DE68907396D1 - Ueberleitungsmittel fuer die kontinuierliche elektrische leitung bei faserverbundverbindungen. - Google Patents
Ueberleitungsmittel fuer die kontinuierliche elektrische leitung bei faserverbundverbindungen.Info
- Publication number
- DE68907396D1 DE68907396D1 DE8989630201T DE68907396T DE68907396D1 DE 68907396 D1 DE68907396 D1 DE 68907396D1 DE 8989630201 T DE8989630201 T DE 8989630201T DE 68907396 T DE68907396 T DE 68907396T DE 68907396 D1 DE68907396 D1 DE 68907396D1
- Authority
- DE
- Germany
- Prior art keywords
- transmitter
- fiber composite
- electrical wiring
- continuous electrical
- composite connections
- 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 - Fee Related
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000009429 electrical wiring Methods 0.000 title 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
- H01R4/58—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
- H01R4/64—Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/277,382 US4888451A (en) | 1988-11-29 | 1988-11-29 | Electrical continuity means for composite joints |
Publications (2)
Publication Number | Publication Date |
---|---|
DE68907396D1 true DE68907396D1 (de) | 1993-08-05 |
DE68907396T2 DE68907396T2 (de) | 1993-10-14 |
Family
ID=23060618
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE89630201T Expired - Fee Related DE68907396T2 (de) | 1988-11-29 | 1989-11-09 | Überleitungsmittel für die kontinuierliche elektrische Leitung bei Faserverbundverbindungen. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4888451A (de) |
EP (1) | EP0371905B1 (de) |
JP (1) | JP2940682B2 (de) |
CA (1) | CA1316232C (de) |
DE (1) | DE68907396T2 (de) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4037119A1 (de) * | 1990-11-22 | 1992-05-27 | Messerschmitt Boelkow Blohm | Anordnung zum abdichten einer trenn- oder verbindungsfuge zwischen zwei bauteilen im wesentlichen aus kunststoff |
GB9107766D0 (en) * | 1991-04-12 | 1991-06-05 | Short Brothers Plc | A structural component |
JPH0664367U (ja) * | 1992-06-09 | 1994-09-09 | 東洋電機製造株式会社 | 積層導体の電気回路 |
US5372336A (en) * | 1993-04-05 | 1994-12-13 | Grumman Aerospace Corporation | Folding wing assembly |
GB9411006D0 (en) * | 1994-06-02 | 1994-07-20 | British Aerospace | Method of fastening composite aircraft skins |
US6327132B1 (en) * | 1998-06-10 | 2001-12-04 | Aerospatiale Matra | Spark resistant structure, in particular for aircraft |
DE602004002482T2 (de) * | 2003-05-30 | 2007-02-01 | Bae Systems Plc | Verbundstruktur-blitzschlagschutz |
JP5610662B2 (ja) * | 2003-09-30 | 2014-10-22 | ザ・ボーイング・カンパニーTheBoeing Company | 保護シート |
US7554785B2 (en) * | 2004-03-23 | 2009-06-30 | The Boeing Company | Lightning damage protection for composite aircraft |
JP4786426B2 (ja) * | 2005-10-06 | 2011-10-05 | 三菱重工業株式会社 | ファスナ |
GB0525896D0 (en) | 2005-12-20 | 2006-02-01 | Airbus Uk Ltd | A joint for use in aircraft construction |
US7790294B2 (en) * | 2006-07-05 | 2010-09-07 | Lockheed Martin Corporation | System, method, and apparatus for three-dimensional woven metal preform structural joint |
FR2905739B1 (fr) * | 2006-09-08 | 2008-11-07 | Airbus France Sas | Assemblage de panneaux et procede de montage d'un assemblage de panneaux |
FR2915458B1 (fr) * | 2007-04-25 | 2010-01-01 | Airbus France | Assemblage de panneaux de fuselage d'un avion |
DE102007052098A1 (de) * | 2007-10-31 | 2009-05-14 | Airbus Deutschland Gmbh | Querstoßlasche zur Schaffung einer Rumpfzelle sowie Verfahren zum Verbinden von zwei insbesondere gewickelten CFK-Rumpfsektionen |
GB0805268D0 (en) * | 2008-03-25 | 2008-04-30 | Airbus Uk Ltd | Composite joint protection |
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 |
US8282042B2 (en) * | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
FR2947523B1 (fr) * | 2009-07-03 | 2011-07-22 | Airbus Operations Sas | Element de fuselage comportant un troncon de fuselage et des moyens de jonction |
GB201004757D0 (en) * | 2010-03-23 | 2010-05-05 | Airbus Operations Ltd | Joint |
