CN1065193C - 用于飞行器机翼的可变缝隙空气制动器 - Google Patents

用于飞行器机翼的可变缝隙空气制动器 Download PDF

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Publication number
CN1065193C
CN1065193C CN95113176.1A CN95113176A CN1065193C CN 1065193 C CN1065193 C CN 1065193C CN 95113176 A CN95113176 A CN 95113176A CN 1065193 C CN1065193 C CN 1065193C
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CN
China
Prior art keywords
wing plate
power
absorption fan
axle
wing
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.)
Expired - Fee Related
Application number
CN95113176.1A
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English (en)
Chinese (zh)
Other versions
CN1130140A (zh
Inventor
D·西普里安
B·赫马杜
P·肖梅尔
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Airbus Group SAS
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Airbus Group SAS
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Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of CN1130140A publication Critical patent/CN1130140A/zh
Application granted granted Critical
Publication of CN1065193C publication Critical patent/CN1065193C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Invalid Beds And Related Equipment (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Body Structure For Vehicles (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
CN95113176.1A 1994-12-26 1995-12-22 用于飞行器机翼的可变缝隙空气制动器 Expired - Fee Related CN1065193C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9415641 1994-12-26
FR9415641A FR2728535A1 (fr) 1994-12-26 1994-12-26 Aerofrein a fente variable pour voilure d'aeronef

Publications (2)

Publication Number Publication Date
CN1130140A CN1130140A (zh) 1996-09-04
CN1065193C true CN1065193C (zh) 2001-05-02

Family

ID=9470237

Family Applications (1)

Application Number Title Priority Date Filing Date
CN95113176.1A Expired - Fee Related CN1065193C (zh) 1994-12-26 1995-12-22 用于飞行器机翼的可变缝隙空气制动器

Country Status (7)

Country Link
US (1) US5735485A (enExample)
EP (1) EP0719704B1 (enExample)
CN (1) CN1065193C (enExample)
CA (1) CA2165513C (enExample)
DE (1) DE69511836T2 (enExample)
ES (1) ES2138171T3 (enExample)
FR (1) FR2728535A1 (enExample)

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CN101155726B (zh) * 2005-04-11 2013-03-13 空中客车德国运营有限责任公司 用于调整飞行器升力特性的装置及方法

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WO2006016070A1 (fr) * 2004-07-16 2006-02-16 Airbus France Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi
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US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
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US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) † 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
DE102005045759A1 (de) * 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
DE102006030315A1 (de) * 2006-06-30 2008-01-17 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
DE102006058561B4 (de) * 2006-12-12 2010-08-26 Hs Genion Gmbh Funktionseinrichtung mit schwenkbarem Element
DE102006059724B4 (de) * 2006-12-18 2011-03-17 Hs Genion Gmbh Luftleitvorrichtung für ein Fahrzeug
DE102007009060A1 (de) * 2007-02-23 2008-08-28 Airbus Deutschland Gmbh Spoiler für eine aerodynamisch wirksame Fläche eines Luftfahrzeugs
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8231079B2 (en) * 2008-03-31 2012-07-31 Honda Patents & Technologies North America, Llc Aerodynamic braking device for aircraft
DE102008020654B4 (de) 2008-04-24 2018-10-04 Airbus Operations Gmbh Tragflügel und Flugzeug mit einer Lateral-Kopplungsvorrichtung
IT1390909B1 (it) * 2008-07-16 2011-10-19 Alenia Aeronautica Spa Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi
EP2174867A1 (de) * 2008-10-10 2010-04-14 Technische Universität München Vorrichtung zum Erzeugen von aerodynamischem Widerstand an einem Luftfahrzeug
GB0911012D0 (en) * 2009-06-25 2009-08-12 Airbus Operations Ltd Cross-bleed dam
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
CN112124563B (zh) * 2009-09-09 2025-02-07 威罗门飞行公司 升降副翼控制系统
US8857761B2 (en) 2010-10-27 2014-10-14 Ata Engineering, Inc. Variable geometry aircraft pylon structure and related operation techniques
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US9567867B2 (en) 2011-09-14 2017-02-14 Ata Engineering, Inc. Methods and apparatus for deployable swirl vanes
CN102540961B (zh) * 2012-01-10 2013-11-13 上海庞丰交通设备科技有限公司 基于plc控制的空气动力制动控制系统
CN103448902A (zh) * 2012-05-29 2013-12-18 中国航空工业集团公司西安飞机设计研究所 一种下单翼飞机的应急断离结构的内襟翼支臂梁及应用
US9108715B2 (en) * 2012-05-29 2015-08-18 The Boeing Company Rotary actuated high lift gapped aileron
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CN104166348B (zh) * 2014-08-07 2016-08-17 北京理工大学 一种单滑块变质心控制飞行器的动态稳定性判定方法
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US11286032B2 (en) * 2019-08-30 2022-03-29 The Boeing Company Butterfly folding fairing
US11548616B1 (en) 2020-03-02 2023-01-10 Lucas Kai-Luen Hung Split-flap wing assembly for a high endurance aircraft
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GB2605195B (en) 2021-03-26 2023-12-13 Airbus Operations Ltd Trailing edge panel support with movable connector
GB2605197B (en) 2021-03-26 2023-12-13 Airbus Operations Ltd Aircraft wing with trailing edge panel
GB2605196B (en) * 2021-03-26 2024-01-10 Airbus Operations Ltd Trailing edge panel support
GB2605194B (en) 2021-03-26 2023-12-13 Airbus Operations Ltd Trailing edge panel support with biasing arrangement
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101155726B (zh) * 2005-04-11 2013-03-13 空中客车德国运营有限责任公司 用于调整飞行器升力特性的装置及方法

Also Published As

Publication number Publication date
FR2728535B1 (enExample) 1997-03-07
EP0719704A1 (fr) 1996-07-03
DE69511836D1 (de) 1999-10-07
CA2165513C (fr) 2009-04-07
US5735485A (en) 1998-04-07
DE69511836T2 (de) 2000-04-13
CA2165513A1 (fr) 1996-06-27
EP0719704B1 (fr) 1999-09-01
ES2138171T3 (es) 2000-01-01
FR2728535A1 (fr) 1996-06-28
CN1130140A (zh) 1996-09-04

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Granted publication date: 20010502

Termination date: 20131222