ES2402466R1 - Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave. - Google Patents

Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave.

Info

Publication number
ES2402466R1
ES2402466R1 ES201031838A ES201031838A ES2402466R1 ES 2402466 R1 ES2402466 R1 ES 2402466R1 ES 201031838 A ES201031838 A ES 201031838A ES 201031838 A ES201031838 A ES 201031838A ES 2402466 R1 ES2402466 R1 ES 2402466R1
Authority
ES
Spain
Prior art keywords
layer
area
structural component
dielectric layer
metal part
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.)
Granted
Application number
ES201031838A
Other languages
English (en)
Other versions
ES2402466A2 (es
ES2402466B1 (es
Inventor
Macarrilla Jose Orencio Granado
Valdegrama Vicente Martinez
Sevilla Alberto Lozano
Rodriguez Daniel Casares
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 Operations SL
Original Assignee
Airbus Operations SL
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 Operations SL filed Critical Airbus Operations SL
Priority to ES201031838A priority Critical patent/ES2402466B1/es
Priority to US13/033,410 priority patent/US9016615B2/en
Priority to CN201110418441.XA priority patent/CN102556357B/zh
Priority to EP20110193533 priority patent/EP2465776B1/en
Priority to ES11193533.4T priority patent/ES2476043T3/es
Publication of ES2402466A2 publication Critical patent/ES2402466A2/es
Publication of ES2402466R1 publication Critical patent/ES2402466R1/es
Application granted granted Critical
Publication of ES2402466B1 publication Critical patent/ES2402466B1/es
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of riveting

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)

Abstract

Disposición de protección de rayos y corrosión en Disposición de protección de rayos y corrosión en un componente estructural de una aeronave en una jun componente estructural de una aeronave en una junta entre un pieza metálica exterior (11) y un counta entre un pieza metálica exterior (11) y un componente (13) realizado total o parcialmente con Cmponente (13) realizado total o parcialmente con CFRP por medio de una fila de remaches metálicos (1FRP por medio de una fila de remaches metálicos (15) que comprende unas capas metálicas interior y e5) que comprende unas capas metálicas interior y exterior (21, 25) y una capa dieléctrica intermediaxterior (21, 25) y una capa dieléctrica intermedia (23), siendo la capa interior (21) en contacto co (23), siendo la capa interior (21) en contacto con dicho componente estructural (13) menos espesa yn dicho componente estructural (13) menos espesa y más grande que la capa exterior (25) en contacto más grande que la capa exterior (25) en contacto con la pieza metálica (11), quedando extendida la con la pieza metálica (11), quedando extendida la capa dieléctrica intermedia (23) en un área mayor capa dieléctrica intermedia (23) en un área mayor que el área del pie (12) de la pieza metálica (11)que el área del pie (12) de la pieza metálica (11) con una mínima distancia lineal predeterminada D1 con una mínima distancia lineal predeterminada D1 entre sus bordes, quedando extendida la capa metá entre sus bordes, quedando extendida la capa metálica exterior (25) en un área mayor que el área delica exterior (25) en un área mayor que el área de la capa dieléctrica intermedia (23) con una mínim la capa dieléctrica intermedia (23) con una mínima distancia lineal D2 predeterminada entre sus bora distancia lineal D2 predeterminada entre sus bordes. des.
ES201031838A 2010-12-14 2010-12-14 Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave. Expired - Fee Related ES2402466B1 (es)

Priority Applications (5)

Application Number Priority Date Filing Date Title
ES201031838A ES2402466B1 (es) 2010-12-14 2010-12-14 Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave.
US13/033,410 US9016615B2 (en) 2010-12-14 2011-02-23 Lightning and corrosion protection arrangement in an aircraft structural component
CN201110418441.XA CN102556357B (zh) 2010-12-14 2011-12-14 飞机结构部件中的雷电和腐蚀防护装置
EP20110193533 EP2465776B1 (en) 2010-12-14 2011-12-14 Lightning and corrosion protection arrangement in an aircraft structural component
ES11193533.4T ES2476043T3 (es) 2010-12-14 2011-12-14 Disposición de protección de rayos y corrosión en un componente estructural de una aeronave

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201031838A ES2402466B1 (es) 2010-12-14 2010-12-14 Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave.

