MX2016002183A - Tapa con sellador inyectado. - Google Patents

Tapa con sellador inyectado.

Info

Publication number
MX2016002183A
MX2016002183A MX2016002183A MX2016002183A MX2016002183A MX 2016002183 A MX2016002183 A MX 2016002183A MX 2016002183 A MX2016002183 A MX 2016002183A MX 2016002183 A MX2016002183 A MX 2016002183A MX 2016002183 A MX2016002183 A MX 2016002183A
Authority
MX
Mexico
Prior art keywords
pocket
skirt
cap
inlet hole
sealing material
Prior art date
Application number
MX2016002183A
Other languages
English (en)
Inventor
Richard Dobbin
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 GB1314994.3A external-priority patent/GB2517473A/en
Priority claimed from GB1321248.5A external-priority patent/GB2520774A/en
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
Publication of MX2016002183A publication Critical patent/MX2016002183A/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
    • F16B37/00—Nuts or like thread-engaging members
    • F16B37/14—Cap nuts; Nut caps or bolt caps
    • 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
    • F16B33/00—Features common to bolt and nut
    • F16B33/004—Sealing; Insulation

Landscapes

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

Abstract

Una tapa para formar una cavidad (130) sellada alrededor de un extremo de un sujetador (120) que sobresale de una estructura (110). La tapa tiene: un cuerpo de tapa con una base (210) anular que termina en una orilla (211), la cual rodea una abertura dentro de la cavidad (130) central, un faldón (220) anular que proporciona una cavidad (240) anular entre el faldón (220) y la base (210) y un orificio (251) de entrada en el faldón (220). El orificio (251) de entrada está en comunicación de fluidos con la cavidad (240) y está dispuesto para interconectarse con un dispositivo de inyección de material sellador para proporcionar un flujo de material sellador a través del faldón (220) mediante el orificio (251) de entrada dentro de la cavidad (240). Una salida (270) también es provista en el faldón (220). La salida (270) está en comunicación de fluidos con la cavidad (240) y está dispuesta para permitir que el aire se escape de la cavidad (240) a través del faldón (220) a través del orificio (270) de salida conforme el material sellador fluye desde el orificio (251) de entrada dentro de la cavidad (240).
MX2016002183A 2013-08-21 2014-07-21 Tapa con sellador inyectado. MX2016002183A (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB1314994.3A GB2517473A (en) 2013-08-21 2013-08-21 Cap with injected sealant
GB1321248.5A GB2520774A (en) 2013-12-02 2013-12-02 Cap with injected sealant
PCT/GB2014/052216 WO2015025130A1 (en) 2013-08-21 2014-07-21 Cap with injected sealant

Publications (1)

Publication Number Publication Date
MX2016002183A true MX2016002183A (es) 2016-06-21

Family

ID=51220601

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016002183A MX2016002183A (es) 2013-08-21 2014-07-21 Tapa con sellador inyectado.

Country Status (8)

Country Link
US (2) US10415623B2 (es)
EP (1) EP3036163B1 (es)
JP (1) JP6483690B2 (es)
KR (1) KR20160044495A (es)
CN (1) CN105473445B (es)
CA (1) CA2919188C (es)
MX (1) MX2016002183A (es)
WO (1) WO2015025130A1 (es)

