electrostatic charges |
US7576966B2 (en) * | 2006-02-23 | 2009-08-18 | The Boeing Company | Method and system for electrical bonding of fuel tank penetrations |
US7561402B2 (en) * | 2006-02-24 | 2009-07-14 | The Boeing Company | Gap lightning surface protection of composite structures |
US7695226B2 (en) * | 2006-09-21 | 2010-04-13 | Alcoa Global Fasteners, Inc. | High performance sleeved interference fasteners for composite applications |
US7898785B2 (en) * | 2006-12-07 | 2011-03-01 | The Boeing Company | Lightning protection system for an aircraft composite structure |
US7599164B2 (en) * | 2006-12-07 | 2009-10-06 | The Boeing Company | Lightning protection system for aircraft composite structure |
US7738236B2 (en) * | 2007-01-12 | 2010-06-15 | The Boeing Company | Light weight system for lightning protection of nonconductive aircraft panels |
DE102007003276B4 (de) * | 2007-01-23 | 2013-11-28 | Airbus Operations Gmbh | Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind |
US7966711B2 (en) | 2007-08-14 | 2011-06-28 | The Boeing Company | Method and apparatus for fastening components using a composite two-piece fastening system |
US8393068B2 (en) * | 2007-11-06 | 2013-03-12 | The Boeing Company | Method and apparatus for assembling composite structures |
FR2924686B1 (fr) | 2007-12-11 | 2010-05-14 | Airbus France | Systeme parafoudre et aeronef comportant un tel systeme. |
FR2924685B1 (fr) * | 2007-12-11 | 2010-03-19 | Airbus France | Systeme parafoudre et aeronef comportant un tel systeme. |
JP5055178B2 (ja) * | 2008-03-24 | 2012-10-24 | 三菱重工業株式会社 | 航空機組立品 |
GB0808524D0 (en) * | 2008-05-12 | 2008-06-18 | Magnomatics Ltd | Magnetic pole-piece structure |
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 |
FR2933378B1 (fr) * | 2008-07-04 | 2010-08-27 | Airbus France | Procede de montage d'une antenne sur un aeronef, et aeronef equipe d'au moins une antenne montee suivant ce procede |
US10537915B2 (en) | 2008-09-15 | 2020-01-21 | The Boeing Company | Contaminant resistant coating fabrication structure and method |
US10188103B2 (en) | 2008-09-15 | 2019-01-29 | The Boeing Company | Antimicrobial coating fabrication method and structure |
WO2010037991A1 (en) * | 2008-10-03 | 2010-04-08 | Short Brothers Plc | Fibre reinforced composite structures and method of manufacture |
US7897249B2 (en) * | 2008-10-07 | 2011-03-01 | The Boeing Company | Composite material structure with interlayer electrical conductance |
FR2939954B1 (fr) * | 2008-12-15 | 2013-01-25 | Eads Europ Aeronautic Defence | Structure en materiau composite protegee des effets de la foudre. |
US8231080B2 (en) * | 2009-02-26 | 2012-07-31 | The Boeing Company | Distributing power in systems having a composite structure |
ES2376323B1 (es) * | 2009-02-27 | 2013-01-24 | Airbus Operations, S.L. | Mejora de la protección contra impacto directo de rayos en zonas remachadas de paneles en cfrp. |
US8305727B2 (en) | 2009-03-09 | 2012-11-06 | Airbus Operations Limited | Aircraft joint and bonding lead |
US8400749B2 (en) | 2009-03-09 | 2013-03-19 | Airbus Operations Limited | Aircraft joint and bonding lead |
GB0904006D0 (en) | 2009-03-09 | 2009-04-22 | Airbus Uk Ltd | Bonding lead |
JP5237170B2 (ja) * | 2009-03-30 | 2013-07-17 | 三菱重工業株式会社 | 複合材タンク、翼、および、複合材タンクの製造方法 |
US9562556B2 (en) | 2009-04-03 | 2017-02-07 | Arconic Inc. | Fasteners with conforming sleeves |
US8322958B2 (en) * | 2009-04-03 | 2012-12-04 | Alcoa Inc. | Fasteners with conforming sleeves |
JP5438837B2 (ja) * | 2009-10-22 | 2014-03-12 | アルコア インコーポレイテッド | 電気伝導性を向上させたスリーブ付ファスナ及びその作製方法 |