Publications (3)

Publication Number Publication Date
ES2402466A2 ES2402466A2 (es) 2013-05-03
ES2402466R1 true ES2402466R1 (es) 2013-05-07
ES2402466B1 ES2402466B1 (es) 2014-03-13

Family

ID=45218535

Family Applications (2)

Application Number Title Priority Date Filing Date
ES201031838A Expired - Fee Related ES2402466B1 (es) 2010-12-14 2010-12-14 Disposicion de proteccion de rayos y corrosion en un componente estructural de una aeronave.
ES11193533.4T Active ES2476043T3 (es) 2010-12-14 2011-12-14 Disposición de protección de rayos y corrosión en un componente estructural de una aeronave

Family Applications After (1)

Application Number Title Priority Date Filing Date
ES11193533.4T Active ES2476043T3 (es) 2010-12-14 2011-12-14 Disposición de protección de rayos y corrosión en un componente estructural de una aeronave

Country Status (4)

Country Link
US (1) US9016615B2 (es)
EP (1) EP2465776B1 (es)
CN (1) CN102556357B (es)
ES (2) ES2402466B1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9481157B2 (en) 2014-03-06 2016-11-01 The Boeing Company Repair apparatus and method for composite panels having a conductive layer
EP3194799A1 (en) * 2014-09-17 2017-07-26 Arconic Inc. Fasteners with dual skin depth washers
US9784132B2 (en) 2015-04-20 2017-10-10 Pratt & Whitney Canada Corp. Voltage discharge channelling assembly for a gas turbine engine
US9964131B1 (en) * 2017-04-28 2018-05-08 The Boeing Company Methods and apparatuses for providing corrosion protection to joined surfaces
JP6770987B2 (ja) * 2018-03-12 2020-10-21 株式会社Ｓｕｂａｒｕ 複合材構造体、航空機及び雷電流の誘導方法
US11572195B2 (en) 2018-07-26 2023-02-07 Honeywell International Inc. Lightning-dissipative aircraft assemblies and valve frames utilized in the same

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
US5417385A (en) * 1991-04-12 1995-05-23 Short Brothers Plc Structural component
US20070230085A1 (en) * 2006-03-29 2007-10-04 The Boeing Company Flex circuit lightning protection applique system for skin fasteners in composite structures

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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.
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.
ES2279664B1 (es) 2004-12-30 2008-08-01 Airbus España S.L. Dispositivo de proteccion contra descargas electricas en aeronaves.
US8038099B2 (en) * 2008-04-30 2011-10-18 The Boeing Company Bonded metal fuselage and method for making the same
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
DE102009026686A1 (de) * 2009-06-03 2010-12-23 Airbus France Anordnung zum Blitzschutz einer elektronischen Einheit

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
US5417385A (en) * 1991-04-12 1995-05-23 Short Brothers Plc Structural component
US20070230085A1 (en) * 2006-03-29 2007-10-04 The Boeing Company Flex circuit lightning protection applique system for skin fasteners in composite structures

Also Published As

Publication number Publication date
EP2465776A2 (en) 2012-06-20
US9016615B2 (en) 2015-04-28
US20120145825A1 (en) 2012-06-14
EP2465776B1 (en) 2014-04-09
CN102556357B (zh) 2015-12-09
ES2476043T3 (es) 2014-07-11
EP2465776A3 (en) 2013-01-16
ES2402466A2 (es) 2013-05-03
ES2402466B1 (es) 2014-03-13
CN102556357A (zh) 2012-07-11

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