DE69911507D1 - Flügelstruktur aus Faserverbundstoff - Google Patents

Flügelstruktur aus Faserverbundstoff

Info

Publication number
DE69911507D1
DE69911507D1 DE69911507T DE69911507T DE69911507D1 DE 69911507 D1 DE69911507 D1 DE 69911507D1 DE 69911507 T DE69911507 T DE 69911507T DE 69911507 T DE69911507 T DE 69911507T DE 69911507 D1 DE69911507 D1 DE 69911507D1
Authority
DE
Germany
Prior art keywords
wing structure
composite wing
composite
wing
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.)
Expired - Fee Related
Application number
DE69911507T
Other languages
English (en)
Other versions
DE69911507T2 (de
Inventor
Kazuaki Amaoka
Hideyuki Sano
Naoya Takizawa
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.)
Subaru Corp
Original Assignee
Fuji Jukogyo KK
Fuji 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 Fuji Jukogyo KK, Fuji Heavy Industries Ltd filed Critical Fuji Jukogyo KK
Application granted granted Critical
Publication of DE69911507D1 publication Critical patent/DE69911507D1/de
Publication of DE69911507T2 publication Critical patent/DE69911507T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
DE69911507T 1998-06-23 1999-06-22 Flügelstruktur aus Faserverbundstoff Expired - Fee Related DE69911507T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP10176093A JP2000006893A (ja) 1998-06-23 1998-06-23 複合材翼構造
JP17609398 1998-06-23

Publications (2)

Publication Number Publication Date
DE69911507D1 true DE69911507D1 (de) 2003-10-30
DE69911507T2 DE69911507T2 (de) 2004-06-24

Family

ID=16007588

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69911507T Expired - Fee Related DE69911507T2 (de) 1998-06-23 1999-06-22 Flügelstruktur aus Faserverbundstoff

Country Status (4)

Country Link
US (1) US6237873B1 (de)
EP (1) EP0967147B1 (de)
JP (1) JP2000006893A (de)
DE (1) DE69911507T2 (de)

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US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
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US9669579B2 (en) 2008-11-13 2017-06-06 The Boeing Company Aircraft skin attachment system
ES2790390T3 (es) 2008-12-05 2020-10-27 Vestas Wind Sys As Palas de turbina eólica eficientes, estructuras de pala de turbina eólica, y sistemas y métodos asociados de fabricación, de montaje y de utilización
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
GB0906157D0 (en) * 2009-04-09 2009-05-20 Airbus Uk Ltd Improved wing structure
EP2487106B1 (de) 2009-10-08 2018-07-25 Mitsubishi Heavy Industries, Ltd. Verbundstoffmaterialstruktur, sowie flugzeugtragfläche und damit ausgestatteter flugzeugrumpf
JP5430424B2 (ja) * 2010-01-28 2014-02-26 本田技研工業株式会社 航空機翼構造の成形方法
DE102010002720A1 (de) * 2010-03-10 2011-09-15 Aloys Wobben Windenergieanlagen-Rotorblatt
US9500179B2 (en) 2010-05-24 2016-11-22 Vestas Wind Systems A/S Segmented wind turbine blades with truss connection regions, and associated systems and methods
JP5808112B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 複合材構造体およびこれを備えた航空機主翼
JP5808111B2 (ja) 2011-02-04 2015-11-10 三菱重工業株式会社 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
JP6100461B2 (ja) * 2011-12-27 2017-03-22 三菱航空機株式会社 ベント部材、航空機の主翼
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US9527575B2 (en) * 2012-11-26 2016-12-27 The Boeing Company Multi-box wing spar and skin
US9446835B2 (en) 2013-01-16 2016-09-20 Otto Aviation Group Aircraft wing
US8973871B2 (en) 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US9470205B2 (en) 2013-03-13 2016-10-18 Vestas Wind Systems A/S Wind turbine blades with layered, multi-component spars, and associated systems and methods
GB2515044A (en) * 2013-06-12 2014-12-17 Airbus Operations Ltd Aircraft wing arrangement
FR3015426B1 (fr) * 2013-12-20 2017-10-27 Airbus Operations Sas Procede de realisation d'un caisson central de voilure
EP2886449A1 (de) * 2013-12-23 2015-06-24 Airbus Operations S.L. Vorderkante für eine Flugzeugsauftriebsfläche
US10272619B2 (en) * 2014-05-19 2019-04-30 The Boeing Company Manufacture of a resin infused one-piece composite truss structure
DE102015103021A1 (de) * 2015-03-03 2016-09-08 Ellergon Antriebstechnik Gesellschaft M.B.H. Hydrofoilfinne
EP3095691A1 (de) * 2015-05-22 2016-11-23 Airbus Operations, S.L. Mehrholmtorsionskastenstruktur
US10724994B2 (en) 2015-12-15 2020-07-28 University Of South Carolina Structural health monitoring method and system
US10421528B2 (en) 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
US10207789B2 (en) 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US10609771B2 (en) 2016-08-18 2020-03-31 University Of South Carolina Printable susceptor for use in induction welding
US20180086429A1 (en) * 2016-09-28 2018-03-29 The Boeing Company Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar
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US5332178A (en) * 1992-06-05 1994-07-26 Williams International Corporation Composite wing and manufacturing process thereof
DE4315600C2 (de) * 1993-05-11 1996-07-25 Daimler Benz Aerospace Airbus Tragstruktur für eine aerodynamische Fläche
DE19528664C2 (de) * 1995-08-04 1997-07-31 Joachim Heyse Tragkörper aus einem Verbundwerkstoff
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5848765A (en) * 1996-06-20 1998-12-15 The Boeing Company Reduced amplitude corrugated web spar

Also Published As

Publication number Publication date
EP0967147B1 (de) 2003-09-24
JP2000006893A (ja) 2000-01-11
EP0967147A2 (de) 1999-12-29
US6237873B1 (en) 2001-05-29
DE69911507T2 (de) 2004-06-24
EP0967147A3 (de) 2002-04-24

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee