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)

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.

Families Citing this family (64)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9807198D0 (en) 1998-04-04 1998-06-03 British Aerospace Adhesively bonded joints in carbon fibre composite structures
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.
US7223312B2 (en) * 2000-09-21 2007-05-29 Integument Technologies, Inc. Methods and materials for reducing damage from environmental electromagnetic effects
US20020081921A1 (en) * 2000-09-21 2002-06-27 Vargo Terrence G. Methods and materials for reducing damage from environmental electromagnetic effects
US6679667B2 (en) * 2001-02-28 2004-01-20 Northrop Grumman Corporation Hot melt fastener filler
GB0117805D0 (en) * 2001-07-21 2001-09-12 Bae Systems Plc A method of securing composite elements together
FR2830236B1 (fr) * 2001-10-02 2004-02-27 Airbus France Dispositif de fixation d'un pare-brise d'aeronef
DE10200564B4 (de) * 2002-01-09 2007-08-09 Eads Deutschland Gmbh Blitzschutzeinrichtung an faserverstärkten Bauteilen für mittels lösbaren Bolzenverbindungen entfernbare Verschluss-Deckel
DE602004002482T2 (de) * 2003-05-30 2007-02-01 Bae Systems Plc Verbundstruktur-blitzschlagschutz
GB0329373D0 (en) 2003-12-18 2004-01-21 Airbus Uk Ltd Method of joining structural elements in an aircraft
EP1544099B1 (en) * 2003-12-18 2009-01-07 Airbus UK Limited Method of joining structural elements in an aircraft
FR2873347B1 (fr) * 2004-07-22 2006-11-17 Airbus France Sas Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
GB0417472D0 (en) * 2004-08-05 2004-09-08 Airbus Uk Ltd Fuel tank system
US7686905B2 (en) 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
US8246770B2 (en) * 2005-09-06 2012-08-21 The Boeing Company Copper grid repair technique for lightning strike protection
US8231751B2 (en) * 2005-09-06 2012-07-31 The Boeing Company Repair technique for lightning strike protection
JP4786426B2 (ja) * 2005-10-06 2011-10-05 三菱重工業株式会社 ファスナ
US7886439B2 (en) * 2005-12-15 2011-02-15 The Boeing Company Ground stud installation on composite structures for electrostatic charges
US20070137032A1 (en) * 2005-12-15 2007-06-21 Braden Stephen M Ground stud installation on composite structure for electrostatic charges
US7277266B1 (en) 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure
US20080003078A1 (en) 2006-05-02 2008-01-03 United Technologies Corporation Fastener
GB0609166D0 (en) * 2006-05-09 2006-06-21 Airbus Uk Ltd Apparatus for and method of inhibiting delamination
US8092134B2 (en) 2006-06-09 2012-01-10 Mitsubishi Heavy Industries, Ltd. Fastener
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
US7599164B2 (en) * 2006-12-07 2009-10-06 The Boeing Company Lightning protection system for aircraft composite structure
US7898785B2 (en) * 2006-12-07 2011-03-01 The Boeing Company Lightning protection system for an 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
FR2924686B1 (fr) 2007-12-11 2010-05-14 Airbus France Systeme parafoudre et aeronef comportant un tel systeme.
FR2924685B1 (fr) * 2007-12-11 2010-03-19 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
KR20120037464A (ko) * 2009-06-12 2012-04-19 로오드 코포레이션 전자파 장애로부터 기판을 차폐하는 방법
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
WO2013084308A1 (ja) * 2011-12-07 2013-06-13 株式会社Ihi 取付用ボスおよびファンケース
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
US10457411B2 (en) * 2016-06-17 2019-10-29 Goodrich Corporation Lightning strike dispersion for composite aircraft structures
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
EP4516683B1 (fr) * 2023-08-31 2025-10-15 Airbus Operations (S.A.S.) Procédé de réparation d'une pièce structurale d'un aéronef présentant un défaut de protection, et pièce structurale d'aéronef ainsi réparée
CN120863894A (zh) * 2025-09-29 2025-10-31 合肥航太电物理技术有限公司 一种飞机油箱雷电点火源防护结构

