CN101557979B - 机翼面板结构 - Google Patents

机翼面板结构 Download PDF

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Publication number
CN101557979B
CN101557979B CN2007800364237A CN200780036423A CN101557979B CN 101557979 B CN101557979 B CN 101557979B CN 2007800364237 A CN2007800364237 A CN 2007800364237A CN 200780036423 A CN200780036423 A CN 200780036423A CN 101557979 B CN101557979 B CN 101557979B
Authority
CN
China
Prior art keywords
inner layer
wing
wing panel
layer material
reinforcement
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.)
Active
Application number
CN2007800364237A
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English (en)
Chinese (zh)
Other versions
CN101557979A (zh
Inventor
詹姆斯·F·阿克曼
理查德·B·坦纳
伊恩·C·伯福德
托马斯·V·金兹威尔
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.)
Boeing Co
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Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of CN101557979A publication Critical patent/CN101557979A/zh
Application granted granted Critical
Publication of CN101557979B publication Critical patent/CN101557979B/zh
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
CN2007800364237A 2006-10-26 2007-07-18 机翼面板结构 Active CN101557979B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/553,017 US7628358B2 (en) 2006-10-26 2006-10-26 Wing panel structure
US11/553,017 2006-10-26
PCT/US2007/016377 WO2008105806A2 (en) 2006-10-26 2007-07-18 Wing panel structure

Publications (2)

Publication Number Publication Date
CN101557979A CN101557979A (zh) 2009-10-14
CN101557979B true CN101557979B (zh) 2012-06-13

Family

ID=39328954

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2007800364237A Active CN101557979B (zh) 2006-10-26 2007-07-18 机翼面板结构

Country Status (8)

Country Link
US (1) US7628358B2 (cg-RX-API-DMAC7.html)
EP (1) EP2076431B1 (cg-RX-API-DMAC7.html)
JP (1) JP5319538B2 (cg-RX-API-DMAC7.html)
CN (1) CN101557979B (cg-RX-API-DMAC7.html)
CA (1) CA2659448C (cg-RX-API-DMAC7.html)
ES (1) ES2770642T3 (cg-RX-API-DMAC7.html)
PT (1) PT2076431T (cg-RX-API-DMAC7.html)
WO (1) WO2008105806A2 (cg-RX-API-DMAC7.html)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080277531A1 (en) 2007-05-11 2008-11-13 The Boeing Company Hybrid Composite Panel Systems and Methods
IT1392320B1 (it) * 2008-12-09 2012-02-24 Alenia Aeronautica Spa Bordo d'attacco per ali ed impennaggi di aeromobili
DE102009013585B4 (de) 2009-03-17 2012-01-26 Airbus Operations Gmbh Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise
US8167245B1 (en) * 2009-11-03 2012-05-01 The Boeing Company Fuel barrier
JP5535957B2 (ja) 2011-02-21 2014-07-02 三菱航空機株式会社 翼パネルの形成方法
US9943937B2 (en) 2012-09-28 2018-04-17 The Boeing Company System and method for manufacturing a wing panel
EP2989003A4 (en) * 2013-04-25 2016-12-07 Saab Ab EXPIRATION OF A STAMPING ELEMENT
US10801836B2 (en) 2017-06-13 2020-10-13 The Boeing Company Composite parts that facilitate ultrasonic imaging of layer boundaries

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
US4667905A (en) * 1983-09-29 1987-05-26 The Boeing Company High strength to weight horizontal and vertical aircraft stabilizer
US5735486A (en) * 1995-08-11 1998-04-07 Deutsche Forschungsanstalt Fur Luft-Und Raumfahrt E.V. Aircraft wing
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US6689246B2 (en) * 1998-07-30 2004-02-10 Japan Aircraft Development Corporation Method of making composite airfoil structures

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2382358A (en) * 1944-02-03 1945-08-14 Budd Edward G Mfg Co Stressed skin airfoil joint
US3058704A (en) * 1958-01-16 1962-10-16 Johnson & Johnson Laminated adhesive sheeting for aircraft
US4344995A (en) * 1980-09-15 1982-08-17 The Boeing Company Hybrid composite structures
US4599255A (en) * 1981-12-28 1986-07-08 The Boeing Company Composite structures having conductive surfaces
DE19845863B4 (de) 1998-10-05 2005-05-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strukturelement mit großen unidirektionalen Steifigkeiten
US6976829B2 (en) 2003-07-16 2005-12-20 Sikorsky Aircraft Corporation Rotor blade tip section
US7115323B2 (en) * 2003-08-28 2006-10-03 The Boeing Company Titanium foil ply replacement in layup of composite skin
US7052573B2 (en) * 2003-11-21 2006-05-30 The Boeing Company Method to eliminate undulations in a composite panel
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
US4667905A (en) * 1983-09-29 1987-05-26 The Boeing Company High strength to weight horizontal and vertical aircraft stabilizer
US5735486A (en) * 1995-08-11 1998-04-07 Deutsche Forschungsanstalt Fur Luft-Und Raumfahrt E.V. Aircraft wing
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US6689246B2 (en) * 1998-07-30 2004-02-10 Japan Aircraft Development Corporation Method of making composite airfoil structures

Also Published As

Publication number Publication date
US20080099613A1 (en) 2008-05-01
CA2659448A1 (en) 2008-09-04
WO2008105806A3 (en) 2009-06-11
CA2659448C (en) 2012-06-19
CN101557979A (zh) 2009-10-14
JP2010507530A (ja) 2010-03-11
ES2770642T3 (es) 2020-07-02
PT2076431T (pt) 2020-01-09
WO2008105806A2 (en) 2008-09-04
EP2076431A2 (en) 2009-07-08
JP5319538B2 (ja) 2013-10-16
EP2076431B1 (en) 2019-12-04
US7628358B2 (en) 2009-12-08

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