ATE523424T1 - Flugzeug mit einem trimmbaren höhenleitwerk - Google Patents

Flugzeug mit einem trimmbaren höhenleitwerk

Info

Publication number
ATE523424T1
ATE523424T1 AT07787319T AT07787319T ATE523424T1 AT E523424 T1 ATE523424 T1 AT E523424T1 AT 07787319 T AT07787319 T AT 07787319T AT 07787319 T AT07787319 T AT 07787319T AT E523424 T1 ATE523424 T1 AT E523424T1
Authority
AT
Austria
Prior art keywords
aircraft
elevator
horizontal stabilizer
trimable
fuselage
Prior art date
Application number
AT07787319T
Other languages
English (en)
Inventor
Manfred Koneczny
Original Assignee
Airbus Operations Gmbh
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 Gmbh filed Critical Airbus Operations Gmbh
Application granted granted Critical
Publication of ATE523424T1 publication Critical patent/ATE523424T1/de

Links

Classifications

    • 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
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Vehicle Body Suspensions (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Cage And Drive Apparatuses For Elevators (AREA)
AT07787319T 2006-07-11 2007-07-10 Flugzeug mit einem trimmbaren höhenleitwerk ATE523424T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006032003.4A DE102006032003B4 (de) 2006-07-11 2006-07-11 Trimmbares Höhenleitwerk
PCT/EP2007/057044 WO2008006831A1 (en) 2006-07-11 2007-07-10 Trimmable horizontal stabilizer

Publications (1)

Publication Number Publication Date
ATE523424T1 true ATE523424T1 (de) 2011-09-15

Family

ID=38476155

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07787319T ATE523424T1 (de) 2006-07-11 2007-07-10 Flugzeug mit einem trimmbaren höhenleitwerk

Country Status (10)

Country Link
US (1) US7963485B2 (de)
EP (1) EP2038171B1 (de)
JP (1) JP5257996B2 (de)
CN (1) CN101495367B (de)
AT (1) ATE523424T1 (de)
BR (1) BRPI0712881A2 (de)
CA (1) CA2656794A1 (de)
DE (1) DE102006032003B4 (de)
RU (1) RU2448019C2 (de)
WO (1) WO2008006831A1 (de)

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US8042772B2 (en) 2008-03-05 2011-10-25 The Boeing Company System and method for pneumatically actuating a control surface of an airfoil
US9127908B2 (en) 2009-02-02 2015-09-08 Aero Vironment, Inc. Multimode unmanned aerial vehicle
JP5865247B2 (ja) 2009-09-09 2016-02-17 エアロバイロメント, インコーポレイテッドAerovironment, Inc. 可搬型ｒｆ透過性発射筒を有する遠隔操作無人航空機レポート抑制発射機のためのシステムおよび装置
WO2011066031A2 (en) 2009-09-09 2011-06-03 Aerovironment, Inc. Elevon control system
US8342451B1 (en) 2009-12-08 2013-01-01 The Boeing Company Variable pitch airfoils
US8931739B1 (en) 2009-12-08 2015-01-13 The Boeing Company Aircraft having inflatable fuselage
US8727280B1 (en) 2009-12-08 2014-05-20 The Boeing Company Inflatable airfoil system having reduced radar and infrared observability
US9175702B1 (en) 2011-05-24 2015-11-03 Stephen Lee Bailey Externally supported foil with reversible camber and variable chord length
CA2918779C (en) * 2013-07-22 2021-03-16 Learjet Inc. Tailplane with positive camber
CN103387048B (zh) * 2013-07-27 2016-01-06 哈尔滨工业大学 气动驱动/变形/承载一体化的变体柔性后缘结构
CN103466076B (zh) * 2013-08-23 2015-12-02 中国航空工业集团公司西安飞机设计研究所 一种飞机平尾随动装置
ES2683159T3 (es) * 2015-12-31 2018-09-25 Airbus Operations S.L Aeronave con motores montados en la parte trasera
CN105691594A (zh) * 2016-01-19 2016-06-22 高萍 一种新的飞翼布局飞行器控制方法及控制装置
EP3448749B1 (de) 2016-04-25 2020-07-01 Bombardier Inc. Luftfahrzeugpitchregelungssystem mit elektronisch übersetztem höhenruder
US10106265B2 (en) 2016-06-24 2018-10-23 General Electric Company Stabilizer assembly for an aircraft AFT engine
US10518865B2 (en) * 2017-05-11 2019-12-31 Bell Helicopter Textron Inc. Aircraft horizontal stabilizer design
US10611460B2 (en) 2017-05-11 2020-04-07 Bell Helicopter Textron Inc. Aircraft vertical stabilizer design
CN110652713B (zh) * 2019-09-30 2021-02-19 浙江海洋大学 一种户外运动用回旋镖
CN112429199B (zh) * 2020-11-18 2021-09-24 北京北航天宇长鹰无人机科技有限公司 一种采用全动升降舵的无人机

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JP4568906B2 (ja) * 2004-12-16 2010-10-27 独立行政法人 宇宙航空研究開発機構 飛行体用翼、飛行体用翼複合材およびその製造方法

Also Published As

Publication number Publication date
JP2009542520A (ja) 2009-12-03
DE102006032003A1 (de) 2008-01-24
CN101495367A (zh) 2009-07-29
US20090289144A1 (en) 2009-11-26
CN101495367B (zh) 2013-04-24
EP2038171A1 (de) 2009-03-25
RU2448019C2 (ru) 2012-04-20
CA2656794A1 (en) 2008-01-17
WO2008006831A1 (en) 2008-01-17
DE102006032003B4 (de) 2015-10-22
RU2009103772A (ru) 2010-08-20
EP2038171B1 (de) 2011-09-07
JP5257996B2 (ja) 2013-08-07
US7963485B2 (en) 2011-06-21
BRPI0712881A2 (pt) 2012-10-09

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