ES2136249T3 - Dispositivo de fijacion para revestimiento composite de aviones. - Google Patents

Dispositivo de fijacion para revestimiento composite de aviones.

Info

Publication number
ES2136249T3
ES2136249T3 ES95303745T ES95303745T ES2136249T3 ES 2136249 T3 ES2136249 T3 ES 2136249T3 ES 95303745 T ES95303745 T ES 95303745T ES 95303745 T ES95303745 T ES 95303745T ES 2136249 T3 ES2136249 T3 ES 2136249T3
Authority
ES
Spain
Prior art keywords
composite coating
screw
interior
fixing device
exterior
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
ES95303745T
Other languages
English (en)
Inventor
Barry John Pridham
Austyn Ch Stephens
Christopher Ch Jones
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Application granted granted Critical
Publication of ES2136249T3 publication Critical patent/ES2136249T3/es
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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Elimination Of Static Electricity (AREA)

Abstract

EN LA PRESENTE INVENCION SE PRESENTA UN METODO PARA FIJAR UN REVESTIMIENTO COMPUESTO EXTERIOR DE UNA AERONAVE (12) A UNA SUBESTRUCTURA INTERIOR (14), QUE PUEDE SER LA PARED DE UN DEPOSITO DE COMBUSTIBLE, Y UNA COMBINACION DE FIJACION. LA INVENCION CONSISTE EN INCORPORAR UNA CAPA ELECTRICAMENTE CONDUCTORA (26) EN UNA SUPERFICIE EXTERIOR DEL REVESTIMIENTO COMPUESTO EXTERIOR (12), INSERTAR UN TORNILLO (11) A TRAVES DE LA CAPA ELECTRICAMENTE CONDUCTORA (26) Y DEL REVESTIMIENTO COMPUESTO EXTERIOR (12) Y A TRAVES DE LA SUBESTRUCTURA INTERIOR (12), ASEGURAR EL TORNILLO (11) CON UNA TUERCA (22) DE MODO QUE QUEDE ACOPLADO DIRECTA O INDIRECTAMENTE A LA SUPERFICIE INTERIOR DE LA SUBESTRUCTURA INTERIOR (14) Y APLICAR UN MATERIAL AISLANTE (34) SOBRE LA CABEZA (16) DEL TORNILLO.
ES95303745T 1994-06-02 1995-06-01 Dispositivo de fijacion para revestimiento composite de aviones. Expired - Lifetime ES2136249T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9411006A GB9411006D0 (en) 1994-06-02 1994-06-02 Method of fastening composite aircraft skins

Publications (1)

Publication Number Publication Date
ES2136249T3 true ES2136249T3 (es) 1999-11-16

Family

ID=10756043

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95303745T Expired - Lifetime ES2136249T3 (es) 1994-06-02 1995-06-01 Dispositivo de fijacion para revestimiento composite de aviones.

Country Status (5)

Country Link
US (1) US5845872A (es)
EP (1) EP0685389B1 (es)
DE (1) DE69511623T2 (es)
ES (1) ES2136249T3 (es)
GB (1) GB9411006D0 (es)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2264299A1 (es) * 2003-06-06 2006-12-16 Airbus España S.L. Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica.

