JP6370790B2 - 航空機群用主翼付根挿入システム - Google Patents

航空機群用主翼付根挿入システム Download PDF

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Publication number
JP6370790B2
JP6370790B2 JP2015534505A JP2015534505A JP6370790B2 JP 6370790 B2 JP6370790 B2 JP 6370790B2 JP 2015534505 A JP2015534505 A JP 2015534505A JP 2015534505 A JP2015534505 A JP 2015534505A JP 6370790 B2 JP6370790 B2 JP 6370790B2
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Japan
Prior art keywords
fuselage
wing
configuration
main wing
main
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Expired - Fee Related
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JP2015534505A
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English (en)
Japanese (ja)
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JP2015533716A5 (enExample
JP2015533716A (ja
Inventor
ペリー・ニコラス・レア
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Boeing Co
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Boeing Co
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Publication date
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Publication of JP2015533716A publication Critical patent/JP2015533716A/ja
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Expired - Fee Related legal-status Critical Current
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2015534505A 2012-09-27 2013-08-28 航空機群用主翼付根挿入システム Expired - Fee Related JP6370790B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/628,117 2012-09-27
US13/628,117 US10118686B2 (en) 2012-09-27 2012-09-27 Wing root insert system for an aircraft family
PCT/US2013/057168 WO2014051923A1 (en) 2012-09-27 2013-08-28 Wing root insert system for an aircraft family

Publications (3)

Publication Number Publication Date
JP2015533716A JP2015533716A (ja) 2015-11-26
JP2015533716A5 JP2015533716A5 (enExample) 2016-10-20
JP6370790B2 true JP6370790B2 (ja) 2018-08-08

Family

ID=49223846

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015534505A Expired - Fee Related JP6370790B2 (ja) 2012-09-27 2013-08-28 航空機群用主翼付根挿入システム

Country Status (5)

Country Link
US (1) US10118686B2 (enExample)
EP (1) EP2872396B1 (enExample)
JP (1) JP6370790B2 (enExample)
CN (1) CN104540730B (enExample)
WO (1) WO2014051923A1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA3061691A1 (en) 2017-05-01 2018-11-08 Bombardier Inc. Aircraft wing unit with upper wing skin defining pressure floor
WO2018203189A1 (en) 2017-05-01 2018-11-08 Bombardier Inc. Aircraft wing unit with pressure fence
FR3091259A1 (fr) * 2018-12-26 2020-07-03 Airbus Operations Voilure d’aeronef comprenant deux ailes fixees l’une sur l’autre

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US7837148B2 (en) 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
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DE102007019692B4 (de) 2007-04-26 2011-06-01 Airbus Operations Gmbh Flügel-Rumpf-Sektion eines Flugzeugs
FR2916417B1 (fr) 2007-05-23 2009-07-24 Airbus France Sas Element structural d'aeronef situe a l'interface entre une aile et le fuselage
FR2920407B1 (fr) 2007-08-29 2010-05-07 Michel Kieffer Technologie de construction des ailes d'un aeronef
US7887009B2 (en) * 2007-12-05 2011-02-15 The Boeing Company Methods and systems for attaching aircraft wings to fuselages
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FR2936489B1 (fr) * 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
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FR2948099B1 (fr) * 2009-07-16 2012-05-11 Airbus Operations Sas Procede de fabrication d'un aeronef a voilure fixe
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DE102011013828A1 (de) * 2011-03-14 2012-09-20 Airbus Operations Gmbh Verkleidungsübergang und Fahrzeug mit einem bewegbaren und einem feststehenden Körper mit einem Verkleidungsübergang
FR2972997B1 (fr) * 2011-03-25 2013-05-10 Airbus Operations Sas Raccordement d'un fuselage a une voilure d'aeronef
US9475585B2 (en) * 2014-06-25 2016-10-25 The Boeing Company Tilt-rotor vertical-lift aircraft

Also Published As

Publication number Publication date
EP2872396A1 (en) 2015-05-20
CN104540730A (zh) 2015-04-22
CN104540730B (zh) 2017-05-10
JP2015533716A (ja) 2015-11-26
EP2872396B1 (en) 2018-12-19
WO2014051923A1 (en) 2014-04-03
US10118686B2 (en) 2018-11-06
US20140084110A1 (en) 2014-03-27

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