BRPI1011548A2 - fixador resistente a relâmpago, cobertura instalada em um extremidade de frente de um membro fixador, e, método para montar um fixador resistente a relâmpago. - Google Patents

fixador resistente a relâmpago, cobertura instalada em um extremidade de frente de um membro fixador, e, método para montar um fixador resistente a relâmpago.

Info

Publication number
BRPI1011548A2
BRPI1011548A2 BRPI1011548A BRPI1011548A BRPI1011548A2 BR PI1011548 A2 BRPI1011548 A2 BR PI1011548A2 BR PI1011548 A BRPI1011548 A BR PI1011548A BR PI1011548 A BRPI1011548 A BR PI1011548A BR PI1011548 A2 BRPI1011548 A2 BR PI1011548A2
Authority
BR
Brazil
Prior art keywords
fastener
lightning
mounting
cover installed
lightning fastener
Prior art date
Application number
BRPI1011548A
Other languages
English (en)
Inventor
Masahiro Bessho
Naomoto Ishikawa
Tamaki Tzuzuki
Toru Hashigami
Toshikatsu Nohara
Wataru Nishimura
Yuichiro Kano
Original Assignee
Mitsubishi Aircraft Corp
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 Mitsubishi Aircraft Corp filed Critical Mitsubishi Aircraft Corp
Publication of BRPI1011548A2 publication Critical patent/BRPI1011548A2/pt
Publication of BRPI1011548B1 publication Critical patent/BRPI1011548B1/pt
Publication of BRPI1011548B8 publication Critical patent/BRPI1011548B8/pt

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
    • F16B33/00—Features common to bolt and nut
    • F16B33/004—Sealing; Insulation
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/01—Locking of screws, bolts or nuts specially adapted to prevent loosening at extreme temperatures
    • 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
    • F16B39/00—Locking of screws, bolts or nuts
    • F16B39/02—Locking of screws, bolts or nuts in which the locking takes place after screwing down
    • F16B39/021—Locking of screws, bolts or nuts in which the locking takes place after screwing down by injecting a settable material after the screwing down
    • 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
    • F16B33/06—Surface treatment of parts furnished with screw-thread, e.g. for preventing seizure or fretting
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49833—Punching, piercing or reaming part by surface of second part
    • Y10T29/49835—Punching, piercing or reaming part by surface of second part with shaping
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Bolts, Nuts, And Washers (AREA)
BRPI1011548A 2009-04-02 2010-04-02 fixador resistente a relâmpago, cobertura instalada em uma extremidade de frente de um membro fixador, e, método para montar um fixador resistente a relâmpago. BRPI1011548B8 (pt)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
JP2009090552 2009-04-02
JP2009-090552 2009-04-02
JP2009279601A JP5610758B2 (ja) 2009-04-02 2009-12-09 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
JP2009-279601 2009-12-09
PCT/JP2010/002429 WO2010113523A1 (ja) 2009-04-02 2010-04-02 耐雷ファスナ、キャップ、耐雷ファスナの取り付け方法

Publications (3)

Publication Number Publication Date
BRPI1011548A2 true BRPI1011548A2 (pt) 2016-03-29
BRPI1011548B1 BRPI1011548B1 (pt) 2020-06-23
BRPI1011548B8 BRPI1011548B8 (pt) 2020-07-07

Family

ID=42827831

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1011548A BRPI1011548B8 (pt) 2009-04-02 2010-04-02 fixador resistente a relâmpago, cobertura instalada em uma extremidade de frente de um membro fixador, e, método para montar um fixador resistente a relâmpago.

Country Status (5)

Country Link
US (2) US8520358B2 (pt)
JP (1) JP5610758B2 (pt)
BR (1) BRPI1011548B8 (pt)
CA (1) CA2755705C (pt)
WO (1) WO2010113523A1 (pt)

