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WO2010070185A3 - Borde de salida de superficie estabilizadora de aeronave - Google Patents

Borde de salida de superficie estabilizadora de aeronave Download PDF

Info

Publication number
WO2010070185A3
WO2010070185A3 PCT/ES2009/070609 ES2009070609W WO2010070185A3 WO 2010070185 A3 WO2010070185 A3 WO 2010070185A3 ES 2009070609 W ES2009070609 W ES 2009070609W WO 2010070185 A3 WO2010070185 A3 WO 2010070185A3
Authority
WO
WIPO (PCT)
Prior art keywords
stabiliser
trailing edge
aircraft
clip
coupling element
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.)
Ceased
Application number
PCT/ES2009/070609
Other languages
English (en)
French (fr)
Other versions
WO2010070185A2 (es
Inventor
Alberto BALSA GONZÁLEZ
Francisco De Paula Burgos Gallego
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.)
Airbus Operations SL
Original Assignee
Airbus Operations SL
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 Airbus Operations SL filed Critical Airbus Operations SL
Priority to CN200980155875.6A priority Critical patent/CN102300770B/zh
Publication of WO2010070185A2 publication Critical patent/WO2010070185A2/es
Publication of WO2010070185A3 publication Critical patent/WO2010070185A3/es
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Clamps And Clips (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

Borde de salida (3) de superficie estabilizadora (1) de aeronave, estando dicha superficie (1) fabricada en material compuesto y comprendiendo un revestimiento exterior (40) y un revestimiento interior (41) que se unen a través de un elemento (20) de unión tipo clip en dicho borde de salida (3), caracterizado porque el elemento (20) de unión tipo clip comprende en sus extremos unos rebajes (23) destinados a acoplar con la zona interior de los revestimientos superior e inferior (40, 41 ) de la superficie estabilizadora (1), de tal forma que el elemento (20) de unión tipo clip es lo suficientemente flexible como para permitir su pinzado, de tal forma que sus extremos quedan alojados, por medio de los citados rebajes (23), entre los revestimientos exterior e interior (40, 41) de la superficie estabilizadora (1) de la aeronave, quedando así la zona exterior de la superficie estabilizadora (1), en su borde de salida (3) formada por una superficie continua aerodinámica sin cambios de pendiente.
PCT/ES2009/070609 2008-12-18 2009-12-18 Borde de salida de superficie estabilizadora de aeronave Ceased WO2010070185A2 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200980155875.6A CN102300770B (zh) 2008-12-18 2009-12-18 飞行器稳定装置表面后缘

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP200803603 2008-12-18
ES200803603A ES2367935B1 (es) 2008-12-18 2008-12-18 Borde de salida de superficie estabilizadora de aeronave.

Publications (2)

Publication Number Publication Date
WO2010070185A2 WO2010070185A2 (es) 2010-06-24
WO2010070185A3 true WO2010070185A3 (es) 2010-08-12

Family

ID=42173173

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070609 Ceased WO2010070185A2 (es) 2008-12-18 2009-12-18 Borde de salida de superficie estabilizadora de aeronave

Country Status (4)

Country Link
US (1) US8444091B2 (es)
CN (1) CN102300770B (es)
ES (1) ES2367935B1 (es)
WO (1) WO2010070185A2 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106567990A (zh) * 2015-10-10 2017-04-19 陕西飞机工业（集团）有限公司 一种泡沫填充结构及其加工方法

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2371401B1 (es) * 2008-06-27 2012-11-07 Airbus Operations, S.L. Estructura de superficie sustentadora de aeronave.
GB201004757D0 (en) * 2010-03-23 2010-05-05 Airbus Operations Ltd Joint
FR2973774B1 (fr) * 2011-04-06 2015-05-08 Airbus Operations Sas Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.
ES2421410B1 (es) * 2012-02-29 2014-10-28 Airbus Operations, S.L. Borde de salida de una superficie aerodinamica de una aeronave
US10173789B2 (en) * 2012-04-02 2019-01-08 Aerosud Technology Solutions (Pty) Ltd. Cellular core composite leading and trailing edges
US9352822B2 (en) * 2012-05-30 2016-05-31 The Boeing Company Bonded composite airfoil
ES2584557T3 (es) * 2012-08-16 2016-09-28 Airbus Operations S.L. Estructura interna altamente integrada de un cajón de torsión de una superficie sustentadora de una aeronave y método para su producción
US10329009B2 (en) * 2014-09-17 2019-06-25 The Boeing Company Composite wing edge attachment and method
ES2799935T3 (es) 2016-02-29 2020-12-22 Airbus Operations Sl Perfil aerodinámico de aeronave con un borde de salida unido por puntos y procedimiento de fabricación del mismo
CN107434031A (zh) 2016-05-25 2017-12-05 空中客车简化股份公司 飞行器翼体的结构部件和包括该结构部件的飞行器
US10532804B2 (en) 2017-02-08 2020-01-14 The Boeing Company Aerodynamic control surface and associated trailing edge close-out method
CN109606637A (zh) * 2018-11-02 2019-04-12 中国航空工业集团公司西安飞机设计研究所 一种通用飞机方向舵的复合材料夹芯壁板结构
EP3683139B1 (en) * 2019-01-18 2021-07-28 Airbus Operations, S.L.U. Flight control surface for an aircraft and method for manufacturing said flight control surface
CN112093029A (zh) * 2019-06-18 2020-12-18 成都飞机工业（集团）有限责任公司 一种飞机翼面后缘
EP3904203A1 (en) * 2020-04-29 2021-11-03 Airbus Operations, S.L. Trailing edge for a composite lifting surface
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
EP4155192B1 (en) 2021-09-28 2025-02-12 Airbus Operations, S.L.U. Profile for a trailing edge of an airfoil and method to repair thereof
FR3159590A1 (fr) * 2024-02-27 2025-08-29 Airbus Operations Profil aérodynamique comprenant au moins un bord de fuite emboîté, aéronef comportant au moins un tel profil aérodynamique

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214092B (de) * 1963-06-08 1966-04-07 Monte Copter Inc Flugzeugtragfluegel, insbesondere Drehfluegel, der in Tiefenrichtung aus zwei oder mehr Teilen zusammensetzbar ist
US20040000613A1 (en) * 2002-06-28 2004-01-01 Thomas William A. Preforms for acute structural edges

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2193951A (en) * 1937-05-28 1940-03-19 John H Van Uum Spring clip device
US2613893A (en) * 1948-04-01 1952-10-14 Curtiss Wright Corp Airfoil construction
CN100455793C (zh) * 2003-03-31 2009-01-28 丹麦技术大学 风轮机叶片、风轮机以及控制风轮机工作条件的方法

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214092B (de) * 1963-06-08 1966-04-07 Monte Copter Inc Flugzeugtragfluegel, insbesondere Drehfluegel, der in Tiefenrichtung aus zwei oder mehr Teilen zusammensetzbar ist
US20040000613A1 (en) * 2002-06-28 2004-01-01 Thomas William A. Preforms for acute structural edges

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106567990A (zh) * 2015-10-10 2017-04-19 陕西飞机工业（集团）有限公司 一种泡沫填充结构及其加工方法

Also Published As

Publication number Publication date
US20100155528A1 (en) 2010-06-24
US8444091B2 (en) 2013-05-21
CN102300770A (zh) 2011-12-28
WO2010070185A2 (es) 2010-06-24
ES2367935A1 (es) 2011-11-11
ES2367935B1 (es) 2012-09-18
CN102300770B (zh) 2015-03-04

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