US8264215B1 (en) * | 2009-12-10 | 2012-09-11 | The Boeing Company | Onboard electrical current sensing system |
ES2396296B1 (es) | 2010-04-30 | 2014-02-06 | Airbus Operations, S.L. | Dispositivo para la instalación de componentes conductores en estructuras. |
ES2396508B1 (es) * | 2010-10-13 | 2014-02-12 | Airbus Operations, S.L. | Sistema de proteccion contra rayos para tapas de acceso en aeronaves. |
US9802714B2 (en) * | 2010-12-03 | 2017-10-31 | The Boeing Company | Electric charge dissipation system for aircraft |
ES2402466B1 (es) * | 2010-12-14 | 2014-03-13 | Airbus Operations, S.L. | Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave. |
JP5615165B2 (ja) * | 2010-12-27 | 2014-10-29 | 三菱重工業株式会社 | 複合材パネル構造体及びその製造方法 |
JP5473892B2 (ja) * | 2010-12-28 | 2014-04-16 | 三菱航空機株式会社 | 耐雷ファスナ、航空機 |
WO2012107741A1 (en) | 2011-02-10 | 2012-08-16 | Airbus Operations Limited | Cap for forming sealed cavity around fastener |
JP5751871B2 (ja) * | 2011-03-10 | 2015-07-22 | 三菱重工業株式会社 | 燃料タンク |
DE102011014819A1 (de) * | 2011-03-23 | 2012-09-27 | Airbus Operations Gmbh | Befestigungsvorrichtung und Verfahren zur Herstellung einer Befestigungsvorrichtung |
DE102011112518B4 (de) | 2011-05-27 | 2020-01-09 | Airbus Defence and Space GmbH | Verfahren zur Herstellung einer Oberflächenstruktur mit Blitzschutz sowie Fahrzeugbauteilherstellverfahren |
US9007739B2 (en) | 2011-08-25 | 2015-04-14 | Lord Corporation | Lightning strike protection system |
RU2475425C1 (ru) * | 2011-10-06 | 2013-02-20 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Устройство металлизации корпуса изделия |
DE102012001859B4 (de) * | 2012-02-01 | 2015-04-23 | Daimler Ag | Verbindungsanordnung und Verfahren zum Verbinden wenigstens eines ersten Bauteils aus einem kohlefaserverstärkten Verbundwerkstoff mit wenigstens einem zweiten Bauteil |
US9481012B2 (en) * | 2012-05-23 | 2016-11-01 | The Boeing Company | Method of filling voids around countersunk fastener heads |
CN102795342A (zh) * | 2012-08-28 | 2012-11-28 | 中航工业三五一厂 | 一种飞机外挂辅助油箱主梁结构 |
EP2730508B1 (de) * | 2012-11-12 | 2016-09-14 | Airbus Operations GmbH | Auskleidungs-/Beplankungstafel und Verfahren zum Messen des elektrischen Bindewiderstandes einer Auskleidungs-/Beplankungstafel |
US9422066B2 (en) | 2013-03-15 | 2016-08-23 | United Technologies Corporation | Grounding sleeve |
JP6267976B2 (ja) * | 2014-01-27 | 2018-01-24 | 三菱航空機株式会社 | 航空機の耐雷適合性の試験対象の決定方法、および耐雷適合性証明方法 |
US9759246B2 (en) | 2014-08-25 | 2017-09-12 | Arconic Inc. | Textured sleeves for fasteners |
BR112017005059A2 (pt) | 2014-09-17 | 2017-12-05 | Arconic Inc | fixadores com elementos de pino revestidos e texturizados |
EP3194799A1 (de) | 2014-09-17 | 2017-07-26 | Arconic Inc. | Befestigungselemente mit zweischichtigen tiefenunterlegscheiben |
US9939004B2 (en) | 2014-09-17 | 2018-04-10 | Arconic Inc | Coated fasteners with conforming seals |
US9669942B2 (en) | 2015-04-10 | 2017-06-06 | The Boeing Company | Lightning damage resistant aircraft skin fasteners |
US9784132B2 (en) | 2015-04-20 | 2017-10-10 | Pratt & Whitney Canada Corp. | Voltage discharge channelling assembly for a gas turbine engine |
US10878139B2 (en) * | 2015-07-27 | 2020-12-29 | The Boeing Company | Composite joint optimization |
US9912137B2 (en) * | 2015-10-05 | 2018-03-06 | The Boeing Company | Methods for diverting lightning current from skin fasteners in composite, non-metallic structures |
JP6620020B2 (ja) * | 2016-01-06 | 2019-12-11 | 川崎重工業株式会社 | 複合部材 |
US10457411B2 (en) * | 2016-06-17 | 2019-10-29 | Goodrich Corporation | Lightning strike dispersion for composite aircraft structures |
