JP2010507530A5 - - Google Patents

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Publication number
JP2010507530A5
JP2010507530A5 JP2009534567A JP2009534567A JP2010507530A5 JP 2010507530 A5 JP2010507530 A5 JP 2010507530A5 JP 2009534567 A JP2009534567 A JP 2009534567A JP 2009534567 A JP2009534567 A JP 2009534567A JP 2010507530 A5 JP2010507530 A5 JP 2010507530A5
Authority
JP
Japan
Prior art keywords
inner layer
outer layer
wing panel
core structure
panel structure
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
JP2009534567A
Other languages
English (en)
Japanese (ja)
Other versions
JP5319538B2 (ja
JP2010507530A (ja
Filing date
Publication date
Priority claimed from US11/553,017 external-priority patent/US7628358B2/en
Application filed filed Critical
Publication of JP2010507530A publication Critical patent/JP2010507530A/ja
Publication of JP2010507530A5 publication Critical patent/JP2010507530A5/ja
Application granted granted Critical
Publication of JP5319538B2 publication Critical patent/JP5319538B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2009534567A 2006-10-26 2007-07-18 翼パネル構造 Active JP5319538B2 (ja)

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 (3)

Publication Number Publication Date
JP2010507530A JP2010507530A (ja) 2010-03-11
JP2010507530A5 true JP2010507530A5 (enExample) 2010-08-19
JP5319538B2 JP5319538B2 (ja) 2013-10-16

Family

ID=39328954

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009534567A Active JP5319538B2 (ja) 2006-10-26 2007-07-18 翼パネル構造

Country Status (8)

Country Link
US (1) US7628358B2 (enExample)
EP (1) EP2076431B1 (enExample)
JP (1) JP5319538B2 (enExample)
CN (1) CN101557979B (enExample)
CA (1) CA2659448C (enExample)
ES (1) ES2770642T3 (enExample)
PT (1) PT2076431T (enExample)
WO (1) WO2008105806A2 (enExample)

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

Family Cites Families (14)

* 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
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
DE3379945D1 (en) * 1983-09-29 1989-07-06 Boeing Co High strength to weight horizontal and vertical aircraft stabilizer
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
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

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