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
JP2011098675A (ja) * 2009-11-06 2011-05-19 Mitsubishi Aircraft Corp 耐雷ファスナ、キャップ、ファスナ部材、耐雷ファスナの取り付け方法
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
EP3366593B1 (en) 2011-02-10 2019-10-23 Airbus Operations Limited Cap for forming sealed cavity around fastener
JP5669635B2 (ja) 2011-03-14 2015-02-12 三菱航空機株式会社 機体構成部材の連結構造
JP5822493B2 (ja) 2011-03-16 2015-11-24 三菱航空機株式会社 耐雷ファスナ、航空機組立品、航空機組立部品の製造方法
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
US20130223951A1 (en) * 2011-04-28 2013-08-29 Masahiro Bessho Cap and fixing structure using the same
JP5713789B2 (ja) * 2011-05-06 2015-05-07 三菱航空機株式会社 ファスナ、航空機組立品、航空機組立品の製造方法、および治具
JP5187985B1 (ja) 2011-11-04 2013-04-24 三菱航空機株式会社 耐雷ファスナ、耐雷ファスナのキャップ
JP5901263B2 (ja) * 2011-12-08 2016-04-06 三菱航空機株式会社 耐雷ファスナ
JP5931458B2 (ja) 2012-01-17 2016-06-08 三菱航空機株式会社 耐雷ファスナ、耐雷ファスナの装着方法
US10301033B2 (en) * 2012-02-01 2019-05-28 The Boeing Company Foamed energy absorptive fastener seal cap
DE102012202053A1 (de) 2012-02-10 2013-08-14 Airbus Operations Gmbh Verbindungsanordnung sowie Verfahren
BR112014022061B1 (pt) * 2012-03-08 2021-02-23 Jurblami, S.L. molde de sineta para encapsulamento com vedante moldável
US9802715B2 (en) 2012-03-29 2017-10-31 The Boeing Company Fastener systems that provide EME protection
ES2592556T3 (es) 2012-04-11 2016-11-30 Prc-Desoto International, Inc. Tapas de sellado para placa de tuerca
EP2855274B1 (en) 2012-05-31 2016-11-09 Airbus Operations Limited Injectable nut cap
US9140291B2 (en) * 2012-09-28 2015-09-22 The Boeing Company Apparatus for covering a fastener system
US10051767B2 (en) 2012-09-28 2018-08-14 The Boeing Company Method and apparatus for covering a fastener system
GB201220002D0 (en) 2012-11-06 2012-12-19 Airbus Operations Ltd Cap with channels for forming a sealed cavity around fastener
FR2998015B1 (fr) * 2012-11-12 2015-05-29 Lisi Aerospace Dispositif pour fixation etanche
JP5575218B2 (ja) * 2012-12-17 2014-08-20 三菱航空機株式会社 耐雷ファスナ、耐雷ファスナのキャップ
JP6270317B2 (ja) 2013-01-29 2018-01-31 三菱航空機株式会社 耐雷ファスナのシーラント層成形用治具、耐雷ファスナのシーラント層成形方法、耐雷ファスナ、航空機の翼、耐雷ファスナの成形方法および航空機の翼の製造方法
JP6162964B2 (ja) 2013-01-29 2017-07-12 三菱航空機株式会社 耐雷ファスナのシーラント層成形用治具、耐雷ファスナのシーラント層成形方法
GB201305459D0 (en) 2013-01-30 2013-05-08 Short Brothers Plc Electrical protector
KR20150143647A (ko) 2013-04-15 2015-12-23 쓰리엠 이노베이티브 프로퍼티즈 컴파니 경량 시일 캡
US9650150B2 (en) * 2013-04-15 2017-05-16 3M Innovative Properties Company Translucent seal cap
JP2016522873A (ja) 2013-04-19 2016-08-04 エアバス オペレーションズ リミティド 注入可能なキャップ
US9829030B2 (en) 2013-04-19 2017-11-28 Airbus Operations Limited Injectable cap
KR20150143852A (ko) * 2013-04-22 2015-12-23 피알시-데소토 인터내쇼날, 인코포레이티드 내부 배리어 링을 포함하는 실란트 캡
US20160131179A1 (en) * 2013-06-11 2016-05-12 Systems And Materials Research Corporation Sealant cap
US9188226B2 (en) 2013-07-15 2015-11-17 The Boeing Company Apparatus for installing a seal cap
GB2516835B (en) * 2013-07-31 2015-11-04 Airbus Operations Ltd Cap to accommodate washers
RU2592958C2 (ru) * 2013-11-06 2016-07-27 Зе Боинг Компани Крепежные системы, обеспечивающие защиту от электромагнитных воздействий
DE202013105469U1 (de) * 2013-12-02 2015-03-03 Makita Corporation Befestigungsanordnung, tragbares Arbeitsgerät zum Befestigen eines ersten Gehäuseteils an einem zweiten Gehäuseteil
JP6324784B2 (ja) * 2014-03-24 2018-05-16 三菱重工業株式会社 キャップ、およびキャップの成形型、キャップを用いた固定構造部、キャップの装着方法
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
US11260945B1 (en) * 2015-03-06 2022-03-01 Robert S Patterson Propeller nut
JP6596960B2 (ja) * 2015-06-18 2019-10-30 いすゞ自動車株式会社 変速機のオイルパイプ取付構造
US20180339788A1 (en) * 2017-05-26 2018-11-29 Joe A. Garcia Protective cap and nut gauge for an aircraft fuel tank fastener system
JP7011293B2 (ja) 2017-11-07 2022-02-10 株式会社大日ハンソー バケットコンベヤ装置
JP6434116B2 (ja) * 2017-12-18 2018-12-05 三菱重工業株式会社 キャップ、およびキャップを用いた固定構造部
FR3076815B1 (fr) * 2018-01-18 2020-02-14 Dassault Aviation Assemblage d'aeronef comprenant un capuchon de recouvrement d'une fixation
US11346387B2 (en) * 2018-04-18 2022-05-31 Textron Innovations, Inc. Integral sealant O-ring
US11046422B2 (en) * 2018-07-16 2021-06-29 Pratt & Whitney Canada Corp. Propeller blade angle feedback arrangement and method
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
US10982704B2 (en) * 2019-01-03 2021-04-20 The Boeing Company EME protection cap system with screw sealant mechanism
US11695225B2 (en) 2019-08-19 2023-07-04 Carlisle Interconnect Technologies, Inc. Electrical connector and bonding system