ES2396881B1 (es) * | 2010-11-30 | 2014-01-29 | Airbus Operations, S.L. | Disposición de interfaz entre dos componentes de una estructura de una aeronave usando una pieza de sellado. |
JP5669635B2 (ja) * | 2011-03-14 | 2015-02-12 | 三菱航空機株式会社 | 機体構成部材の連結構造 |
DE102011107624A1 (de) | 2011-06-30 | 2013-01-03 | Eads Deutschland Gmbh | Verbindungsanordnung zur aerodynamisch glatten Verbindung zweier Profilelemente, Verfahren zu deren Fertigung und Vorrichtung zur Durchführung des Verfahrens |
GB201200912D0 (en) * | 2012-01-19 | 2012-02-29 | Airbus Operations Ltd | Fastener receptacle strip |
US8816221B2 (en) * | 2012-02-29 | 2014-08-26 | Hamilton Sundstrand Corporation | Low electrical resistance bond |
FR2994584B1 (fr) * | 2012-08-17 | 2014-08-29 | Snecma | Carter en aluminium d'une turbomachine |
US9643734B2 (en) * | 2013-03-18 | 2017-05-09 | The Boeing Company | Electromagnetic energy surface protection |
US9676469B2 (en) * | 2014-04-10 | 2017-06-13 | Lockheed Martin Corporation | System and method for fastening structures |
JP6139582B2 (ja) | 2015-02-23 | 2017-05-31 | 株式会社Subaru | 航空機用構造体、航空機用構造体の製造方法及び航空機用構造体の設計情報の作成方法 |
GB2545655A (en) * | 2015-12-18 | 2017-06-28 | Airbus Operations Ltd | A structure formed from composite material |
EP3299297B1 (de) | 2016-09-27 | 2018-12-12 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügelflugzeug mit strukturanordnung mit einer elektrisch leitenden verbindung |
US10124745B2 (en) * | 2017-01-06 | 2018-11-13 | GM Global Technology Operations LLC | Joining arrangement and method with molded stake and aperture |
JP6778221B2 (ja) * | 2018-01-15 | 2020-10-28 | 株式会社Subaru | 締結構造 |
US11383820B2 (en) * | 2019-06-11 | 2022-07-12 | The Boeing Company | Aerodynamic surface lap splice |
DE102021105806B4 (de) | 2021-03-10 | 2024-04-11 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Aerodynamischer Profilkörper für Luftfahrzeuge |
GB2614720A (en) * | 2022-01-13 | 2023-07-19 | Airbus Operations Ltd | Lightning strike protection layer |
DE102023102200B3 (de) | 2023-01-31 | 2024-02-01 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Aerodynamischer Profilkörper für Luftfahrzeuge |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2125882A (en) * | 1937-03-17 | 1938-08-09 | Henry A Berliner | Aircraft construction |
US2274422A (en) * | 1940-01-20 | 1942-02-24 | Gen Electric | Electrical connection |
US3556591A (en) * | 1968-10-09 | 1971-01-19 | Anna L Medearis | Foot support |
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 |
JPS56165367U (de) * | 1980-05-12 | 1981-12-08 | ||
US4502092A (en) * | 1982-09-30 | 1985-02-26 | The Boeing Company | Integral lightning protection system for composite aircraft skins |
US4478915A (en) * | 1983-11-07 | 1984-10-23 | United Technologies Corporation | Corrosion resistant shim for electrically joining incompatible materials |
US4574325A (en) * | 1984-02-09 | 1986-03-04 | The Boeing Company | Lightning protection electrical circuit path for coupling between aircraft structures |
US4628402A (en) * | 1985-09-30 | 1986-12-09 | The Boeing Company | Lightning protection of fasteners in composite material |
US4789918A (en) * | 1986-11-03 | 1988-12-06 | The Boeing Company | Fastened lightning protection repair system and method for its use |
-
1988
- 1988-11-29 US US07/277,382 patent/US4888451A/en not_active Expired - Fee Related
-
1989
- 1989-09-22 CA CA000612671A patent/CA1316232C/en not_active Expired - Fee Related
- 1989-11-09 DE DE89630201T patent/DE68907396T2/de not_active Expired - Fee Related
- 1989-11-09 EP EP89630201A patent/EP0371905B1/de not_active Expired - Lifetime
- 1989-11-28 JP JP1308821A patent/JP2940682B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0371905A2 (de) | 1990-06-06 |
DE68907396T2 (de) | 1993-10-14 |
CA1316232C (en) | 1993-04-13 |
US4888451A (en) | 1989-12-19 |
EP0371905A3 (en) | 1990-08-29 |
EP0371905B1 (de) | 1993-06-30 |
JP2940682B2 (ja) | 1999-08-25 |
JPH02225200A (ja) | 1990-09-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |