ES2097451T3 - Una pantalla protectora contra chispas electricas. - Google Patents

Una pantalla protectora contra chispas electricas.

Info

Publication number
ES2097451T3
ES2097451T3 ES93305727T ES93305727T ES2097451T3 ES 2097451 T3 ES2097451 T3 ES 2097451T3 ES 93305727 T ES93305727 T ES 93305727T ES 93305727 T ES93305727 T ES 93305727T ES 2097451 T3 ES2097451 T3 ES 2097451T3
Authority
ES
Spain
Prior art keywords
laminate
laminated
protective screen
against electric
electric sparks
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
ES93305727T
Other languages
English (en)
Inventor
Christophe Domine
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 ES2097451T3 publication Critical patent/ES2097451T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/28Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/26Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/02Lightning protectors; Static dischargers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/08Reinforcements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/18Aircraft

Abstract

SE PROVEEN UN ESCUDO PARA ILUMINACION QUE COMPRENDE UN LAMINADO (13,14) PLASTICO REFORZADO CON FIBRA, UNA ESTRUCTURA (12) FIJADA AL BORDE DE ATAQUE Y UN ALA (1) DE AVION COMPRENDIENDO DICHO ESCUDO LAMINADO. EL ESCUDO LAMINADO COMPRENDE UNA SERIE DE LAMINAS (21,22) DE MATERIAL DE FIBRA REFORZADA MANTENIDAS JUNTAS POR MATERIAL MATRIZ PLASTICO, INCLUYENDO EL LAMINADO UNA CAPA DE MATERIAL (19) ELECTRICAMENTE CONDUCTOR INTERPUESTA ENTRE UNA LAMINA (21) EXTERNA Y SU SIGUIENTE LAMINA (22) ADYACENTE PARA CONDUCIR CORRIENTE DE ILUMINACION PEGADA AL LAMINADO A FIADORES (31,32) CONDUCTORES QUE PASAN A TRAVES DEL LAMINADO (13,14).
ES93305727T 1992-07-24 1993-07-21 Una pantalla protectora contra chispas electricas. Expired - Lifetime ES2097451T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB929215827A GB9215827D0 (en) 1992-07-24 1992-07-24 A lightning shield

Publications (1)

Publication Number Publication Date
ES2097451T3 true ES2097451T3 (es) 1997-04-01

Family

ID=10719284

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93305727T Expired - Lifetime ES2097451T3 (es) 1992-07-24 1993-07-21 Una pantalla protectora contra chispas electricas.

Country Status (5)

Country Link
US (1) US5499782A (es)
EP (1) EP0580417B1 (es)
DE (1) DE69307798T2 (es)
ES (1) ES2097451T3 (es)
GB (1) GB9215827D0 (es)

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FR2765066B1 (fr) * 1997-06-20 1999-08-20 Aerospatiale Structure anti-etincelage, notamment pour aeronef
US6327132B1 (en) 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.
GB9926579D0 (en) * 1999-11-11 2000-01-12 British Aerospace Reinforcement of a laminated member for an aircraft
GB0117805D0 (en) * 2001-07-21 2001-09-12 Bae Systems Plc A method of securing composite elements together
US9511536B2 (en) * 2002-10-18 2016-12-06 The Boeing Company Method and apparatus to assist with removing an adhesive system
DK176298B1 (da) * 2003-09-15 2007-06-18 Lm Glasfiber As Metode til lynsikring af en vinge til et vindenergianlæg, en lynsikret vinge samt et vindenergianlæg med en sådan vinge
WO2005032812A2 (en) 2003-09-30 2005-04-14 The Boeing Company Applique
US7867621B2 (en) * 2003-09-30 2011-01-11 The Boeing Company Wide area lightning diverter overlay
US7377750B1 (en) 2004-03-19 2008-05-27 Northern Power Systems, Inc. Lightning protection system for a wind turbine
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
DE05819580T1 (de) * 2004-09-01 2008-04-24 Bell Helicopter Textron, Inc., Fort Worth Pressgeformte teile mit einer eingebetteten leiterschicht und herstellungsverfahren dafür
EP1826402B1 (en) * 2004-11-11 2016-08-24 Gamesa Innovation & Technology, S.L. Lightning conductor system for wind generator blades comprising carbon fibre laminates
ES2255436B1 (es) * 2004-11-11 2007-07-01 Gamesa Eolica, S.A. Sistema pararrayos para pala de aerogenerador con laminados de fibra de carbono.
US7236343B2 (en) * 2005-01-05 2007-06-26 The Boeing Company Method and system for lightning current conduction protection using foil bonded strips
US7686905B2 (en) * 2005-09-06 2010-03-30 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
US8246770B2 (en) * 2005-09-06 2012-08-21 The Boeing Company Copper grid repair technique for lightning strike protection
GB0609166D0 (en) * 2006-05-09 2006-06-21 Airbus Uk Ltd Apparatus for and method of inhibiting delamination
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
EP2122162B1 (en) * 2007-02-19 2017-06-28 Vestas Wind Systems A/S Wind turbine rotor blade and method of manufacturing such rotor blade
US7954763B2 (en) * 2007-04-05 2011-06-07 The Boeing Company Methods and systems for composite structural truss
US8490362B2 (en) * 2007-04-05 2013-07-23 The Boeing Company Methods and systems for composite structural truss
US7721996B2 (en) * 2007-11-13 2010-05-25 The Boeing Company Fabrication and installation of preformed dielectric inserts for lightning strike protection
ES2557998T5 (es) * 2008-04-15 2019-06-24 Siemens Ag Pala de turbina eólica con un conductor de rayos integrado y método para la fabricación de la misma
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.
US8222541B2 (en) * 2009-06-19 2012-07-17 General Electric Company Avionics chassis
US8474188B2 (en) * 2010-08-16 2013-07-02 Henniges Automotive Sealing Systems North America, Inc. Carrier having a living hinge
FR3000700B1 (fr) * 2013-01-10 2015-02-27 Herakles Revetement anti-foudre
EP2818415B1 (en) * 2013-06-27 2019-01-02 Airbus Operations GmbH Panel member for an airframe
US9702255B2 (en) * 2013-11-26 2017-07-11 Textron Innovations, Inc. Propeller with lightening strike protection
US9481157B2 (en) * 2014-03-06 2016-11-01 The Boeing Company Repair apparatus and method for composite panels having a conductive layer
US9816482B2 (en) * 2014-11-17 2017-11-14 General Electric Company Spar cap for a wind turbine rotor blade
JP6417933B2 (ja) * 2014-12-26 2018-11-07 株式会社Ihi 円筒状ケース及びジェットエンジン
US10329030B2 (en) * 2016-03-04 2019-06-25 The Boeing Company Conductive radius filler system and method
US10458425B2 (en) * 2016-06-02 2019-10-29 General Electric Company Conical load spreader for composite bolted joint
JP7433134B2 (ja) * 2020-05-22 2024-02-19 三菱重工業株式会社 風車翼、風車、及び、風車翼の製造方法

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FR2668580B1 (fr) * 1990-10-30 1993-01-22 Aerospatiale Structure anti-etincelage, notamment pour aeronef.

Also Published As

Publication number Publication date
EP0580417A1 (en) 1994-01-26
GB9215827D0 (en) 1992-09-09
DE69307798D1 (de) 1997-03-13
DE69307798T2 (de) 1997-05-22
EP0580417B1 (en) 1997-01-29
US5499782A (en) 1996-03-19

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