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3897712A (en) * 1974-01-09 1975-08-05 Textron Inc Plastic headed fastener assembly
US4382049A (en) * 1981-11-30 1983-05-03 Mcdonnell Douglas Corporation Forming a lightning spark isolation barrier
JPS5983386A (ja) * 1982-11-04 1984-05-14 エナジーサポート株式会社 避雷手段の劣化表示装置
US4832049A (en) 1985-04-22 1989-05-23 Canon Kabushiki Kaisha Apparatus for detecting abnormality of the spinal column
US4630168A (en) * 1985-12-16 1986-12-16 The Boeing Company Lightning protection fastener
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
US4826380A (en) 1988-01-19 1989-05-02 Ltv Aerospace & Defense Company Pre-cast sealant dome and method
US4905931A (en) * 1988-02-18 1990-03-06 The Boeing Company Arc suppression around fasteners
GB8828025D0 (en) * 1988-12-01 1989-01-05 Atomic Energy Authority Uk Screw fasteners for aeronautical use
GB8924231D0 (en) * 1989-10-27 1989-12-13 British Aerospace Carbon fibre composite structures
FR2668580B1 (fr) * 1990-10-30 1993-01-22 Aerospatiale Structure anti-etincelage, notamment pour aeronef.
JP2548889Y2 (ja) * 1992-09-24 1997-09-24 日本碍子株式会社 避雷ユニット付き碍子
FR2718706B1 (fr) * 1994-04-15 1996-06-14 Aerospatiale Structure anti-étincelage, notamment pour aéronef.
ES2334735B1 (es) * 2007-11-15 2011-01-26 Airbus España S.L. Dispositivo de proteccion contra descargas electricas en elementos defijacion.
ES2332758B1 (es) * 2007-12-10 2011-01-17 Airbus España S.L. Dispositivo integrado de proteccion contra descargas electricas en elementos de fijacion conductores.
JP5055178B2 (ja) * 2008-03-24 2012-10-24 三菱重工業株式会社 航空機組立品
FR2930682B1 (fr) * 2008-04-29 2010-05-21 Airbus France Ensemble comprenant une antenne de radiolignement de descente et un organe support
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
JP2011098675A (ja) * 2009-11-06 2011-05-19 Mitsubishi Aircraft Corp 耐雷ファスナ、キャップ、ファスナ部材、耐雷ファスナの取り付け方法
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
JP5669635B2 (ja) * 2011-03-14 2015-02-12 三菱航空機株式会社 機体構成部材の連結構造
JP5822493B2 (ja) * 2011-03-16 2015-11-24 三菱航空機株式会社 耐雷ファスナ、航空機組立品、航空機組立部品の製造方法
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

Also Published As

Publication number Publication date
US20150344151A1 (en) 2015-12-03
US20120074257A1 (en) 2012-03-29
JP5610758B2 (ja) 2014-10-22
US9334065B2 (en) 2016-05-10
BRPI1011548B1 (pt) 2020-06-23
WO2010113523A1 (ja) 2010-10-07
CA2755705C (en) 2014-07-08
JP2010254287A (ja) 2010-11-11
US8520358B2 (en) 2013-08-27
BRPI1011548B8 (pt) 2020-07-07
CA2755705A1 (en) 2010-10-07

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