WO2008143092A1 - 航空機組立品およびその製造方法 - Google Patents

航空機組立品およびその製造方法 Download PDF

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Publication number
WO2008143092A1
WO2008143092A1 PCT/JP2008/058856 JP2008058856W WO2008143092A1 WO 2008143092 A1 WO2008143092 A1 WO 2008143092A1 JP 2008058856 W JP2008058856 W JP 2008058856W WO 2008143092 A1 WO2008143092 A1 WO 2008143092A1
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft assembly
outer board
manufacturing
same
fastener
Prior art date
Application number
PCT/JP2008/058856
Other languages
English (en)
French (fr)
Inventor
Kazuyuki Oguri
Takahiro Sekigawa
Original Assignee
Mitsubishi Heavy Industries, 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
Application filed by Mitsubishi Heavy Industries, Ltd. filed Critical Mitsubishi Heavy Industries, Ltd.
Priority to EP08752727.1A priority Critical patent/EP2147855A4/en
Priority to CA2677311A priority patent/CA2677311C/en
Priority to US12/525,177 priority patent/US8482897B2/en
Priority to BRPI0807353-8A priority patent/BRPI0807353A2/pt
Publication of WO2008143092A1 publication Critical patent/WO2008143092A1/ja

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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

Abstract

　耐久性が向上するとともに良好な耐雷性を備え得る航空機組立品を提供する。繊維で強化された外板用樹脂材料を主たる要素として構成された外板（５）と、この外板（５）を内側から支持する構造材（７）と、これら外板（５）と構造材（７）とを結合するファスナ（３）とを備えている航空機組立品（１）であって、少なくともファスナ（３）の頭部（１７）を覆うように設置された絶縁性を有する絶縁体層（２３）と、少なくとも絶縁体層（２３）を覆うように設置され、導電性を有する銅の粉末を含有する導電層用樹脂材料で形成された導電体層（２５）と、を備えている航空機組立品を提供する。
PCT/JP2008/058856 2007-05-21 2008-05-14 航空機組立品およびその製造方法 WO2008143092A1 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP08752727.1A EP2147855A4 (en) 2007-05-21 2008-05-14 AIRCRAFT ASSEMBLY AND METHOD FOR THE PRODUCTION THEREOF
CA2677311A CA2677311C (en) 2007-05-21 2008-05-14 Aircraft assembly and method for manufacturing the same
US12/525,177 US8482897B2 (en) 2007-05-21 2008-05-14 Aircraft assembly and method for manufacturing the same
BRPI0807353-8A BRPI0807353A2 (pt) 2007-05-21 2008-05-14 Conjunto de aeronave e método de fabricação do mesmo

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2007134473A JP2008285115A (ja) 2007-05-21 2007-05-21 航空機組立品およびその製造方法
JP2007-134473 2007-05-21

Publications (1)

Publication Number Publication Date
WO2008143092A1 true WO2008143092A1 (ja) 2008-11-27

Family

ID=40031801

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2008/058856 WO2008143092A1 (ja) 2007-05-21 2008-05-14 航空機組立品およびその製造方法

Country Status (6)

Country Link
US (1) US8482897B2 (ja)
EP (1) EP2147855A4 (ja)
JP (1) JP2008285115A (ja)
BR (1) BRPI0807353A2 (ja)
CA (1) CA2677311C (ja)
WO (1) WO2008143092A1 (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010537881A (ja) * 2007-08-30 2010-12-09 ザ・ボーイング・カンパニー ファスナ取り付け前の落雷保護システムの高速点検
JP2013224142A (ja) * 2009-04-02 2013-10-31 Mitsubishi Aircraft Corp 耐雷ファスナ、航空機、耐雷ファスナの取り付け方法

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4719203B2 (ja) * 2007-09-28 2011-07-06 三菱重工業株式会社 耐雷ファスナ
ES2376323B1 (es) * 2009-02-27 2013-01-24 Airbus Operations, S.L. Mejora de la protección contra impacto directo de rayos en zonas remachadas de paneles en cfrp.
BR112012000203B1 (pt) * 2009-06-12 2020-01-28 Lord Corp método para proteção de um substrato contra relâmpagos
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
US9108363B2 (en) 2011-10-06 2015-08-18 The Boeing Company Thin wall bushing for robust electrical bonding to fiber-reinforced structures
US20140331477A1 (en) * 2013-05-07 2014-11-13 The Boeing Company Flush fastener design and installation
US9481157B2 (en) * 2014-03-06 2016-11-01 The Boeing Company Repair apparatus and method for composite panels having a conductive layer
US9845142B2 (en) * 2014-08-15 2017-12-19 The Boeing Company Conductive thermoplastic ground plane for use in an aircraft
US20160229552A1 (en) * 2015-02-05 2016-08-11 The Boeing Company Intermetallic and composite metallic gap filler
US10329031B2 (en) * 2016-06-17 2019-06-25 Goodrich Corporation Electricity dispersion for aircraft evacuation assemblies

