ES2608357T3 - Conjunto de dispositivo de sujeción con manguito - Google Patents

Conjunto de dispositivo de sujeción con manguito Download PDF

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Publication number
ES2608357T3
ES2608357T3 ES13821347.5T ES13821347T ES2608357T3 ES 2608357 T3 ES2608357 T3 ES 2608357T3 ES 13821347 T ES13821347 T ES 13821347T ES 2608357 T3 ES2608357 T3 ES 2608357T3
Authority
ES
Spain
Prior art keywords
gap
counterbore
sleeve
frame
clamping
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.)
Active
Application number
ES13821347.5T
Other languages
English (en)
Inventor
Russell J. Heeter
John A. Ward
Thu A. Nguyen
Jeffrey A. Wilkerson
John R. Porter
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2608357T3 publication Critical patent/ES2608357T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/28—Clamped connections, spring connections
    • H01R4/30—Clamped connections, spring connections utilising a screw or nut clamping member
    • H01R4/304—Clamped connections, spring connections utilising a screw or nut clamping member having means for improving contact
    • 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
    • F16B33/006—Non-metallic fasteners using screw-thread
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R43/00—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors
    • H01R43/16—Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for manufacturing contact members, e.g. by punching and by bending
    • 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
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/93—Fastener comprising feature for establishing a good electrical connection, e.g. electrostatic discharge or insulation feature

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Connection Of Plates (AREA)
  • Bolts, Nuts, And Washers (AREA)
  • Clamps And Clips (AREA)
  • Studio Devices (AREA)

Abstract

Un sistema de sujeción con manguito conductor (200) para unir una primera estructura (210) con una segunda estructura (240), que comprende: una primera estructura (210) con una superficie superior (215) y una primera superficie de cara (220), con un primer hueco (225) allí; una segunda estructura (240) con una segunda superficie de cara (245) y una superficie inferior (240), con un segundo hueco allí (255); un dispositivo de sujeción eléctricamente conductor (105) con un cabezal de sujeción (110) y una pata de sujeción (120) que se extiende desde dicho cabezal de sujeción; un manguito de sujeción eléctricamente conductor (130) configurado para entrar a través de dicho primer hueco (225) y dicho segundo hueco (255) cuando dicho primer hueco y dicho segundo hueco están alineados, y configurados para recibir dicha pata de sujeción (120) de dicho sujeción, el manguito de sujeción (130) además comprende un extremo sobresaliente (145) configurado para extenderse más allá de la superficie inferior (250) de la segunda estructura (240) cuando el manguito de sujeción está dispuesto a través de dicho primer hueco y dicho segundo hueco; y una tuerca (150) configurada para unirse a la pata de sujeción (120), la tuerca tiene un contrataladro (155) formado allí, el contrataladro tiene: un diámetro de contrataladro con un tamaño como para mantener un espacio radial (185) entre una superficie de cara hacia adentro (160) del contrataladro y una superficie exterior (140) del manguito de sujeción (130); y una profundidad de contrataladro con un tamaño como para mantener un espacio axial (190) entre un extremo distal del manguito de sujeción y una superficie inferior (165) del contrataladro (155); caracterizada por que el contrataladro (155) además comprende una tira (180) entre la superficie de cara hacia adentro (160) y la superficie inferior (165).

Description

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Claims (1)

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ES13821347.5T 2013-02-04 2013-12-20 Conjunto de dispositivo de sujeción con manguito Active ES2608357T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/758,612 US9343824B2 (en) 2013-02-04 2013-02-04 Sleeved fastener assembly
US201313758612 2013-02-04
PCT/US2013/077087 WO2014120362A1 (en) 2013-02-04 2013-12-20 Sleeved fastener assembly

Publications (1)

Publication Number Publication Date
ES2608357T3 true ES2608357T3 (es) 2017-04-10

Family

ID=49956462

Family Applications (1)

Application Number Title Priority Date Filing Date
ES13821347.5T Active ES2608357T3 (es) 2013-02-04 2013-12-20 Conjunto de dispositivo de sujeción con manguito

Country Status (6)

Country Link
US (2) US9343824B2 (es)
EP (1) EP2951095B1 (es)
JP (1) JP6370314B2 (es)
CN (1) CN105008224B (es)
ES (1) ES2608357T3 (es)
WO (1) WO2014120362A1 (es)

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US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
JP6139582B2 (ja) 2015-02-23 2017-05-31 株式会社Ｓｕｂａｒｕ 航空機用構造体、航空機用構造体の製造方法及び航空機用構造体の設計情報の作成方法
US10329031B2 (en) * 2016-06-17 2019-06-25 Goodrich Corporation Electricity dispersion for aircraft evacuation assemblies
US10179640B2 (en) * 2016-08-24 2019-01-15 The Boeing Company Wing and method of manufacturing
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US20190061803A1 (en) * 2017-08-28 2019-02-28 Fuji Kiko Co., Ltd. Electric steering column apparatus
US11047417B2 (en) * 2018-10-11 2021-06-29 GM Global Technology Operations LLC Fastening assembly
CN109850124A (zh) * 2018-12-12 2019-06-07 惠阳航空螺旋桨有限责任公司 一种螺旋桨复合材料整流罩紧固装置
US11396900B2 (en) * 2019-05-10 2022-07-26 The Boeing Company Fastener and methods of manufacturing and use
FR3102945B1 (fr) * 2019-11-13 2022-03-25 Airbus Operations Sas Procédé de réparation d’un assemblage comportant au moins un boulon et assemblage ainsi réparé
CN112072335B (zh) * 2020-09-25 2022-06-24 中国直升机设计研究所 一种复合材料结构件之间导电结构及导电处理方法

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Also Published As

Publication number Publication date
EP2951095A1 (en) 2015-12-09
CN105008224B (zh) 2017-05-31
JP2016511185A (ja) 2016-04-14
US20160261052A1 (en) 2016-09-08
WO2014120362A1 (en) 2014-08-07
EP2951095B1 (en) 2016-09-21
US9343824B2 (en) 2016-05-17
US10186788B2 (en) 2019-01-22
CN105008224A (zh) 2015-10-28
JP6370314B2 (ja) 2018-08-08
US20140219745A1 (en) 2014-08-07

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