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982494A (en) * 1959-06-11 1961-05-02 Douglas Aircraft Co Inc Lightning arrestor for radomes
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
DE3278383D1 (en) * 1982-09-30 1988-05-26 Boeing Co Integral lightning protection system for composite aircraft skins
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
DE3301669A1 (de) * 1983-01-20 1984-07-26 Bayer Ag, 5090 Leverkusen Blitzschutzverbundmaterial
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
US4681497A (en) * 1985-05-29 1987-07-21 Microdot Inc. Encapsulated fastener
US4760493A (en) * 1985-09-30 1988-07-26 The Boeing Company Lightning protection system for composite material aircraft structures
US4628402A (en) * 1985-09-30 1986-12-09 The Boeing Company Lightning protection of fasteners in composite material
US4630168A (en) * 1985-12-16 1986-12-16 The Boeing Company Lightning protection fastener
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
US4718801A (en) * 1986-07-24 1988-01-12 Microdot Inc. Composite core fastener
US4912594A (en) * 1986-11-03 1990-03-27 The Boeing Company Integral lightning protection repair system and method for its use
GB8628555D0 (en) 1986-11-28 1987-01-07 British Aerospace Anti lightning strike fasteners
GB8704585D0 (en) * 1987-02-26 1987-04-01 British Aerospace Lighting strike protection
GB2212580B (en) 1987-11-14 1992-03-25 British Aerospace Methods of fastening composite aircraft skins
US4888451A (en) * 1988-11-29 1989-12-19 United Technologies Corporation Electrical continuity means for composite joints
GB9215827D0 (en) * 1992-07-24 1992-09-09 British Aerospace A lightning shield

Cited By (2)

* 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.
ES2264299B1 (es) * 2003-06-06 2007-11-16 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
EP0685389B1 (en) 1999-08-25
GB9411006D0 (en) 1994-07-20
US5845872A (en) 1998-12-08
DE69511623T2 (de) 1999-12-09
EP0685389A1 (en) 1995-12-06
DE69511623D1 (de) 1999-09-30

Similar Documents

Publication Publication Date Title
ES2136249T3 (es) Dispositivo de fijacion para revestimiento composite de aviones.
ES516358A0 (es) Un procedimiento para dotar a un conductor electrico de una capa exterior semiconductora que puede desprenderse con el fin de efectuar reparaciones.
HK30587A (en) Luminous indicating device
BR9612202A (pt) ''f filamento eletroluminescente''
MX171975B (es) Filamento calentador encapsulado para tapon encendedor
ES2158459T3 (es) Revestimiento de barrera termica con subcapa mejorada y piezas revestidas por dicha barrera termica.
CU23281A3 (es) Componente de metal conductivo elã0/00ctricamente con superficie tratada de un montaje de pila elã0/00ctrica de ã"xido sã"lido
JPS51114886A (en) Photocoupling semiconductor device and its manufacturing process
UY24207A1 (es) Cigarrillo y calentador para ser utilizados en un sistema eléctrico para fumar
ES2078379T3 (es) Procedimiento para crear una union superconductora de conductores de nb3sn y nbti, y union superconductora.
CO4790195A1 (es) Producto de seguridad y valor con un elemento luminiscente
AR246825A1 (es) Soporte de montaje y metodo para montar un filtro dielectrico sobre un substrato.
JPS6431369A (en) Electric heating unit
DE3576019D1 (de) Steckerbuchse mit isolierstoffummantelung sowie vorrichtung fuer ihre herstellung.
SMP200700052B (it) Maniglia luminosa per porte, arredamenti, mezzi ditrasporto o simili
PT1393596E (pt) Vidro com um revestimento opaco
AR021223A1 (es) Articulo de vidrio recubierto, termo-reforzado, y metodo para producir el mismo.
DE4300819A1 (de) Verkleidungselement mit Leuchtleiste
ES2162718A1 (es) Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones.
ES2090040T3 (es) Un dispositivo de instalacion de antena que utiliza un dispositivo de acoplamiento de tipo tornillo.
IT8822335A0 (it) Procedimento e dispositivo per la preparazione di rondelle con almeno una superficie piana.
ES2133768T3 (es) Articulo compuesto y procedimiento para fabricarlo.
ES2147805T3 (es) Dispositivo para la conexion a masa de cables electricos, especialmente a una carroceria de un vehiculo.
ES2039892T3 (es) Adaptador de cableado y procedimiento para su formacion.
CN206739018U (zh) 柔性霓虹灯带堵头及匹配的柔性霓虹灯带

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 685389

Country of ref document: ES