ES2162718A1 - Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones. - Google Patents
Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones.Info
- Publication number
- ES2162718A1 ES2162718A1 ES009801611A ES9801611A ES2162718A1 ES 2162718 A1 ES2162718 A1 ES 2162718A1 ES 009801611 A ES009801611 A ES 009801611A ES 9801611 A ES9801611 A ES 9801611A ES 2162718 A1 ES2162718 A1 ES 2162718A1
- Authority
- ES
- Spain
- Prior art keywords
- fastening elements
- protection system
- covering
- metal mesh
- lightning protection
- 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.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title abstract 2
- 239000002184 metal Substances 0.000 abstract 2
- 238000005553 drilling Methods 0.000 abstract 1
- 239000002828 fuel tank Substances 0.000 abstract 1
- 238000003780 insertion Methods 0.000 abstract 1
- 230000037431 insertion Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 239000011810 insulating material Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Bolts, Nuts, And Washers (AREA)
Abstract
Un sistema de protección contra descargas eléctricas, especialmente rayos, de componentes estructurales de aviones, que comprende una malla metálica (1) que cubre la cara exterior de toda la superficie expuesta a impacto de rayos; una pieza o arandela (2) de material aislante que se coloca en el interior de la pieza interna (P.I.) a sujetar; una tira de malla metálica (3) ubicada en el exterior de la hilera de elementos sujetadores (R), cuya introducción se realiza durante el mismo proceso de curado del componente estructural, efectuándose posteriormente el taladrado y avellanado de dicho componente para la instalación de los elementos sujetadores (R); y un acabado orgánico (A.O.) que cubre toda la estructura, incluida la cabeza de los elementos sujetadores (R). El invento es aplicable a tanques de combustible fabricados de materiales compuestos.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009801611A ES2162718A1 (es) | 1998-07-29 | 1998-07-29 | Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones. |
EP99500129A EP0976653A1 (en) | 1998-07-29 | 1999-07-28 | Lightning protection system for composite aircraft structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009801611A ES2162718A1 (es) | 1998-07-29 | 1998-07-29 | Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2162718A1 true ES2162718A1 (es) | 2002-01-01 |
Family
ID=8304691
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES009801611A Pending ES2162718A1 (es) | 1998-07-29 | 1998-07-29 | Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones. |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0976653A1 (es) |
ES (1) | ES2162718A1 (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2264299A1 (es) * | 2003-06-06 | 2006-12-16 | Airbus España S.L. | Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica. |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10200564B4 (de) * | 2002-01-09 | 2007-08-09 | Eads Deutschland Gmbh | Blitzschutzeinrichtung an faserverstärkten Bauteilen für mittels lösbaren Bolzenverbindungen entfernbare Verschluss-Deckel |
FR2866991B1 (fr) | 2004-02-26 | 2006-05-19 | Airbus France | Dispositif de retour d'alimentation electrique pour equipements avioniques |
GB0417472D0 (en) | 2004-08-05 | 2004-09-08 | Airbus Uk Ltd | Fuel tank system |
GB0417473D0 (en) | 2004-08-05 | 2004-09-08 | Airbus Uk Ltd | Fuel tank |
US20070129902A1 (en) * | 2005-08-05 | 2007-06-07 | Orbell Richard | Electronic module mounting means |
JP4995823B2 (ja) * | 2005-09-29 | 2012-08-08 | エアバス オペレーションズ、ソシエダ リミタダ | 複合材料でつくられた燃料タンクを放電から保護する方法 |
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. |
US10457411B2 (en) * | 2016-06-17 | 2019-10-29 | Goodrich Corporation | Lightning strike dispersion for composite aircraft structures |
WO2018063970A1 (en) | 2016-09-27 | 2018-04-05 | 3M Innovative Properties Company | Protection film |
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 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0248122A2 (en) * | 1986-06-06 | 1987-12-09 | The Boeing Company | Lightning protection system for conductive composite material structure |
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. |
GB2212580A (en) * | 1987-11-14 | 1989-07-26 | British Aerospace | Anti-lightning fastener |
FR2626629A1 (fr) * | 1988-01-29 | 1989-08-04 | Aerospatiale | Procede et dispositif de fixation d'elements de structures d'aeronefs protegees contre la foudre, et outil pour la mise en oeuvre de ce procede |
EP0685389A1 (en) * | 1994-06-02 | 1995-12-06 | British Aerospace Public Limited Company | Method of fastening composite aircraft skins |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3775713A (en) | 1972-11-03 | 1973-11-27 | Westinghouse Electric Corp | Circuit breaker with externally operable means for manual adjustment and manual tripping |
US4479163A (en) | 1982-09-30 | 1984-10-23 | The Boeing Company | Integral lightning protection system for composite aircraft skins |
GB8504819D0 (en) | 1985-02-25 | 1985-03-27 | Ici Plc | Extraction of metal values |
US4657902A (en) | 1985-03-25 | 1987-04-14 | The Rockefeller University | Therapeutic use of tin mesoporphyrin |
FR2765066B1 (fr) * | 1997-06-20 | 1999-08-20 | Aerospatiale | Structure anti-etincelage, notamment pour aeronef |
-
1998
- 1998-07-29 ES ES009801611A patent/ES2162718A1/es active Pending
-
1999
- 1999-07-28 EP EP99500129A patent/EP0976653A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0248122A2 (en) * | 1986-06-06 | 1987-12-09 | The Boeing Company | Lightning protection system for conductive composite material structure |
GB2212580A (en) * | 1987-11-14 | 1989-07-26 | British Aerospace | Anti-lightning fastener |
FR2626629A1 (fr) * | 1988-01-29 | 1989-08-04 | Aerospatiale | Procede et dispositif de fixation d'elements de structures d'aeronefs protegees contre la foudre, et outil pour la mise en oeuvre de ce procede |
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. |
EP0685389A1 (en) * | 1994-06-02 | 1995-12-06 | British Aerospace Public Limited Company | Method of fastening composite aircraft skins |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2264299A1 (es) * | 2003-06-06 | 2006-12-16 | Airbus España S.L. | Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica. |
Also Published As
Publication number | Publication date |
---|---|
EP0976653A1 (en) | 2000-02-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EC2A | Search report published |
Date of ref document: 20020101 Kind code of ref document: A1 Effective date: 20020101 |
|
FC2A | Grant refused |
Effective date: 20030303 |