WO2010063868A3 - Superficie estabilizadora y de control direccional de aeronave. - Google Patents

Superficie estabilizadora y de control direccional de aeronave. Download PDF

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Publication number
WO2010063868A3
WO2010063868A3 PCT/ES2009/070557 ES2009070557W WO2010063868A3 WO 2010063868 A3 WO2010063868 A3 WO 2010063868A3 ES 2009070557 W ES2009070557 W ES 2009070557W WO 2010063868 A3 WO2010063868 A3 WO 2010063868A3
Authority
WO
WIPO (PCT)
Prior art keywords
rudder
aircraft
vertical stabilizer
internal profile
stabilizing
Prior art date
Application number
PCT/ES2009/070557
Other languages
English (en)
French (fr)
Other versions
WO2010063868A2 (es
Inventor
Jorge Pablo Verde Preckler
José Miguel VIZARRO TORIBIO
Original Assignee
Airbus Operations, S.L.
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, S.L. filed Critical Airbus Operations, S.L.
Priority to ES09804138.7T priority Critical patent/ES2501365T3/es
Priority to CN200980149224.6A priority patent/CN102239083B/zh
Priority to EP09804138.7A priority patent/EP2371707B1/en
Publication of WO2010063868A2 publication Critical patent/WO2010063868A2/es
Publication of WO2010063868A3 publication Critical patent/WO2010063868A3/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/18—Stabilising surfaces adjustable in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/08—Adjustable control surfaces or members, e.g. rudders bodily displaceable
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Transmission Devices (AREA)
  • Traffic Control Systems (AREA)

Abstract

Superficie estabilizadora y de control direccional de una aeronave, comprendiendo dicha superficie un estabilizador vertical (2) y un timón de dirección (3), siendo el citado timón de dirección (3) deflectable con respecto al estabilizador vertical (2), comprendiendo además el timón de dirección (3) un perfil interior (10) que es extraíble y retráctil a través de un sistema de actuación (40) con respecto al resto de la estructura del timón de dirección (3), tal que la superficie estabilizadora y de control, en la posición de retracción del perfil interior (10) del timón de dirección (3), es una superficie aerodinámica óptima en condiciones de vuelo normales, al tiempo que se consigue el aumento de la superficie aerodinámica de control del estabilizador vertical (2) por requerimientos de controlabilidad de la aeronave a bajas velocidades de la citada aeronave y ante fuertes momentos de guiñada originados sobre la misma, en la posición en la que el perfil interior (10) del timón de dirección (3) está extraído, pudiendo además la estructura del timón de dirección (3) abrirse, tal que permita la extracción del perfil interior (10), cerrándose dicha estructura una vez que se ha extraído por completo el perfil interior (10), tal que el timón de dirección (3) forme con el perfil interior (10) extendido una estructura que conserve sus propiedades de superficie aerodinámica y continuidad de flujo.
PCT/ES2009/070557 2008-12-04 2009-12-04 Superficie estabilizadora y de control direccional de aeronave. WO2010063868A2 (es)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES09804138.7T ES2501365T3 (es) 2008-12-04 2009-12-04 Superficie estabilizadora y de control direccional de aeronave
CN200980149224.6A CN102239083B (zh) 2008-12-04 2009-12-04 飞机方向控制和稳定化表面
EP09804138.7A EP2371707B1 (en) 2008-12-04 2009-12-04 Aircraft directional control and stabilizing surface

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP200803447 2008-12-04
ES200803447A ES2382062B1 (es) 2008-12-04 2008-12-04 Superficie estabilizadora y de control direccional de aeronave

Publications (2)

Publication Number Publication Date
WO2010063868A2 WO2010063868A2 (es) 2010-06-10
WO2010063868A3 true WO2010063868A3 (es) 2010-07-29

Family

ID=41163181

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070557 WO2010063868A2 (es) 2008-12-04 2009-12-04 Superficie estabilizadora y de control direccional de aeronave.

