CN103097240B - 一种用于增加由具有多个开口的蒙皮板承载的负荷的机翼结构及用于进入飞机机翼结构内部的方法 - Google Patents

一种用于增加由具有多个开口的蒙皮板承载的负荷的机翼结构及用于进入飞机机翼结构内部的方法 Download PDF

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Publication number
CN103097240B
CN103097240B CN201180039950.XA CN201180039950A CN103097240B CN 103097240 B CN103097240 B CN 103097240B CN 201180039950 A CN201180039950 A CN 201180039950A CN 103097240 B CN103097240 B CN 103097240B
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China
Prior art keywords
openings
wing
frame
aircraft
airfoil
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CN201180039950.XA
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Chinese (zh)
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CN103097240A (zh
Inventor
J·H·卡姆帕纳
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Boeing Co
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Boeing Co
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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
    • 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
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Automatic Assembly (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
CN201180039950.XA 2010-08-17 2011-07-21 一种用于增加由具有多个开口的蒙皮板承载的负荷的机翼结构及用于进入飞机机翼结构内部的方法 Active CN103097240B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/857,750 US8348196B2 (en) 2010-08-17 2010-08-17 Multi-spar port box joint
US12/857,750 2010-08-17
PCT/US2011/044766 WO2012024051A1 (en) 2010-08-17 2011-07-21 Multi-spar port box joint

Publications (2)

Publication Number Publication Date
CN103097240A CN103097240A (zh) 2013-05-08
CN103097240B true CN103097240B (zh) 2015-08-12

Family

ID=44629784

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201180039950.XA Active CN103097240B (zh) 2010-08-17 2011-07-21 一种用于增加由具有多个开口的蒙皮板承载的负荷的机翼结构及用于进入飞机机翼结构内部的方法

Country Status (6)

Country Link
US (2) US8348196B2 (enExample)
EP (1) EP2605959B1 (enExample)
JP (1) JP5823519B2 (enExample)
CN (1) CN103097240B (enExample)
ES (1) ES2574308T3 (enExample)
WO (1) WO2012024051A1 (enExample)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
ES2372849B1 (es) * 2010-03-25 2012-12-13 Airbus Operations, S.L. Estructura de unión de cajones de torsión en una aeronave mediante un herraje triforme de materiales compuestos no metálicos.
US8348196B2 (en) 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
US9266625B1 (en) * 2012-06-27 2016-02-23 The Boeing Company System and method for scanning a wing box skin
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
CN105539812A (zh) * 2014-10-28 2016-05-04 中国航空工业集团公司西安飞机设计研究所 一种机翼翼梁对接接头
US9828083B2 (en) * 2014-11-14 2017-11-28 The Boeing Company Methods and components for wing-to-fuselage integration
EP3095691A1 (en) * 2015-05-22 2016-11-23 Airbus Operations, S.L. Multi-spar torsion box structure
US9994298B2 (en) 2015-06-30 2018-06-12 Lockheed Martin Corporation System for embedded removable aperture
CN106314759A (zh) * 2016-09-06 2017-01-11 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞机机翼的翼梁连接结构
CA3062404A1 (en) * 2017-05-01 2018-11-08 Bombardier Inc. Aircraft wing-to-fuselage interface permitting positional adjustment
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10766598B2 (en) * 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
ES2912379T3 (es) * 2018-08-01 2022-05-25 Airbus Operations Slu Anclaje para unir el estabilizador de cola horizontal de una aeronave
US11352063B2 (en) * 2018-08-30 2022-06-07 Clark Equipment Company Frame access aperture
FR3091259A1 (fr) * 2018-12-26 2020-07-03 Airbus Operations Voilure d’aeronef comprenant deux ailes fixees l’une sur l’autre
US11511846B2 (en) 2020-05-27 2022-11-29 The Boeing Company Aircraft with multi spar box connection to fuselage
US11370523B2 (en) 2020-05-27 2022-06-28 The Boeing Company Aircraft with multi spar box connection to fuselage
US12404003B2 (en) 2020-08-12 2025-09-02 The Boeing Company CFRP fuselage frame with securement to vertical tail fin
US11932398B2 (en) 2020-08-24 2024-03-19 The Boeing Company Horizontal stabilizer assembly for an aircraft
US12252245B2 (en) * 2021-01-20 2025-03-18 The Boeing Company Beaded composite structures and methods for manufacturing beaded composite structures
EP4197918B1 (fr) * 2021-12-16 2024-08-21 Airbus Operations (S.A.S.) Pièce de coin flexible destinée à contribuer à une liaison entre au moins trois parois d' au moins un caisson d' aéronef
US12291330B2 (en) * 2023-08-10 2025-05-06 The Boeing Company Aircraft wing having a truss system for coupling a center wing section to an outboard wing section

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741943A (en) * 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US20020195524A1 (en) * 1999-07-19 2002-12-26 Fuji Jukogyo Kabushiki Kaisha Method of fabricating a wing of composite material
US20080128553A1 (en) * 2006-11-30 2008-06-05 The Boeing Company Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures
US20090206203A1 (en) * 2006-07-28 2009-08-20 Tristan Crawford Aircraft wing box and manufacture thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3417946A (en) 1967-12-29 1968-12-24 Lockheed Aircraft Corp T-tail construction for aircraft
ES2335837B1 (es) * 2007-06-29 2011-02-18 Airbus España, Sl. Cubierta para boca de acceso de aeronave.
US8348196B2 (en) 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741943A (en) * 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US20020195524A1 (en) * 1999-07-19 2002-12-26 Fuji Jukogyo Kabushiki Kaisha Method of fabricating a wing of composite material
US20090206203A1 (en) * 2006-07-28 2009-08-20 Tristan Crawford Aircraft wing box and manufacture thereof
US20080128553A1 (en) * 2006-11-30 2008-06-05 The Boeing Company Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures

Also Published As

Publication number Publication date
WO2012024051A1 (en) 2012-02-23
CN103097240A (zh) 2013-05-08
ES2574308T3 (es) 2016-06-16
US20120043422A1 (en) 2012-02-23
EP2605959A1 (en) 2013-06-26
US8348196B2 (en) 2013-01-08
EP2605959B1 (en) 2016-04-20
US20130105629A1 (en) 2013-05-02
US8517312B2 (en) 2013-08-27
JP2013534194A (ja) 2013-09-02
JP5823519B2 (ja) 2015-11-25

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