JPH01263030A - 複合材のファスナ継手 - Google Patents

複合材のファスナ継手

Info

Publication number
JPH01263030A
JPH01263030A JP9170488A JP9170488A JPH01263030A JP H01263030 A JPH01263030 A JP H01263030A JP 9170488 A JP9170488 A JP 9170488A JP 9170488 A JP9170488 A JP 9170488A JP H01263030 A JPH01263030 A JP H01263030A
Authority
JP
Japan
Prior art keywords
fastener
joint
hole
parts
fastener joint
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.)
Granted
Application number
JP9170488A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0455859B2 (2
Inventor
Hiromichi Koiwai
弘道 小祝
Tamon Ikeda
池田　多門
Takeo Inatomi
丈夫 稲富
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.)
National Institute of Advanced Industrial Science and Technology AIST
Original Assignee
Agency of Industrial Science and Technology
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 Agency of Industrial Science and Technology filed Critical Agency of Industrial Science and Technology
Priority to JP9170488A priority Critical patent/JPH01263030A/ja
Publication of JPH01263030A publication Critical patent/JPH01263030A/ja
Publication of JPH0455859B2 publication Critical patent/JPH0455859B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
JP9170488A 1988-04-15 1988-04-15 複合材のファスナ継手 Granted JPH01263030A (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9170488A JPH01263030A (ja) 1988-04-15 1988-04-15 複合材のファスナ継手

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9170488A JPH01263030A (ja) 1988-04-15 1988-04-15 複合材のファスナ継手

Publications (2)

Publication Number Publication Date
JPH01263030A true JPH01263030A (ja) 1989-10-19
JPH0455859B2 JPH0455859B2 (2) 1992-09-04

Family

ID=14033902

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9170488A Granted JPH01263030A (ja) 1988-04-15 1988-04-15 複合材のファスナ継手

Country Status (1)

Country Link
JP (1) JPH01263030A (2)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1316420A1 (en) * 2001-11-29 2003-06-04 Saint-Gobain Technical Fabrics Energy absorbant laminate for mechanical composite joints
WO2011043346A1 (ja) * 2009-10-08 2011-04-14 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
WO2012105691A1 (ja) * 2011-02-04 2012-08-09 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
WO2013129122A1 (ja) * 2012-02-29 2013-09-06 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
WO2015146690A1 (ja) * 2014-03-28 2015-10-01 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7087296B2 (en) 2001-11-29 2006-08-08 Saint-Gobain Technical Fabrics Canada, Ltd. Energy absorbent laminate
EP1316420A1 (en) * 2001-11-29 2003-06-04 Saint-Gobain Technical Fabrics Energy absorbant laminate for mechanical composite joints
JP5308533B2 (ja) * 2009-10-08 2013-10-09 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
WO2011043346A1 (ja) * 2009-10-08 2011-04-14 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
CN102481971A (zh) * 2009-10-08 2012-05-30 三菱重工业株式会社 复合材料构造体、具备该构造体的航空器主翼及航空器机身
US9108718B2 (en) 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
WO2012105691A1 (ja) * 2011-02-04 2012-08-09 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
JP5654055B2 (ja) * 2011-02-04 2015-01-14 三菱重工業株式会社 複合材構造体、これを備えた航空機主翼および航空機胴体
RU2553608C2 (ru) * 2011-02-04 2015-06-20 Мицубиси Хеви Индастрис, Лтд. Конструкция из композитного материала и оснащенные ей крыло и фюзеляж летательного аппарата
CN103201167A (zh) * 2011-02-04 2013-07-10 三菱重工业株式会社 复合材料构造体、具备此构造体的飞机主翼及飞机机身
EP2671792A4 (en) * 2011-02-04 2018-01-03 MITSUBISHI HEAVY INDUSTRIES, Ltd. Composite material structure, and aircraft wing and fuselage provided therewith
JP2013180627A (ja) * 2012-02-29 2013-09-12 Mitsubishi Heavy Ind Ltd 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
WO2013129122A1 (ja) * 2012-02-29 2013-09-06 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
EP2821340A4 (en) * 2012-02-29 2015-12-02 Mitsubishi Heavy Ind Ltd COMPOSITE STRUCTURAL BODY, PLANE WING AND AIRPLANE HULL, AND METHOD FOR PRODUCING THE COMPOSITE STRUCTURAL STRUCTURE BODY
US9475568B2 (en) 2012-02-29 2016-10-25 Mitsubishi Heavy Industries, Ltd. Composite structure, aircraft wing and aircraft fuselage including composite structure, and method of manufacturing composite structure
WO2015146690A1 (ja) * 2014-03-28 2015-10-01 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
JP2015189082A (ja) * 2014-03-28 2015-11-02 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
RU2645500C1 (ru) * 2014-03-28 2018-02-21 Мицубиси Хеви Индастрис, Лтд. Конструкция из композиционного материала и содержащие ее крыло летательного аппарата и фюзеляж летательного аппарата, способ изготовления конструкции из композиционного материала
US10137664B2 (en) 2014-03-28 2018-11-27 Mitsubishi Heavy Industries, Ltd. Composite material structure, aircraft wing and aircraft fuselage provided with same, and method for manufacturing composite material structure

Also Published As

Publication number Publication date
JPH0455859B2 (2) 1992-09-04

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Legal Events

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