DE102016215457A1 (de) | 2016-08-18 | 2018-02-22 | Airbus Operations Gmbh | Kontaktvorrichtung mit gewölbtem Kontaktelementsegment |
JP7161989B2 (ja) * | 2016-09-27 | 2022-10-27 | スリーエム イノベイティブ プロパティズ カンパニー | 保護フィルム |
EP3555488B1 (de) | 2016-12-13 | 2023-04-12 | Howmet Aerospace Inc. | Reduzierte elektromagnetische signatur von konformen konischen dichtungsbefestigungssystemen |
CN108045557A (zh) * | 2017-12-15 | 2018-05-18 | 惠阳航空螺旋桨有限责任公司 | 一种螺旋桨整流罩 |
US11038334B2 (en) * | 2019-01-14 | 2021-06-15 | The Boeing Company | Aircraft wing composite ribs having electrical grounding paths |
CN110047563B (zh) * | 2019-03-19 | 2021-10-26 | 首钢集团有限公司 | 一种复合材料雷击损伤模拟方法及装置 |
US11181137B2 (en) * | 2019-05-20 | 2021-11-23 | The Boeing Company | Fastener systems and assemblies for coupling a part to a composite structure, and related methods |
LU102368B1 (en) | 2020-12-31 | 2022-06-30 | Luxembourg Inst Science & Tech List | Lightning strike protection material and Structure |
CN114180083B (zh) * | 2021-11-19 | 2023-09-01 | 中国直升机设计研究所 | 一种利用铜杯实现的复合材料结构件之间导电处理方法 |
GB2620563A (en) * | 2022-07-07 | 2024-01-17 | Airbus Operations Ltd | Structure with lightning-strike protection layer |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3755713A (en) * | 1972-07-25 | 1973-08-28 | Boeing Co | Electrically conductive surface for aircraft |
US3989984A (en) * | 1975-07-11 | 1976-11-02 | Mcdonnell Douglas Corporation | Aircraft lightning protection means |
US4502092A (en) * | 1982-09-30 | 1985-02-26 | The Boeing Company | Integral lightning protection system for composite aircraft skins |
WO1984001487A1 (en) * | 1982-09-30 | 1984-04-12 | Boeing Co | Integral lightning protection system for composite aircraft skins |
US4628402A (en) * | 1985-09-30 | 1986-12-09 | The Boeing Company | Lightning protection of fasteners in composite material |
US4755904A (en) * | 1986-06-06 | 1988-07-05 | The Boeing Company | Lightning protection system for conductive composite material structure |
US4839771A (en) * | 1987-12-04 | 1989-06-13 | The Boeing Company | Apparatus for providing a lightning protective vehicle surface |
ES2006356A6 (es) * | 1988-03-07 | 1989-04-16 | Const Aeronauticas Sa | Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones, particularmente depositos o tanques de combustible fabricados de materiales compuestos. |
GB9411006D0 (en) * | 1994-06-02 | 1994-07-20 | British Aerospace | Method of fastening composite aircraft skins |
US5698316A (en) * | 1996-10-07 | 1997-12-16 | The Boeing Company | Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps |
US6327132B1 (en) * | 1998-06-10 | 2001-12-04 | Aerospatiale Matra | Spark resistant structure, in particular for aircraft |
ES2162718A1 (es) * | 1998-07-29 | 2002-01-01 | Const Aeronauticas Sa | Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones. |
-
2003
- 2003-06-06 ES ES200301351A patent/ES2264299B1/es not_active Expired - Fee Related
- 2003-12-19 DE DE60303783T patent/DE60303783T2/de not_active Expired - Lifetime
- 2003-12-19 AT AT03380301T patent/ATE318755T1/de not_active IP Right Cessation
- 2003-12-19 EP EP03380301A patent/EP1484245B1/de not_active Expired - Lifetime
- 2003-12-22 US US10/743,279 patent/US7307825B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
ES2264299B1 (es) | 2007-11-16 |
DE60303783D1 (de) | 2006-04-27 |
ES2264299A1 (es) | 2006-12-16 |
US20040246651A1 (en) | 2004-12-09 |
EP1484245A1 (de) | 2004-12-08 |
US7307825B2 (en) | 2007-12-11 |
DE60303783T2 (de) | 2006-11-16 |
EP1484245B1 (de) | 2006-03-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |