ES2054266T3 - Sujetador para estructura de fibra de carbono. - Google Patents

Sujetador para estructura de fibra de carbono.

Info

Publication number
ES2054266T3
ES2054266T3 ES90311714T ES90311714T ES2054266T3 ES 2054266 T3 ES2054266 T3 ES 2054266T3 ES 90311714 T ES90311714 T ES 90311714T ES 90311714 T ES90311714 T ES 90311714T ES 2054266 T3 ES2054266 T3 ES 2054266T3
Authority
ES
Spain
Prior art keywords
lightning
conductive sleeve
bolt
carbon fiber
interior
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
ES90311714T
Other languages
English (en)
Inventor
Leslie Pegg
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 ES2054266T3 publication Critical patent/ES2054266T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S411/00—Expanded, threaded, driven, headed, tool-deformed, or locked-threaded fastener
    • Y10S411/904—Fastener or fastener element composed of nonmetallic material
    • Y10S411/907—Elastomeric

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Bolts, Nuts, And Washers (AREA)

Abstract

UNA ESTRUCTURA COMPUESTA RESISTENTE A LOS RELAMPAGOS, ESPECIALMENTE PARA AERONAVES, EN EL QUE UN PANEL DE REVESTIMIENTO COMPUESTO, (10) POR EJEMPLO DE FIBRA DE CARBON SE UNE A UNA ESTRUCTURA COMPUESTA INTERIOR (11) POR MEDIO DE UNO O MAS CONJUNTOS DE FIJADORES RESISTENTES A LOS RELAMPAGOS (12). EL CONJUNTO DE FIJADORES COMPRENDE UNA TUERCA (21) Y UN PERNO (13), EL PERNO SE ENCUENTRA EN CONTACTO CONDUCTOR CON UNA MANGA CONDUCTORA (25) ACOPLADA AL PANEL DE REVESTIMIENTO (10) Y UNA MANGA NO CONDUCTORA (20) ACOPLADA A LA ESTRUCTURA INTERNA (11). LA TUERCA ESTA CONTENIDA DENTRO DE UN CONJUNTO DE TUERCAS RECUBIERTAS (14) COLOCADAS EN EL REVERSO DE LA ESTRUCTURA INTERIOR (11). LA MANGA NO CONDUCTORA (20) Y EL CONJUNTO DE TUERCAS RECUBIERTAS AISLA LA ESTRUCTURA INTERIOR (11) DE LOS EFECTOS DE UN RELAMPAGO, LA MANGA CONDUCTORA (25) SUMINISTRA UN INTERFASE CONDUCTOR DE ALTA CALIDAD ENTRE EL PERNO Y EL PANEL DE REVESTIMIENTO. POR ESTOS MEDIOS SE PREVIENE LA PENETRACION ADVERSA DE CORRIENTE DE RELAMPAGO DENTRO DE LA ESTRUCTURA INTERNA.
ES90311714T 1989-10-27 1990-10-25 Sujetador para estructura de fibra de carbono. Expired - Lifetime ES2054266T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB898924231A GB8924231D0 (en) 1989-10-27 1989-10-27 Carbon fibre composite structures

Publications (1)

Publication Number Publication Date
ES2054266T3 true ES2054266T3 (es) 1994-08-01

Family

ID=10665280

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90311714T Expired - Lifetime ES2054266T3 (es) 1989-10-27 1990-10-25 Sujetador para estructura de fibra de carbono.

Country Status (6)

Country Link
US (1) US5175665A (es)
EP (1) EP0425292B1 (es)
CA (1) CA2028632C (es)
DE (1) DE69009672T2 (es)
ES (1) ES2054266T3 (es)
GB (1) GB8924231D0 (es)

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US8791375B2 (en) * 2010-12-16 2014-07-29 The Boeing Company Electrically conductive bushing connection to structure for current path
JP5487093B2 (ja) * 2010-12-17 2014-05-07 三菱航空機株式会社 耐雷ファスナ、耐雷ファスナの取付構造、航空機
JP5473892B2 (ja) * 2010-12-28 2014-04-16 三菱航空機株式会社 耐雷ファスナ、航空機
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CN104364520B (zh) * 2012-06-04 2018-03-23 Lm Wp 专利控股有限公司 风力涡轮机叶片闪电旁路系统
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Also Published As

Publication number Publication date
CA2028632C (en) 2001-07-10
EP0425292B1 (en) 1994-06-08
DE69009672T2 (de) 1994-10-06
US5175665A (en) 1992-12-29
DE69009672D1 (de) 1994-07-14
EP0425292A1 (en) 1991-05-02
GB8924231D0 (en) 1989-12-13
CA2028632A1 (en) 1991-04-28

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