DE69508899D1 - Verbundmaterial und Verbundelement mit dadurch sichergestellter elektrischer Kontinuität, dessen Herstellungsverfahren und dessen Verwendung in Flugzeugindustrie - Google Patents

Verbundmaterial und Verbundelement mit dadurch sichergestellter elektrischer Kontinuität, dessen Herstellungsverfahren und dessen Verwendung in Flugzeugindustrie

Info

Publication number
DE69508899D1
DE69508899D1 DE69508899T DE69508899T DE69508899D1 DE 69508899 D1 DE69508899 D1 DE 69508899D1 DE 69508899 T DE69508899 T DE 69508899T DE 69508899 T DE69508899 T DE 69508899T DE 69508899 D1 DE69508899 D1 DE 69508899D1
Authority
DE
Germany
Prior art keywords
manufacturing process
electrical continuity
aircraft industry
composite
composite material
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
Application number
DE69508899T
Other languages
English (en)
Other versions
DE69508899T2 (de
Inventor
Rene Jerome Poggi
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Application granted granted Critical
Publication of DE69508899D1 publication Critical patent/DE69508899D1/de
Publication of DE69508899T2 publication Critical patent/DE69508899T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05F—STATIC ELECTRICITY; NATURALLY-OCCURRING ELECTRICITY
    • H05F3/00—Carrying-off electrostatic charges
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12444—Embodying fibers interengaged or between layers [e.g., paper, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12556—Organic component
    • Y10T428/12569—Synthetic resin

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
DE69508899T 1994-12-16 1995-12-12 Verbundmaterial und Verbundelement mit dadurch sichergestellter elektrischer Kontinuität, dessen Herstellungsverfahren und dessen Verwendung in Flugzeugindustrie Expired - Fee Related DE69508899T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9415194A FR2728395A1 (fr) 1994-12-16 1994-12-16 Element en materiau composite avec assemblage(s) de continuite electrique a travers l'element, son procede de fabrication et son utilisation en aeronautique

Publications (2)

Publication Number Publication Date
DE69508899D1 true DE69508899D1 (de) 1999-05-12
DE69508899T2 DE69508899T2 (de) 1999-12-02

Family

ID=9469884

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69508899T Expired - Fee Related DE69508899T2 (de) 1994-12-16 1995-12-12 Verbundmaterial und Verbundelement mit dadurch sichergestellter elektrischer Kontinuität, dessen Herstellungsverfahren und dessen Verwendung in Flugzeugindustrie

Country Status (4)

Country Link
US (2) US5863667A (de)
EP (1) EP0717585B1 (de)
DE (1) DE69508899T2 (de)
FR (1) FR2728395A1 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040035070A1 (en) * 2002-06-21 2004-02-26 Chen Kuei Yung Wang Economical impact resistant compression molded door
US7554785B2 (en) * 2004-03-23 2009-06-30 The Boeing Company Lightning damage protection for composite aircraft
ES2255454B1 (es) * 2004-12-15 2007-07-01 Gamesa Eolica, S.A. Sistema pararrayos para pala de aerogenerador.
US7157663B1 (en) 2005-10-12 2007-01-02 The Boeing Company Conducting-fiber deicing systems and methods
US20070080481A1 (en) * 2005-10-12 2007-04-12 The Boeing Company Apparatus and methods for fabrication of composite components
DE102007003277B4 (de) * 2007-01-23 2012-08-02 Airbus Operations Gmbh Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen
FR2914622B1 (fr) * 2007-04-04 2009-05-15 Airbus France Sas Aeronef comprenant une structure assurant les fonctions structurale et electrique
DE102007025230A1 (de) * 2007-05-31 2008-12-04 Robert Bosch Gmbh Verfahren zum Ableiten eines elektrischen Überspannungspotentials
US7628879B2 (en) * 2007-08-23 2009-12-08 The Boeing Company Conductive scrim embedded structural adhesive films
FR2940927B1 (fr) * 2009-01-09 2013-01-04 Eads Europ Aeronautic Defence Structure en materiau composite protegee des effets de la foudre
ES2371623B1 (es) * 2009-12-11 2012-11-22 Airbus Operations S.L. Proceso de compactación de una pieza de materiales compuestos.
DE102014004118A1 (de) 2014-03-24 2015-09-24 Airbus Operations Gmbh Neuartiges blitzschutzmaterial für faerverbundbauteile
US9909197B2 (en) * 2014-12-22 2018-03-06 Semes Co., Ltd. Supporting unit and substrate treating apparatus including the same
FR3062327B1 (fr) * 2017-01-30 2019-04-19 Safran Aircraft Engines Procede pour le decollement d'un element metallique colle a un element en materiau composite
PT3581796T (pt) * 2018-06-14 2022-05-04 Siemens Gamesa Renewable Energy As Interface de condutividade escalonada

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3347978A (en) * 1963-06-03 1967-10-17 Lockheed Aircraft Corp Electrically conductive joints and gaskets
US3906308A (en) * 1973-09-27 1975-09-16 Mc Donnell Douglas Corp Aircraft lightning protection system
US3989984A (en) * 1975-07-11 1976-11-02 Mcdonnell Douglas Corporation Aircraft lightning protection means
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
GB2121598A (en) * 1982-04-27 1983-12-21 Marconi Co Ltd Sealing optoelectronic packages
US4529836A (en) * 1983-07-15 1985-07-16 Sperry Corporation Stress absorption matrix
US4576776A (en) * 1984-08-13 1986-03-18 Boeing Commercial Airplane Company Flow forming of composite material
FR2578377B1 (fr) * 1984-12-26 1988-07-01 Aerospatiale Element chauffant de dispositif de degivrage d'une structure alaire, dispositif et son procede d'obtention
JPS62220269A (ja) * 1986-03-20 1987-09-28 Tdk Corp 半田付け方法
US4965408A (en) * 1989-02-01 1990-10-23 Borden, Inc. Composite sheet material for electromagnetic radiation shielding
US4977296A (en) * 1989-02-23 1990-12-11 Hemming Leland H Radio frequency shielding tape
US5250342A (en) * 1989-05-24 1993-10-05 United Technologies Corporation Composite EMI shield having clean, highly conductive surfaces for conductive bonding
US5239125A (en) * 1990-06-19 1993-08-24 The United States Of America As Represented By The Secretary Of The Army EMI/RFI shield
JP2526820Y2 (ja) * 1991-05-24 1997-02-26 北川工業株式会社 電磁波シールド用編物
US5595801A (en) * 1991-07-30 1997-01-21 International Paper Company Laminated shielding material and method for shielding an enclosure therewith
FR2687195B1 (fr) * 1992-02-12 1995-07-07 Eurocopter France Organe d'assemblage a tete fraisee, tel qu'un rivet, pour l'assemblage de pieces en materiau composite munies de revetements electriquement conducteurs, et structure obtenue par cet assemblage.
USH1306H (en) * 1993-01-21 1994-05-03 The United States Of America As Represented By The Secretary Of The Army Method of using an improved solder to bridge a nonmetallic gap between metallic surfaces, said improved solder, and an improved solder connection to bridge a nonmetallic gap between metallic surfaces
US5346775A (en) * 1993-02-22 1994-09-13 At&T Laboratories Article comprising solder with improved mechanical properties

Also Published As

Publication number Publication date
FR2728395A1 (fr) 1996-06-21
US5863667A (en) 1999-01-26
EP0717585B1 (de) 1999-04-07
DE69508899T2 (de) 1999-12-02
EP0717585A1 (de) 1996-06-19
US6126061A (en) 2000-10-03
FR2728395B1 (de) 1997-02-21

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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