MX367717B - Tapa inyectable. - Google Patents

Tapa inyectable.

Info

Publication number
MX367717B
MX367717B MX2015014572A MX2015014572A MX367717B MX 367717 B MX367717 B MX 367717B MX 2015014572 A MX2015014572 A MX 2015014572A MX 2015014572 A MX2015014572 A MX 2015014572A MX 367717 B MX367717 B MX 367717B
Authority
MX
Mexico
Prior art keywords
cap
annular
cap member
sealing material
cavity
Prior art date
Application number
MX2015014572A
Other languages
English (en)
Other versions
MX2015014572A (es
Inventor
Dobbin Richard
Liversage David
Original Assignee
Airbus Operations Ltd
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
Priority claimed from GB201307134A external-priority patent/GB201307134D0/en
Priority claimed from GB201316990A external-priority patent/GB201316990D0/en
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
Publication of MX2015014572A publication Critical patent/MX2015014572A/es
Publication of MX367717B publication Critical patent/MX367717B/es

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
    • 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
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/14—Cap nuts; Nut caps or bolt caps
    • 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
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gasket Seals (AREA)
  • Closures For Containers (AREA)

Abstract

La presente invención propone una tapa (100) para formar una cavidad sellada (12) sellada alrededor de un extremo de un sujetador (2-4) para así contener eventos de desgasificación o de chispa en caso de un impacto de rayo en el sujetador (2-4). La invención también propone una junta que comprende tal tapa (100), y un estuche de partes y un método para instalar tal tapa (100). La tapa (100) de conformidad con la invención comprende un miembro (10) interno de tapa que tiene un base (11) anular que termina en un borde (18), el cual rodea una abertura dentro de la cavidad (12) de aire para encerrar un extremo del sujetador (2,4), y un miembro (20) externo de tapa que tiene un faldón anular o reborde (40) que se extiende en forma radial hacia afuera lejos de la base (11) anular, el faldón anular o reborde (40) y la base (11) anular entre ellos define una cavidad (34a-c) anular de sellado. La tapa (100) también comprende una entrada (44) de material sellador que comprende una abertura (22) en el miembro (20) externo de tapa que está en comunicación de fluidos con la cavidad (34a-c) anular de sellado, la abertura (32) está dispuesta para interconectarse con el dispositivo (80) de inyección de material sellador para proporcionar un flujo de material (81) de sellado curable desde la entrada (44) de material sellador dentro de la cavidad (34a-c) anular de sellado. El miembro (20) externo de tapa tiene una superficie interna formada con una primera característica de cierre (95, 96) y el miembro (10) interno de tapa tiene una superficie externa formada con una segunda característica (97) de cierre que forma una junta de ajuste a presión con una primera característica (95, 96) de cierre.
MX2015014572A 2013-04-19 2014-04-16 Tapa inyectable. MX367717B (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB201307134A GB201307134D0 (en) 2013-04-19 2013-04-19 Injectable nut cap
GB201316990A GB201316990D0 (en) 2013-09-25 2013-09-25 Injectable cap
PCT/GB2014/051192 WO2014170672A1 (en) 2013-04-19 2014-04-16 Injectable cap

Publications (2)

Publication Number Publication Date
MX2015014572A MX2015014572A (es) 2016-12-16
MX367717B true MX367717B (es) 2019-09-03

Family

ID=50543230

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015014572A MX367717B (es) 2013-04-19 2014-04-16 Tapa inyectable.

