CN104540730B - 用于航空器家族的翼根插入系统 - Google Patents

用于航空器家族的翼根插入系统 Download PDF

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Publication number
CN104540730B
CN104540730B CN201380041431.6A CN201380041431A CN104540730B CN 104540730 B CN104540730 B CN 104540730B CN 201380041431 A CN201380041431 A CN 201380041431A CN 104540730 B CN104540730 B CN 104540730B
Authority
CN
China
Prior art keywords
wing
fuselage
construction
pair
central sections
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
CN201380041431.6A
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English (en)
Chinese (zh)
Other versions
CN104540730A (zh
Inventor
P·N·瑞阿
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
Original Assignee
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 CN104540730A publication Critical patent/CN104540730A/zh
Application granted granted Critical
Publication of CN104540730B publication Critical patent/CN104540730B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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)
CN201380041431.6A 2012-09-27 2013-08-28 用于航空器家族的翼根插入系统 Expired - Fee Related CN104540730B (zh)

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 (2)

Publication Number Publication Date
CN104540730A CN104540730A (zh) 2015-04-22
CN104540730B true CN104540730B (zh) 2017-05-10

Family

ID=49223846

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380041431.6A Expired - Fee Related CN104540730B (zh) 2012-09-27 2013-08-28 用于航空器家族的翼根插入系统

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

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6726149B2 (en) * 2002-05-31 2004-04-27 The Boeing Company Derivative aircraft and methods for their manufacture

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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
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Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6726149B2 (en) * 2002-05-31 2004-04-27 The Boeing Company Derivative aircraft and methods for their manufacture

Also Published As

Publication number Publication date
EP2872396A1 (en) 2015-05-20
CN104540730A (zh) 2015-04-22
JP2015533716A (ja) 2015-11-26
EP2872396B1 (en) 2018-12-19
JP6370790B2 (ja) 2018-08-08
WO2014051923A1 (en) 2014-04-03
US10118686B2 (en) 2018-11-06
US20140084110A1 (en) 2014-03-27

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