JP5808111B2 - 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 - Google Patents

航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 Download PDF

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Publication number
JP5808111B2
JP5808111B2 JP2011023154A JP2011023154A JP5808111B2 JP 5808111 B2 JP5808111 B2 JP 5808111B2 JP 2011023154 A JP2011023154 A JP 2011023154A JP 2011023154 A JP2011023154 A JP 2011023154A JP 5808111 B2 JP5808111 B2 JP 5808111B2
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Japan
Prior art keywords
structural member
aircraft
hole
main wing
members
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Expired - Fee Related
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JP2011023154A
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English (en)
Japanese (ja)
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JP2012162147A5 (OSRAM
JP2012162147A (ja
Inventor
雄也 田中
雄也 田中
鈴木　秀之
秀之 鈴木
豊 金山
豊 金山
一貴 佐藤
一貴 佐藤
正剛 波多野
正剛 波多野
齋藤　暁
暁 齋藤
晃永 渡邉
晃永 渡邉
良 安倍
良 安倍
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Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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Publication date
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Priority to JP2011023154A priority Critical patent/JP5808111B2/ja
Priority to CN201280003462.8A priority patent/CN103180207B/zh
Priority to EP12742098.2A priority patent/EP2671794B1/en
Priority to PCT/JP2012/051699 priority patent/WO2012105415A1/ja
Priority to US13/881,590 priority patent/US9751608B2/en
Publication of JP2012162147A publication Critical patent/JP2012162147A/ja
Publication of JP2012162147A5 publication Critical patent/JP2012162147A5/ja
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Publication of JP5808111B2 publication Critical patent/JP5808111B2/ja
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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
JP2011023154A 2011-02-04 2011-02-04 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体 Expired - Fee Related JP5808111B2 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2011023154A JP5808111B2 (ja) 2011-02-04 2011-02-04 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
CN201280003462.8A CN103180207B (zh) 2011-02-04 2012-01-26 复合材料构造体、具备该复合材料构造体的航空器主翼及航空器机身
EP12742098.2A EP2671794B1 (en) 2011-02-04 2012-01-26 Composite material structure, and aircraft wing and fuselage provided therewith
PCT/JP2012/051699 WO2012105415A1 (ja) 2011-02-04 2012-01-26 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
US13/881,590 US9751608B2 (en) 2011-02-04 2012-01-26 Composite material structure, and aircraft wing and aircraft fuselage provided therewith

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011023154A JP5808111B2 (ja) 2011-02-04 2011-02-04 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体

Publications (3)

Publication Number Publication Date
JP2012162147A JP2012162147A (ja) 2012-08-30
JP2012162147A5 JP2012162147A5 (OSRAM) 2014-03-20
JP5808111B2 true JP5808111B2 (ja) 2015-11-10

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JP2011023154A Expired - Fee Related JP5808111B2 (ja) 2011-02-04 2011-02-04 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体

Country Status (5)

Country Link
US (1) US9751608B2 (OSRAM)
EP (1) EP2671794B1 (OSRAM)
JP (1) JP5808111B2 (OSRAM)
CN (1) CN103180207B (OSRAM)
WO (1) WO2012105415A1 (OSRAM)

Cited By (1)

* Cited by examiner, † Cited by third party
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US11040512B2 (en) 2017-11-08 2021-06-22 Northrop Grumman Systems Corporation Composite structures, forming apparatuses and related systems and methods

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* Cited by examiner, † Cited by third party
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JP6004669B2 (ja) 2012-02-29 2016-10-12 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
US20150203187A1 (en) * 2013-04-02 2015-07-23 The Boeing Company Continuously Curved Spar and Method of Manufacturing
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