Country Status (7)

Country Link
US (1) US9829030B2 (es)
EP (1) EP2986509B1 (es)
JP (1) JP6302046B2 (es)
CN (1) CN105121287B (es)
CA (1) CA2908919C (es)
MX (1) MX367717B (es)
WO (1) WO2014170672A1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105473445B (zh) 2013-08-21 2017-10-03 空中客车营运有限公司 具有注入的密封剂的帽
GB2535518A (en) * 2015-02-20 2016-08-24 Airbus Operations Ltd Cap with injected sealant
GB2535519A (en) 2015-02-20 2016-08-24 Airbus Operations Ltd Two part cap
US11161156B2 (en) * 2015-10-27 2021-11-02 Hamilton Sundstrand Corporation Powder monitoring
US9937746B2 (en) * 2016-05-03 2018-04-10 Maclean Fogg Company Capped wheel fastener and method of assembly
EP3392418B1 (de) * 2017-04-19 2020-04-29 Geberit International AG Befestigungssystem
GB2568069A (en) * 2017-11-03 2019-05-08 Airbus Operations Ltd A nut cap
GB2572377A (en) * 2018-03-28 2019-10-02 Airbus Operations Ltd Cap with sealant flow path
DE202018104479U1 (de) * 2018-08-03 2018-08-21 Fairchild Fasteners Europe - Camloc Gmbh Einsatz zur Verbindung eines elektrischen Anschlusses mit einer Wand sowie Schutzkappe für einen Einsatz
US11022164B2 (en) * 2018-09-11 2021-06-01 The Boeing Company Double shell fastener caps
GB2579229A (en) 2018-11-26 2020-06-17 Airbus Operations Ltd Spark containment cap
US10982704B2 (en) * 2019-01-03 2021-04-20 The Boeing Company EME protection cap system with screw sealant mechanism
GB2582631A (en) * 2019-03-28 2020-09-30 Airbus Operations Ltd A joint for an aircraft assembly
GB2598373A (en) * 2020-08-28 2022-03-02 Airbus Operations Ltd Spark containment cap

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710113A (en) 1952-01-23 1955-06-07 Gen Dynamics Corp Seal construction
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
FR2626629B1 (fr) 1988-01-29 1990-03-09 Aerospatiale Procede et dispositif de fixation d'elements de structures d'aeronefs protegees contre la foudre, et outil pour la mise en oeuvre de ce procede
US4905931A (en) 1988-02-18 1990-03-06 The Boeing Company Arc suppression around fasteners
JPH02102910A (ja) * 1988-10-13 1990-04-16 Dainippon Toryo Co Ltd ボルト・ナットの防食方法及び保護キャップ
JPH0439313U (es) * 1990-07-27 1992-04-03
US5419666A (en) 1993-09-27 1995-05-30 Best; Don A. Protective waterproof cover assembly for covering a fastener
JP3023464U (ja) * 1995-10-04 1996-04-16 株式会社ビッグウエスト ナットキャップ
DE102005030817B4 (de) 2005-07-01 2008-07-24 Radolid Thiel Gmbh Schutzkappe für Schraubverbindungen sowie Verfahren zur Herstellung von Schutzkappen für Schraubverbindungen
JP5055178B2 (ja) * 2008-03-24 2012-10-24 三菱重工業株式会社 航空機組立品
JP5610758B2 (ja) 2009-04-02 2014-10-22 三菱航空機株式会社 耐雷ファスナ、キャップ、耐雷ファスナの取り付け方法、航空機
US9228604B2 (en) 2011-02-10 2016-01-05 Airbus Operations Limited Cap for forming sealed cavity around fastener
US8388293B2 (en) * 2011-02-28 2013-03-05 Physical Systems, Inc. Insulated and sealed cap for a fastener component
JP5611097B2 (ja) * 2011-03-30 2014-10-22 三菱航空機株式会社 耐雷防爆用ファスナ
CA2873823C (en) 2012-05-31 2018-09-04 Airbus Operations Limited Injectable nut cap

Also Published As

Publication number Publication date
EP2986509B1 (en) 2018-05-30
JP6302046B2 (ja) 2018-03-28
US20160069376A1 (en) 2016-03-10
US9829030B2 (en) 2017-11-28
CA2908919C (en) 2019-11-26
CN105121287A (zh) 2015-12-02
MX2015014572A (es) 2016-12-16
CA2908919A1 (en) 2014-10-23
WO2014170672A1 (en) 2014-10-23
EP2986509A1 (en) 2016-02-24
JP2016517941A (ja) 2016-06-20
CN105121287B (zh) 2017-05-24

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