FR2626629B1 - 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 - Google Patents

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

Info

Publication number
FR2626629B1
FR2626629B1 FR8801065A FR8801065A FR2626629B1 FR 2626629 B1 FR2626629 B1 FR 2626629B1 FR 8801065 A FR8801065 A FR 8801065A FR 8801065 A FR8801065 A FR 8801065A FR 2626629 B1 FR2626629 B1 FR 2626629B1
Authority
FR
France
Prior art keywords
tool
carrying
protected against
fixing elements
aircraft structures
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
FR8801065A
Other languages
English (en)
Other versions
FR2626629A1 (fr
Inventor
Bernard Jean-Francois Boime
Guy Forner
Jean-Luc Christian Mar Larcher
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
Priority to FR8801065A priority Critical patent/FR2626629B1/fr
Publication of FR2626629A1 publication Critical patent/FR2626629A1/fr
Application granted granted Critical
Publication of FR2626629B1 publication Critical patent/FR2626629B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • F16B33/00—Features common to bolt and nut
    • F16B33/004—Sealing; Insulation
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05F—STATIC ELECTRICITY; NATURALLY-OCCURRING ELECTRICITY
    • H05F3/00—Carrying-off electrostatic charges
    • H05F3/02—Carrying-off electrostatic charges by means of earthing connections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
FR8801065A 1988-01-29 1988-01-29 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 Expired - Lifetime FR2626629B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8801065A FR2626629B1 (fr) 1988-01-29 1988-01-29 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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8801065A FR2626629B1 (fr) 1988-01-29 1988-01-29 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

Publications (2)

Publication Number Publication Date
FR2626629A1 FR2626629A1 (fr) 1989-08-04
FR2626629B1 true FR2626629B1 (fr) 1990-03-09

Family

ID=9362772

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8801065A Expired - Lifetime FR2626629B1 (fr) 1988-01-29 1988-01-29 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

Country Status (1)

Country Link
FR (1) FR2626629B1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104364158A (zh) * 2012-05-31 2015-02-18 空中客车营运有限公司 可注射螺帽盖
CN104549905A (zh) * 2013-10-22 2015-04-29 波音公司 施用密封剂的设备和方法
CN105228905A (zh) * 2013-05-16 2016-01-06 空中客车营运有限公司 可注射螺帽

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Publication number Priority date Publication date Assignee Title
FR2677412B1 (fr) * 1991-06-05 1993-10-15 Aerospatiale Ste Nationale Indle Outillage pour le collage d'organes de revetement electriquement conducteurs dans les zones de fixation d'une piece en materiau composite.
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.
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.
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.
US7014143B2 (en) * 2002-10-11 2006-03-21 The Boeing Company Aircraft lightning strike protection and grounding technique
ES2279664B1 (es) * 2004-12-30 2008-08-01 Airbus España S.L. Dispositivo de proteccion contra descargas electricas en aeronaves.
EP2331320B1 (fr) 2008-10-03 2013-03-13 Short Brothers Plc Structures composites renforcées par des fibres et procédé de fabrication
JP5846587B2 (ja) * 2009-04-02 2016-01-20 三菱航空機株式会社 耐雷ファスナ、航空機、耐雷ファスナの取り付け方法
JP5535843B2 (ja) * 2010-09-14 2014-07-02 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
FR2971719B1 (fr) * 2011-02-22 2014-01-24 Dassault Aviat Dispositif d'enduction d'un objet saillant par un produit fluide, ensemble de distribution et de procede associes
GB2491799A (en) * 2011-03-03 2012-12-19 S & T Systems Ltd Locking of threaded fasteners
CN103635388A (zh) * 2011-04-28 2014-03-12 三菱重工业株式会社 盖以及利用该盖的固定结构部
DE102012202053A1 (de) * 2012-02-10 2013-08-14 Airbus Operations Gmbh Verbindungsanordnung sowie Verfahren
EP2986509B1 (fr) 2013-04-19 2018-05-30 Airbus Operations Limited Coiffe injectable
EP2986529B1 (fr) 2013-04-19 2017-08-02 Airbus Operations Limited Chapeau injectable
GB2516835B (en) 2013-07-31 2015-11-04 Airbus Operations Ltd Cap to accommodate washers
EP3036163B1 (fr) 2013-08-21 2019-09-04 Airbus Operations Limited Capuchon avec mastic d'étanchéité injecté
DE102014220202A1 (de) * 2014-10-06 2016-04-07 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Versiegelungshilfsmittel, Verbindungsmittel mit einer Versiegelung sowie Verfahren zum Versiegeln des Verbindungsmittels
US10035287B2 (en) * 2014-11-17 2018-07-31 The Boeing Company Method for sealing a fastener
GB2535518A (en) 2015-02-20 2016-08-24 Airbus Operations Ltd Cap with injected sealant
JP2016190627A (ja) * 2015-03-31 2016-11-10 三菱重工業株式会社 構造体製造装置、構造体製造方法、および構造体
GB2568890A (en) 2017-11-29 2019-06-05 Airbus Operations Ltd Spark containment cap
BE1027420B1 (nl) * 2019-07-04 2021-02-08 Unilin Bv Een verbindingssysteem

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710113A (en) * 1952-01-23 1955-06-07 Gen Dynamics Corp Seal construction
LU40701A1 (fr) * 1961-01-04 1961-12-11
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
US4349859A (en) * 1980-09-24 1982-09-14 Mcdonnell Douglas Corporation Shielded structural or containment member
DE3278383D1 (en) * 1982-09-30 1988-05-26 Boeing Co Integral lightning protection system for composite aircraft skins

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104364158A (zh) * 2012-05-31 2015-02-18 空中客车营运有限公司 可注射螺帽盖
CN105228905A (zh) * 2013-05-16 2016-01-06 空中客车营运有限公司 可注射螺帽
CN105228905B (zh) * 2013-05-16 2017-06-20 空中客车营运有限公司 可注射螺帽
CN104549905A (zh) * 2013-10-22 2015-04-29 波音公司 施用密封剂的设备和方法
CN104549905B (zh) * 2013-10-22 2019-01-08 波音公司 施用密封剂的设备和方法

Also Published As

Publication number Publication date
FR2626629A1 (fr) 1989-08-04

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