JP5901516B2 - 改良型ウイング構造体 - Google Patents

改良型ウイング構造体 Download PDF

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Publication number
JP5901516B2
JP5901516B2 JP2012504081A JP2012504081A JP5901516B2 JP 5901516 B2 JP5901516 B2 JP 5901516B2 JP 2012504081 A JP2012504081 A JP 2012504081A JP 2012504081 A JP2012504081 A JP 2012504081A JP 5901516 B2 JP5901516 B2 JP 5901516B2
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JP
Japan
Prior art keywords
spar
wing structure
attached
wing
cap
Prior art date
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Expired - Fee Related
Application number
JP2012504081A
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English (en)
Japanese (ja)
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JP2012523348A (ja
JP2012523348A5 (enExample
Inventor
マイケル タッカー
マイケル タッカー
ティモシー サンダーソン
ティモシー サンダーソン
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Airbus Operations Ltd
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Airbus Operations Ltd
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Publication date
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
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Publication of JP2012523348A5 publication Critical patent/JP2012523348A5/ja
Application granted granted Critical
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/34Tanks constructed integrally with wings, e.g. for fuel or water
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
JP2012504081A 2009-04-09 2010-03-31 改良型ウイング構造体 Expired - Fee Related JP5901516B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0906157.3 2009-04-09
GBGB0906157.3A GB0906157D0 (en) 2009-04-09 2009-04-09 Improved wing structure
PCT/GB2010/050555 WO2010116170A2 (en) 2009-04-09 2010-03-31 Improved wing structure

Publications (3)

Publication Number Publication Date
JP2012523348A JP2012523348A (ja) 2012-10-04
JP2012523348A5 JP2012523348A5 (enExample) 2013-04-25
JP5901516B2 true JP5901516B2 (ja) 2016-04-13

Family

ID=40750359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012504081A Expired - Fee Related JP5901516B2 (ja) 2009-04-09 2010-03-31 改良型ウイング構造体

Country Status (7)

Country Link
US (1) US8616499B2 (enExample)
EP (1) EP2417022B1 (enExample)
JP (1) JP5901516B2 (enExample)
CN (1) CN102387963B (enExample)
CA (1) CA2755557A1 (enExample)
GB (1) GB0906157D0 (enExample)
WO (1) WO2010116170A2 (enExample)

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FR2981880B1 (fr) * 2011-10-28 2014-09-19 Daher Aerospace Procede pour etancher un reservoir de carburant
CN103434638A (zh) * 2013-09-16 2013-12-11 哈尔滨工业大学 复合材料机翼中梁与加强肋的混合连接方法
US9994298B2 (en) 2015-06-30 2018-06-12 Lockheed Martin Corporation System for embedded removable aperture
CN105627836B (zh) * 2016-02-18 2018-08-24 江西洪都航空工业集团有限责任公司 一种组合梁式翼面结构
GB2550403A (en) * 2016-05-19 2017-11-22 Airbus Operations Ltd Aerofoil body with integral curved spar-cover
US10556665B2 (en) * 2016-06-20 2020-02-11 The Boeing Company Apparatuses and methods for improved sealing
US10745147B2 (en) * 2016-11-11 2020-08-18 Bell Helicopter Textron Inc. Detachable cargo mirror
CN107244409B (zh) * 2017-05-31 2019-08-09 彩虹无人机科技有限公司 一种复合材料机翼整体油箱结构
ES2800182T3 (es) * 2017-07-13 2020-12-28 Airbus Operations Sl Disposición estructural de caja para una aeronave y procedimiento de fabricación de la misma
CN108100224B (zh) * 2018-01-17 2020-12-25 安徽中骄智能科技有限公司 一种集成电池平凸翼式无人机
CN109305328B (zh) * 2018-11-12 2024-01-16 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种翼盒及飞机
CN110525634B (zh) * 2019-09-09 2021-03-23 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种尾翼后缘舱与主盒段的连接结构
GB2587671A (en) * 2019-10-02 2021-04-07 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
DE102022116949A1 (de) * 2022-07-07 2024-01-18 Airbus Operations Gmbh Tragfläche für ein Luftfahrzeug

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GB130695A (en) 1918-03-16 1919-08-14 Henry William Phillips Improvements in Beams, Spars, Ribs, or the like, for Aerial Machines.
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GB491302A (en) 1937-03-24 1938-08-30 Messerschmitt Boelkow Blohm Improvements in and relating to bracing members for the wings, steering surfaces and the like of aircraft
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US3907442A (en) 1972-11-01 1975-09-23 Briles Manufacturing Omark Ind Fastener sealant injection system
JPS5330599A (en) * 1976-08-30 1978-03-22 Boeing Co Aerodynamic rotary wing composite construction and method of manufacturing thereof
FR2381662A1 (fr) * 1977-02-28 1978-09-22 Aerospatiale Pale, notamment pour un rotor d'helicoptere, et son procede de fabrication
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JPS63258297A (ja) * 1987-04-16 1988-10-25 富士重工業株式会社 複合材による箱形構造体の補強構造
JPH0751997Y2 (ja) * 1990-07-13 1995-11-29 三菱重工業株式会社 複合材外板のインジェクションシール用穴のプラグ
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JPH07172395A (ja) * 1993-12-20 1995-07-11 Mitsubishi Heavy Ind Ltd 航空機のインテグラルタンク
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US7249943B2 (en) * 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
US7264200B2 (en) * 2004-07-23 2007-09-04 The Boeing Company System and method for improved rotor tip performance
EP1674389B1 (de) 2004-12-22 2007-09-12 Airbus Deutschland GmbH (HRB 43527) Tragwerk einer aerodynamischen Wirkfläche eines Flugzeugs
US7686905B2 (en) * 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
FI119726B (fi) * 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
EP1946913B1 (en) * 2007-01-22 2011-03-16 Saab Ab Method and apparatus for manufacturing a wing spar profile element
US7905706B1 (en) * 2007-12-21 2011-03-15 Florida Turbine Technologies, Inc. Turbine blade with spar and shell cooling
US8165703B2 (en) * 2008-08-18 2012-04-24 Airbus Operations S.L. Computer assisted method for the advanced design of bent parts of composite material
US7901184B2 (en) * 2009-06-16 2011-03-08 General Electric Company Torsionally loadable wind turbine blade

Also Published As

Publication number Publication date
WO2010116170A3 (en) 2011-01-13
CN102387963A (zh) 2012-03-21
CN102387963B (zh) 2015-05-20
CA2755557A1 (en) 2010-10-14
EP2417022A2 (en) 2012-02-15
JP2012523348A (ja) 2012-10-04
GB0906157D0 (en) 2009-05-20
EP2417022B1 (en) 2013-11-06
WO2010116170A2 (en) 2010-10-14
US20120037755A1 (en) 2012-02-16
US8616499B2 (en) 2013-12-31

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