JP6644481B2 - 航空機翼の複合固定縁及びその取り付け方法 - Google Patents

航空機翼の複合固定縁及びその取り付け方法 Download PDF

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Publication number
JP6644481B2
JP6644481B2 JP2015118307A JP2015118307A JP6644481B2 JP 6644481 B2 JP6644481 B2 JP 6644481B2 JP 2015118307 A JP2015118307 A JP 2015118307A JP 2015118307 A JP2015118307 A JP 2015118307A JP 6644481 B2 JP6644481 B2 JP 6644481B2
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Japan
Prior art keywords
composite
wing
skin panel
shoulder
edge
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JP2015118307A
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Japanese (ja)
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JP2016175631A5 (enExample
JP2016175631A (ja
Inventor
クリス・ジェー・フォスター
グレゴリー・エム・サンティーニ
ジョン・ヴィー・ダヴィ
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Boeing Co
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Boeing Co
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
JP2015118307A 2014-09-17 2015-06-11 航空機翼の複合固定縁及びその取り付け方法 Active JP6644481B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/488,987 2014-09-17
US14/488,987 US10329009B2 (en) 2014-09-17 2014-09-17 Composite wing edge attachment and method

Publications (3)

Publication Number Publication Date
JP2016175631A JP2016175631A (ja) 2016-10-06
JP2016175631A5 JP2016175631A5 (enExample) 2018-07-26
JP6644481B2 true JP6644481B2 (ja) 2020-02-12

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JP2015118307A Active JP6644481B2 (ja) 2014-09-17 2015-06-11 航空機翼の複合固定縁及びその取り付け方法

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US (2) US10329009B2 (enExample)
EP (1) EP3000719B1 (enExample)
JP (1) JP6644481B2 (enExample)
CN (1) CN105438438B (enExample)

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US20170259521A1 (en) * 2016-02-08 2017-09-14 Bell Helicopter Textron Inc. Large Cell Core Stiffened Panels with Solid Inserts
EP3243743B1 (en) * 2016-05-11 2021-05-05 Airbus Operations Limited Aircraft joint
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US10179640B2 (en) * 2016-08-24 2019-01-15 The Boeing Company Wing and method of manufacturing
ES2764122T3 (es) * 2016-12-02 2020-06-02 Airbus Operations Sl Integración del borde de ataque de un estabilizador de aeronave con el cajón de torsión y el fuselaje
NL2018263B1 (nl) * 2017-01-31 2018-08-16 Fibercore Ip Bv Aerodynamisch of hydrodynamisch blad uit gelaagd materiaal
EP3421352B1 (en) * 2017-06-28 2022-10-26 Airbus Operations S.L. Modular lifting surface and method for manufacturing thereof
GB201710385D0 (en) * 2017-06-29 2017-08-16 Airbus Operations Gmbh Aerofoil structure and method of assembly
US10773789B2 (en) * 2017-07-07 2020-09-15 The Boeing Company Skin-panel interface of an aircraft
US10828851B2 (en) * 2017-07-28 2020-11-10 The Boeing Company Slip sheet with compensation surface
CN108032988B (zh) * 2017-10-25 2020-06-16 北京航空航天大学 一种纤维增强复合材料飞行器舱段连接结构及其制备方法
CN108100218B (zh) * 2017-11-16 2021-04-16 中国航空工业集团公司西安飞机设计研究所 一种带翼型的可拆卸雷达罩支撑结构
GB201719790D0 (en) 2017-11-28 2018-01-10 Airbus Operations Gmbh Aircraft joint with a curable composite bushing
EP3521162B1 (en) 2018-02-02 2022-06-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A helicopter with a fuselage and a tail boom which are connected via a shear connection
US11047308B2 (en) * 2018-06-29 2021-06-29 The Boeing Company Acoustic panel for thrust reversers
GB2577936A (en) * 2018-10-12 2020-04-15 Airbus Operations Ltd Aircraft assembly
CN109649675B (zh) * 2018-11-30 2021-10-29 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种机翼下壁板对接区的密封优化方法
CN109572996B (zh) * 2018-12-04 2022-04-19 中国航空工业集团公司西安飞机设计研究所 一种考虑温度变化的尾翼抗鸟撞附加蒙皮前缘结构
CN109815528A (zh) * 2018-12-13 2019-05-28 航天神舟飞行器有限公司 一种基于大型复合翼气的飞行器参数优化的方法
CN110065620A (zh) * 2019-04-12 2019-07-30 西安飞机工业（集团）有限责任公司 一种复合材料壁板连接结构
CN110145678B (zh) * 2019-05-13 2022-06-17 湖北三江航天红阳机电有限公司 一种大尺寸复杂蜂窝夹层结构复合壳片以及整体成型方法
US11383820B2 (en) * 2019-06-11 2022-07-12 The Boeing Company Aerodynamic surface lap splice
US11352124B2 (en) * 2019-11-01 2022-06-07 The Boeing Company Continuous skin leading edge slats
US11401026B2 (en) 2020-05-21 2022-08-02 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11572152B2 (en) 2020-05-21 2023-02-07 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11554848B2 (en) * 2020-05-21 2023-01-17 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11453476B2 (en) 2020-05-21 2022-09-27 The Boeing Company Structural composite airfoils with an improved leading edge, and related methods
CN114771802A (zh) 2021-01-22 2022-07-22 波音公司 空气动力学结构以及形成空气动力学结构的方法
GB2611298A (en) * 2021-09-27 2023-04-05 Airbus Operations Ltd A kit of parts for forming an aerofoil assembly
EP4186783B1 (en) * 2021-11-24 2025-01-08 Airbus Operations, S.L.U. Manufacturing method of a control surface of an aircraft
FR3136506B1 (fr) * 2022-06-10 2025-05-02 Safran Nacelles Procédé de réalisation d’un assemblage de pièces pour un ensemble propulsif d’aéronef
CN115871956B (zh) * 2022-11-27 2025-12-02 中国特种飞行器研究所 一种基于等效腔体的漂浮特性试验模型

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FR2936495B1 (fr) * 2008-09-30 2011-06-03 Airbus France Assemblage de panneaux pour fuselage d'aeronef.
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GB0901640D0 (en) * 2009-02-03 2009-03-11 Airbus Uk Ltd Joint
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Also Published As

Publication number Publication date
CN105438438A (zh) 2016-03-30
EP3000719A1 (en) 2016-03-30
US10933972B2 (en) 2021-03-02
US20160244143A1 (en) 2016-08-25
EP3000719B1 (en) 2020-08-19
CN105438438B (zh) 2019-12-27
US20190071165A1 (en) 2019-03-07
JP2016175631A (ja) 2016-10-06
US10329009B2 (en) 2019-06-25

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