DE69801752D1 - Funkensichere struktur, insbesondere für flugzeuge - Google Patents

Funkensichere struktur, insbesondere für flugzeuge

Info

Publication number
DE69801752D1
DE69801752D1 DE69801752T DE69801752T DE69801752D1 DE 69801752 D1 DE69801752 D1 DE 69801752D1 DE 69801752 T DE69801752 T DE 69801752T DE 69801752 T DE69801752 T DE 69801752T DE 69801752 D1 DE69801752 D1 DE 69801752D1
Authority
DE
Germany
Prior art keywords
airplanes
spark
free structure
free
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
Application number
DE69801752T
Other languages
English (en)
Other versions
DE69801752T2 (de
Inventor
Luc Andrivet
Jean-Pierre Avenet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of DE69801752D1 publication Critical patent/DE69801752D1/de
Publication of DE69801752T2 publication Critical patent/DE69801752T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/02Lightning protectors; Static dischargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Elimination Of Static Electricity (AREA)
  • Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)
  • Conductive Materials (AREA)
  • Laminated Bodies (AREA)
DE69801752T 1997-06-20 1998-06-10 Funkensichere struktur, insbesondere für flugzeuge Expired - Lifetime DE69801752T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9707696A FR2765066B1 (fr) 1997-06-20 1997-06-20 Structure anti-etincelage, notamment pour aeronef
PCT/FR1998/001182 WO1998058840A1 (fr) 1997-06-20 1998-06-10 Structure anti-etincelage, notamment pour aeronef

Publications (2)

Publication Number Publication Date
DE69801752D1 true DE69801752D1 (de) 2001-10-25
DE69801752T2 DE69801752T2 (de) 2002-07-04

Family

ID=9508221

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69801752T Expired - Lifetime DE69801752T2 (de) 1997-06-20 1998-06-10 Funkensichere struktur, insbesondere für flugzeuge

Country Status (7)

Country Link
EP (1) EP0988228B1 (de)
AU (1) AU729113B2 (de)
CA (1) CA2285102C (de)
DE (1) DE69801752T2 (de)
ES (1) ES2163281T3 (de)
FR (1) FR2765066B1 (de)
WO (1) WO1998058840A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
ES2163951B1 (es) * 1998-07-29 2003-05-16 Airbus Espana Sl Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones.
ES2279664B1 (es) * 2004-12-30 2008-08-01 Airbus España S.L. Dispositivo de proteccion contra descargas electricas en aeronaves.
FR2903733B1 (fr) 2006-07-12 2011-03-04 Airbus France Turbomoteur pour aeronef.
FR2924687B1 (fr) 2007-12-11 2010-05-07 Airbus France Systeme parafoudre et aeronef comportant un tel systeme
DE102012202053A1 (de) 2012-02-10 2013-08-14 Airbus Operations Gmbh Verbindungsanordnung sowie Verfahren
WO2014148963A1 (en) * 2013-03-22 2014-09-25 Saab Ab A method for joining a first composite structure to at least a second structure and a mechanical and/or electrical joint
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
US9912137B2 (en) * 2015-10-05 2018-03-06 The Boeing Company Methods for diverting lightning current from skin fasteners in composite, non-metallic structures
US10457411B2 (en) * 2016-06-17 2019-10-29 Goodrich Corporation Lightning strike dispersion for composite aircraft structures
US10640232B2 (en) * 2016-12-20 2020-05-05 The Boeing Company Conductive fastening system for composite structures

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3755713A (en) * 1972-07-25 1973-08-28 Boeing Co Electrically conductive surface for aircraft
US4186237A (en) * 1975-03-17 1980-01-29 Vereinigte Flugtechnische Werke-Fokker Gmbh Multi-component protective covering for construction parts designed to protect against the effects of lightning
US3989984A (en) * 1975-07-11 1976-11-02 Mcdonnell Douglas Corporation Aircraft lightning protection means
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
US4912594A (en) * 1986-11-03 1990-03-27 The Boeing Company Integral lightning protection repair system and method for its use
GB9215827D0 (en) * 1992-07-24 1992-09-09 British Aerospace A lightning shield

Also Published As

Publication number Publication date
DE69801752T2 (de) 2002-07-04
AU7925198A (en) 1999-01-04
EP0988228A1 (de) 2000-03-29
CA2285102A1 (fr) 1998-12-30
CA2285102C (fr) 2005-10-18
EP0988228B1 (de) 2001-09-19
FR2765066B1 (fr) 1999-08-20
ES2163281T3 (es) 2002-01-16
AU729113B2 (en) 2001-01-25
WO1998058840A1 (fr) 1998-12-30
FR2765066A1 (fr) 1998-12-24

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Legal Events

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8364 No opposition during term of opposition