Country Status (5)

Country Link
US (1) US8152097B2 (es)
EP (1) EP2371707B1 (es)
CN (1) CN102239083B (es)
ES (2) ES2382062B1 (es)
WO (1) WO2010063868A2 (es)

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FR2973774B1 (fr) * 2011-04-06 2015-05-08 Airbus Operations Sas Procede d'amelioration de l'efficacite aerodynamique d'un empennage vertical d'aeronef.
EP2736804B1 (en) 2011-07-26 2015-09-02 Learjet Inc. Rudder bias gain changer
CN103569346B (zh) * 2013-11-13 2016-04-20 中国航空工业集团公司西安飞机设计研究所 一种舰载运输类飞机的垂尾结构
US9643716B2 (en) * 2014-04-01 2017-05-09 The Boeing Company Air vehicle, actuator assembly and associated method of manufacture
FR3026386B1 (fr) 2014-09-30 2016-10-21 Airbus Helicopters Giravion muni d'un dispositif stabilisateur
CN105574257B (zh) * 2015-12-12 2019-02-12 中国航空工业集团公司西安飞机设计研究所 一种飞机双铰链方向舵效率计算方法
CN105523169B (zh) * 2015-12-28 2017-11-03 哈尔滨工业大学 一种可变弯的机翼舵面
CN105836106B (zh) * 2016-05-23 2018-03-13 南京航空航天大学 基于形状记忆合金驱动的变体机翼后缘及其偏转方法
CN107499499B (zh) * 2017-07-20 2021-01-08 中国航空工业集团公司西安飞机设计研究所 一种带机械回中功能的飞机作动系统
CN108033012A (zh) * 2017-12-13 2018-05-15 四川宝天智控系统有限公司 Vtol固定翼无人机及其固定翼结构
CN108082449B (zh) * 2018-03-06 2022-06-10 中航通飞华南飞机工业有限公司 一种大型飞机舵面悬挂结构
CN108674633A (zh) * 2018-07-25 2018-10-19 北京因时机器人科技有限公司 舵面控制机构和航模
CN109018303B (zh) * 2018-08-14 2020-05-19 晨龙飞机（荆门）有限公司 一种可快速上仰和下俯的飞机平尾翼
CN109592011A (zh) * 2018-11-02 2019-04-09 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复合材料壁板结构
CN109592014A (zh) * 2018-11-02 2019-04-09 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转轴结构及操纵方法
CN109484671B (zh) * 2018-11-27 2020-06-05 北京空间技术研制试验中心 飞行器舵面恒定铰链力矩加载机构及加载方法
EP3816041A1 (en) * 2019-10-29 2021-05-05 Airbus Operations, S.L.U. Control surface for an aircraft and control structure for an aircraft with anti-flutter balance weight
CN112498661B (zh) * 2020-12-04 2024-01-30 中国航空工业集团公司沈阳飞机设计研究所 一种多功能舵面结构
CN112407245A (zh) * 2020-12-14 2021-02-26 中国科学院工程热物理研究所 一种飞行器
CN113772079A (zh) * 2021-09-30 2021-12-10 南方科技大学 鸭翼尾座式无人机
RU2764335C1 (ru) * 2021-10-15 2022-01-17 Общество с ограниченной ответственностью «Научно Инженерная Компания» Устройство управления закрылками крыла самолёта
CN114348239A (zh) * 2022-01-24 2022-04-15 北京航空航天大学 一种形状记忆合金驱动的可连续自动偏转舵面肋架结构
CN115783241B (zh) * 2023-02-08 2023-05-16 中国空气动力研究与发展中心计算空气动力研究所 融合体飞行器的异步偏转航向控制组合舵控制方法

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US3162401A (en) * 1960-12-12 1964-12-22 Hawker Siddeley Aviation Ltd Aircraft and lift devices therefor
JPS5459798A (en) * 1977-10-20 1979-05-14 Mitsubishi Heavy Ind Ltd Aircraft that direction of empennage can be varied
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FR2911113A1 (fr) * 2007-01-04 2008-07-11 Airbus France Sa Empennage horizontal pour aeronef.

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Publication number Priority date Publication date Assignee Title
US2292613A (en) * 1940-12-30 1942-08-11 Chapman Frederick Burnham Retractible airplane wing
US3162401A (en) * 1960-12-12 1964-12-22 Hawker Siddeley Aviation Ltd Aircraft and lift devices therefor
JPS5459798A (en) * 1977-10-20 1979-05-14 Mitsubishi Heavy Ind Ltd Aircraft that direction of empennage can be varied
US6834835B1 (en) * 2004-03-12 2004-12-28 Qortek, Inc. Telescopic wing system
FR2911113A1 (fr) * 2007-01-04 2008-07-11 Airbus France Sa Empennage horizontal pour aeronef.

Also Published As

Publication number Publication date
CN102239083A (zh) 2011-11-09
ES2501365T3 (es) 2014-10-01
US8152097B2 (en) 2012-04-10
ES2382062B1 (es) 2013-04-26
ES2382062A1 (es) 2012-06-05
EP2371707A2 (en) 2011-10-05
CN102239083B (zh) 2014-01-29
WO2010063868A2 (es) 2010-06-10
EP2371707B1 (en) 2014-04-30
US20090256025A1 (en) 2009-10-15

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