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
US4630168A (en) 1985-12-16 1986-12-16 The Boeing Company Lightning protection fastener
US4681497A (en) * 1985-05-29 1987-07-21 Microdot Inc. Encapsulated fastener
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
US5845872A (en) 1994-06-02 1998-12-08 British Aerospace Plc Method and arrangement for fastening composite aircraft skins
JP2001093336A (ja) * 1999-09-22 2001-04-06 Fuji Photo Film Co Ltd 透明導電性フイルムおよびそのアース方法
US7050286B2 (en) * 2003-05-30 2006-05-23 Bae Systems Plc Composite structure lighting protection
JP2007005442A (ja) * 2005-06-22 2007-01-11 Toppan Printing Co Ltd 導電性転写箔およびそれを使用したｉｃカード

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2326455A (en) 1942-03-13 1943-08-10 Glenn L Martin Co Fastening means
FR1069237A (fr) 1952-12-29 1954-07-06 Ferodo Sa Rivet pour garnitures de friction
US3494243A (en) * 1967-06-28 1970-02-10 Standard Pressed Steel Co Sealing fastener
US3618444A (en) * 1969-05-16 1971-11-09 Usm Corp Corrosion resistant fasteners
US3755713A (en) * 1972-07-25 1973-08-28 Boeing Co Electrically conductive surface for aircraft
US4235147A (en) 1978-08-16 1980-11-25 The Atlas Bolt & Screw Company Fastener having sealing head
US4316690A (en) 1980-05-14 1982-02-23 Voller Ronald L Capped bolt
US4460300A (en) * 1982-01-11 1984-07-17 Illinois Tool Works Inc. Fastener with head cap having a concealed edge
US4628402A (en) * 1985-09-30 1986-12-09 The Boeing Company Lightning protection of fasteners in composite material
US5035764A (en) * 1987-08-28 1991-07-30 Wasatch Fiber Group, Inc. Cohesive finishes for composite materials
US4884929A (en) 1987-12-21 1989-12-05 Lockheed Corporation Flush head fastener
JPH0318045A (ja) 1989-06-14 1991-01-25 Matsushita Electron Corp 半導体装置
JP2701144B2 (ja) 1995-11-27 1998-01-21 株式会社丸エム製作所 トルクリミット付きボルト
JP3502357B2 (ja) 1996-02-28 2004-03-02 グローバルメディアオンライン株式会社 端末装置及び通信システム
US5868356A (en) * 1996-09-13 1999-02-09 The Boeing Company Fastener system using biangular countersink geometry
JPH10184633A (ja) 1996-12-24 1998-07-14 Aoyama Seisakusho Co Ltd ボルト
CN2354219Y (zh) 1998-09-18 1999-12-15 谷杏石 合成绝缘氧化锌避雷器
JP4436954B2 (ja) 2000-03-02 2010-03-24 トーカロ株式会社 耐摩耗性等の表面特性に優れるプラスチック基複合材料およびその製造方法
US6679667B2 (en) * 2001-02-28 2004-01-20 Northrop Grumman Corporation Hot melt fastener filler
US6953509B2 (en) * 2003-06-03 2005-10-11 The Boeing Company Method for preparing pre-coated, metallic components and components prepared thereby
DE102004060782B3 (de) 2004-12-17 2006-03-09 Harting Electronics Gmbh & Co. Kg Geschirmter, hochpoliger Leiterplattensteckverbinder
US20060177284A1 (en) * 2005-02-07 2006-08-10 The Boeing Company Method for preparing pre-coated aluminum and aluminum-alloy fasteners and components having high-shear strength and readily deformable regions
JP4786426B2 (ja) 2005-10-06 2011-10-05 三菱重工業株式会社 ファスナ
US7599164B2 (en) * 2006-12-07 2009-10-06 The Boeing Company Lightning protection system for aircraft composite structure
US7883050B2 (en) * 2007-06-28 2011-02-08 The Boeing Company Composites with integrated multi-functional circuits

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
US4681497A (en) * 1985-05-29 1987-07-21 Microdot Inc. Encapsulated fastener
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
US5845872A (en) 1994-06-02 1998-12-08 British Aerospace Plc Method and arrangement for fastening composite aircraft skins
JP2001093336A (ja) * 1999-09-22 2001-04-06 Fuji Photo Film Co Ltd 透明導電性フイルムおよびそのアース方法
US7050286B2 (en) * 2003-05-30 2006-05-23 Bae Systems Plc Composite structure lighting protection
JP2007005442A (ja) * 2005-06-22 2007-01-11 Toppan Printing Co Ltd 導電性転写箔およびそれを使用したｉｃカード

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP2147855A4

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010537881A (ja) * 2007-08-30 2010-12-09 ザ・ボーイング・カンパニー ファスナ取り付け前の落雷保護システムの高速点検
JP2013224142A (ja) * 2009-04-02 2013-10-31 Mitsubishi Aircraft Corp 耐雷ファスナ、航空機、耐雷ファスナの取り付け方法

Also Published As

Publication number Publication date
EP2147855A1 (en) 2010-01-27
BRPI0807353A2 (pt) 2014-05-06
US20100108804A1 (en) 2010-05-06
EP2147855A4 (en) 2013-08-14
CA2677311A1 (en) 2008-11-27
JP2008285115A (ja) 2008-11-27
CA2677311C (en) 2012-06-26
US8482897B2 (en) 2013-07-09

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