DE69505620T2 - Funkensichere struktur, insbesondere für flugzeuge - Google Patents

Funkensichere struktur, insbesondere für flugzeuge

Info

Publication number
DE69505620T2
DE69505620T2 DE69505620T DE69505620T DE69505620T2 DE 69505620 T2 DE69505620 T2 DE 69505620T2 DE 69505620 T DE69505620 T DE 69505620T DE 69505620 T DE69505620 T DE 69505620T DE 69505620 T2 DE69505620 T2 DE 69505620T2
Authority
DE
Germany
Prior art keywords
spark
aircraft
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
DE69505620T
Other languages
English (en)
Other versions
DE69505620D1 (de
Inventor
Jean-Pierre Avenet
Pascal Gondot
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE69505620D1 publication Critical patent/DE69505620D1/de
Publication of DE69505620T2 publication Critical patent/DE69505620T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • F16B35/04—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
DE69505620T 1994-04-15 1995-04-13 Funkensichere struktur, insbesondere für flugzeuge Expired - Lifetime DE69505620T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9404507A FR2718706B1 (fr) 1994-04-15 1994-04-15 Structure anti-étincelage, notamment pour aéronef.
PCT/FR1995/000477 WO1995028319A1 (fr) 1994-04-15 1995-04-13 Structure anti-etincelage, notamment pour aeronef

Publications (2)

Publication Number Publication Date
DE69505620D1 DE69505620D1 (de) 1998-12-03
DE69505620T2 true DE69505620T2 (de) 1999-03-25

Family

ID=9462139

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69505620T Expired - Lifetime DE69505620T2 (de) 1994-04-15 1995-04-13 Funkensichere struktur, insbesondere für flugzeuge

Country Status (6)

Country Link
US (1) US5709356A (de)
EP (1) EP0702643B1 (de)
CA (1) CA2163624C (de)
DE (1) DE69505620T2 (de)
FR (1) FR2718706B1 (de)
WO (1) WO1995028319A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
SE516459C2 (sv) * 2000-11-24 2002-01-15 Saab Ericsson Space Ab Konstruktion och förfarande vid bärraket eller satellit
GB0117805D0 (en) * 2001-07-21 2001-09-12 Bae Systems Plc A method of securing composite elements together
US7303481B2 (en) * 2005-02-04 2007-12-04 Itt Manufacturing Enterprises, Inc. Electrically isolated actuator output shaft
US8398027B2 (en) * 2007-09-17 2013-03-19 The Boeing Company Method and apparatus for reinforcing composite structures
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.
JP5610758B2 (ja) * 2009-04-02 2014-10-22 三菱航空機株式会社 耐雷ファスナ、キャップ、耐雷ファスナの取り付け方法、航空機
JP5619446B2 (ja) 2010-03-23 2014-11-05 三菱重工業株式会社 キャップ、これを用いた締結構造およびこの締結構造を有する航空機
US8791375B2 (en) * 2010-12-16 2014-07-29 The Boeing Company Electrically conductive bushing connection to structure for current path
GB201101311D0 (en) * 2011-01-26 2011-03-09 Airbus Uk Ltd Fastener assembly
JP5931429B2 (ja) * 2011-12-20 2016-06-08 三菱航空機株式会社 耐雷ファスナ
EP2620360A1 (de) * 2012-01-24 2013-07-31 EADS Construcciones Aeronauticas, S.A. Brandschutzvorrichtung für ein Flugzeug
US9291187B2 (en) * 2013-05-20 2016-03-22 The Boeing Company Nut, washer and fastener head for electromagnetic effect protection
US9140288B2 (en) * 2014-01-09 2015-09-22 Hung-I Hsu Pipeline fastener
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
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
JP6461380B2 (ja) 2015-08-27 2019-01-30 アーコニック インコーポレイテッドＡｒｃｏｎｉｃ Ｉｎｃ． ファスナーのロック部材
US11234899B2 (en) * 2017-05-11 2022-02-01 Scalpal Llc Grasping facilitators and uses thereof and kits involving the same
US10385908B2 (en) * 2016-03-31 2019-08-20 The Boeing Company Conformal clearance fit fastener, fastener system, and method for composite structures
US10087975B2 (en) * 2016-04-28 2018-10-02 The Boeing Company Expandable, resin filled fastener, fastener system, and method for composite structures
US11969864B2 (en) 2017-05-11 2024-04-30 Scalpal Llc Multi-tier torque enhancer driver and/or receiver and method of using same
US20180339788A1 (en) * 2017-05-26 2018-11-29 Joe A. Garcia Protective cap and nut gauge for an aircraft fuel tank fastener system
CN110228596A (zh) * 2018-11-16 2019-09-13 熊秀 防雷紧固件及紧固方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2787185A (en) * 1953-06-29 1957-04-02 Boeing Co Expansion fastener with sealing liner
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
SU1042277A1 (ru) * 1981-03-04 1991-12-23 Предприятие П/Я В-2739 Панель
US4556591A (en) * 1981-09-25 1985-12-03 The Boeing Company Conductive bonded/bolted joint seals for composite aircraft
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
GB8628555D0 (en) * 1986-11-28 1987-01-07 British Aerospace Anti lightning strike fasteners
GB2212580B (en) * 1987-11-14 1992-03-25 British Aerospace Methods of fastening composite aircraft skins
US4839771A (en) * 1987-12-04 1989-06-13 The Boeing Company Apparatus for providing a lightning protective vehicle surface
US4905931A (en) * 1988-02-18 1990-03-06 The Boeing Company Arc suppression around fasteners
GB8828025D0 (en) * 1988-12-01 1989-01-05 Atomic Energy Authority Uk Screw fasteners for aeronautical use
GB8924231D0 (en) * 1989-10-27 1989-12-13 British Aerospace Carbon fibre composite structures
FR2668580B1 (fr) * 1990-10-30 1993-01-22 Aerospatiale Structure anti-etincelage, notamment pour aeronef.
US5314144A (en) * 1991-12-18 1994-05-24 Raytheon Company Thermally compensating insert fastener

Also Published As

Publication number Publication date
CA2163624A1 (fr) 1995-10-26
FR2718706A1 (fr) 1995-10-20
EP0702643B1 (de) 1998-10-28
FR2718706B1 (fr) 1996-06-14
WO1995028319A1 (fr) 1995-10-26
CA2163624C (fr) 2005-01-18
US5709356A (en) 1998-01-20
DE69505620D1 (de) 1998-12-03
EP0702643A1 (de) 1996-03-27

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Legal Events

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