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US6679667B2 (en) * 2001-02-28 2004-01-20 Northrop Grumman Corporation Hot melt fastener filler
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US8231751B2 (en) * 2005-09-06 2012-07-31 The Boeing Company Repair technique for lightning strike protection
US7686905B2 (en) 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
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BRPI0711444B1 (pt) * 2006-06-09 2020-04-28 Mitsubishi Heavy Ind Ltd montagem de avião
JP4657194B2 (ja) * 2006-11-20 2011-03-23 本田技研工業株式会社 前縁スキンの段差調整構造および前縁スキンの組付方法
US7898785B2 (en) * 2006-12-07 2011-03-01 The Boeing Company Lightning protection system for an aircraft composite structure
US7599164B2 (en) * 2006-12-07 2009-10-06 The Boeing Company Lightning protection system for aircraft composite structure
US7738236B2 (en) * 2007-01-12 2010-06-15 The Boeing Company Light weight system for lightning protection of nonconductive aircraft panels
DE102007003276B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind
JP2008285115A (ja) * 2007-05-21 2008-11-27 Mitsubishi Heavy Ind Ltd 航空機組立品およびその製造方法
US7883050B2 (en) * 2007-06-28 2011-02-08 The Boeing Company Composites with integrated multi-functional circuits
US7934676B2 (en) * 2007-06-28 2011-05-03 The Boeing Company Pre-fabricated article for EME protection of an aircraft
US8398027B2 (en) * 2007-09-17 2013-03-19 The Boeing Company Method and apparatus for reinforcing composite structures
JP4719203B2 (ja) * 2007-09-28 2011-07-06 三菱重工業株式会社 耐雷ファスナ
US20090092764A1 (en) * 2007-10-05 2009-04-09 Hoeckelman Leslie A Method and apparatus for simultaneous spray and cure initiation of curable polymer coating compositions
US7835130B2 (en) 2007-10-05 2010-11-16 The Boeing Company Method and apparatus for lightning protection of a composite structure
US7721996B2 (en) * 2007-11-13 2010-05-25 The Boeing Company Fabrication and installation of preformed dielectric inserts for lightning strike protection
FR2924685B1 (fr) 2007-12-11 2010-03-19 Airbus France Systeme parafoudre et aeronef comportant un tel systeme.
FR2924686B1 (fr) * 2007-12-11 2010-05-14 Airbus France Systeme parafoudre et aeronef comportant un tel systeme.
JP5055178B2 (ja) * 2008-03-24 2012-10-24 三菱重工業株式会社 航空機組立品
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
GB0819159D0 (en) * 2008-10-20 2008-11-26 Airbus Uk Ltd Joint between aircraft components
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.
JP5237170B2 (ja) * 2009-03-30 2013-07-17 三菱重工業株式会社 複合材タンク、翼、および、複合材タンクの製造方法
BRPI1010855A2 (pt) * 2009-06-12 2016-04-05 Lord Corp método para proteção de um substrato contra interferência eletromagnética
US8282042B2 (en) * 2009-06-22 2012-10-09 The Boeing Company Skin panel joint for improved airflow
US9821538B1 (en) 2009-06-22 2017-11-21 The Boeing Company Ribbed caul plate for attaching a strip to a panel structure and method for use
EP2455286B1 (en) 2010-11-22 2016-09-28 Airbus Defence and Space SA Lightning protection for composite aircraft structures
US20120201999A1 (en) * 2011-02-08 2012-08-09 Woods Mark A Methods and apparatus for mechanically joining metal components and composite components
JP5535956B2 (ja) * 2011-02-14 2014-07-02 三菱重工業株式会社 耐雷ファスナ
EP2789827B1 (en) * 2011-12-07 2018-11-14 IHI Corporation Attachment boss and fan case
US9481012B2 (en) * 2012-05-23 2016-11-01 The Boeing Company Method of filling voids around countersunk fastener heads
US9739402B2 (en) 2013-03-04 2017-08-22 Eaton Corporation Electrically conductive seals for fluid conveyance systems
EP2799220B1 (en) * 2013-04-30 2020-06-17 Airbus Operations S.L. Composite structure for an aircraft and manufacturing method thereof
US20140331477A1 (en) * 2013-05-07 2014-11-13 The Boeing Company Flush fastener design and installation
US9908637B2 (en) * 2014-05-23 2018-03-06 The Boeing Company Modified shank fasteners for electromagnetic effect (EME) technology
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
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US11572195B2 (en) 2018-07-26 2023-02-07 Honeywell International Inc. Lightning-dissipative aircraft assemblies and valve frames utilized in the same
JP2020034144A (ja) * 2018-08-31 2020-03-05 川崎重工業株式会社 シール構造
US11137014B2 (en) 2019-01-08 2021-10-05 The Boeing Company Conductive fastening system and method for improved EME performance
CN114180083B (zh) * 2021-11-19 2023-09-01 中国直升机设计研究所 一种利用铜杯实现的复合材料结构件之间导电处理方法

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2264299A1 (es) * 2003-06-06 2006-12-16 Airbus España S.L. Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica.

Also Published As

Publication number Publication date
US5845872A (en) 1998-12-08
EP0685389A1 (en) 1995-12-06
EP0685389B1 (en) 1999-08-25
GB9411006D0 (en) 1994-07-20
DE69511623D1 (de) 1999-09-30
DE69511623T2 (de) 1999-12-09

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