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CA2919188C (en) 2013-08-21 2020-06-09 Airbus Operations Limited Cap with injected sealant
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GB2533317B (en) 2014-12-16 2017-08-23 Airbus Operations Ltd Spark containment cap
GB2535168A (en) 2015-02-09 2016-08-17 Airbus Operations Ltd Method of installing a spark containment cap
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
JP6742810B2 (ja) * 2016-05-20 2020-08-19 株式会社日立製作所 ボルトキャップ
CN106626467A (zh) * 2016-12-19 2017-05-10 中航成飞民用飞机有限责任公司 罩封器、做罩封装置及做罩封方法
GB2557961A (en) * 2016-12-20 2018-07-04 Airbus Operations Ltd Cap for a fastener
GB2557962A (en) 2016-12-20 2018-07-04 Airbus Operations Ltd Cap for a fastener
US10655667B2 (en) 2017-09-28 2020-05-19 The Boeing Company Rapid installation thermoplastic EME protection cap
GB2568890A (en) * 2017-11-29 2019-06-05 Airbus Operations Ltd Spark containment cap
GB2572377A (en) 2018-03-28 2019-10-02 Airbus Operations Ltd Cap with sealant flow path
GB2572376A (en) 2018-03-28 2019-10-02 Airbus Operations Ltd Cap with sealant flow path
US10962043B2 (en) 2018-04-24 2021-03-30 The Boeing Company Anchoring nut for an EME protection cap system
US10920818B2 (en) * 2018-04-27 2021-02-16 The Boeing Company Anchoring washer for an EME protection cap system
US10948004B2 (en) * 2018-07-26 2021-03-16 The Boeing Company Anchoring bolt head for an EME protection cap system
US11022164B2 (en) * 2018-09-11 2021-06-01 The Boeing Company Double shell fastener caps
US11078947B2 (en) 2018-09-11 2021-08-03 The Boeing Company Combustion quenching fastener caps with holes
US11248647B2 (en) 2018-11-09 2022-02-15 The Boeing Company EME cap for preventing uncured sealant squeeze out
US10989244B2 (en) 2018-11-20 2021-04-27 The Boeing Company EME protection cap system with push sealant extrusion mechanism
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
US10767684B1 (en) * 2019-04-26 2020-09-08 Solsera, Inc. Flat roof mounting device
US11236777B2 (en) * 2019-05-06 2022-02-01 The Boeing Company Friction fit electromagnetic effect protection cap system
US11788573B2 (en) 2019-05-23 2023-10-17 The Boeing Company Multi-component melt electromagnetic effect protection cap system
GB2584433A (en) * 2019-05-30 2020-12-09 Airbus Operations Ltd Spark containment cap
EP3779217A1 (en) * 2019-08-12 2021-02-17 Asyst Technologies, Llc Injectable cap assembly and method of use
WO2021046473A1 (en) * 2019-09-05 2021-03-11 Novaria Holdings, LLC Nut cap
WO2021155039A1 (en) * 2020-01-29 2021-08-05 Novaria Holdings, LLC One-piece nut cap
US11754111B2 (en) 2020-03-16 2023-09-12 The Boeing Company Compression fit EME protection seal cap

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MX2015014571A (es) * 2013-04-19 2016-07-05 Airbus Operations Ltd Tapa inyectable.
MX367717B (es) * 2013-04-19 2019-09-03 Airbus Operations Ltd Tapa inyectable.
JP2016524676A (ja) * 2013-04-22 2016-08-18 ピーアールシー−デソト インターナショナル，インコーポレイティド 内部隔壁リングを含むシーラント・キャップ
FR3005121B1 (fr) * 2013-04-30 2015-05-22 Airbus Operations Sas Dispositif de guidage destine a etre interpose entre un dispositif de fixation de pieces d'un assemblage, et un dispositif de protection du dispositif de fixation
GB2516835B (en) 2013-07-31 2015-11-04 Airbus Operations Ltd Cap to accommodate washers
CA2919188C (en) 2013-08-21 2020-06-09 Airbus Operations Limited Cap with injected sealant
GB2533317B (en) * 2014-12-16 2017-08-23 Airbus Operations Ltd Spark containment cap
GB2535168A (en) * 2015-02-09 2016-08-17 Airbus Operations Ltd Method of installing a spark containment cap
GB2535519A (en) * 2015-02-20 2016-08-24 Airbus Operations Ltd Two part cap
GB2535518A (en) * 2015-02-20 2016-08-24 Airbus Operations Ltd Cap with injected sealant

Also Published As

Publication number Publication date
WO2015025130A1 (en) 2015-02-26
EP3036163A1 (en) 2016-06-29
CN105473445B (zh) 2017-10-03
US10415623B2 (en) 2019-09-17
CA2919188A1 (en) 2015-02-26
US20190345969A1 (en) 2019-11-14
CN105473445A (zh) 2016-04-06
US10774869B2 (en) 2020-09-15
CA2919188C (en) 2020-06-09
EP3036163B1 (en) 2019-09-04
US20160195125A1 (en) 2016-07-07
JP6483690B2 (ja) 2019-03-13
KR20160044495A (ko) 2016-04-25
JP2016534934A (ja) 2016-11-10

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