ATE524380T1 - Betätigungssystem für vorderkantenhochauftriebsvorrichtung - Google Patents

Betätigungssystem für vorderkantenhochauftriebsvorrichtung

Info

Publication number
ATE524380T1
ATE524380T1 AT08806803T AT08806803T ATE524380T1 AT E524380 T1 ATE524380 T1 AT E524380T1 AT 08806803 T AT08806803 T AT 08806803T AT 08806803 T AT08806803 T AT 08806803T AT E524380 T1 ATE524380 T1 AT E524380T1
Authority
AT
Austria
Prior art keywords
leading edge
lift device
pivot point
actuation mechanism
actuating system
Prior art date
Application number
AT08806803T
Other languages
English (en)
Inventor
Francois Cathelain
Edmund Kay
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE524380T1 publication Critical patent/ATE524380T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Basic Packing Technique (AREA)
  • Lifting Devices For Agricultural Implements (AREA)
  • Manipulator (AREA)
  • Paper (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Valve Device For Special Equipments (AREA)
AT08806803T 2007-10-31 2008-10-27 Betätigungssystem für vorderkantenhochauftriebsvorrichtung ATE524380T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0721284.8A GB0721284D0 (en) 2007-10-31 2007-10-31 Actuation system for leading edge high-lift device
PCT/GB2008/050996 WO2009056873A1 (en) 2007-10-31 2008-10-27 Actuation system for leading edge high-lift device

Publications (1)

Publication Number Publication Date
ATE524380T1 true ATE524380T1 (de) 2011-09-15

Family

ID=38834526

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08806803T ATE524380T1 (de) 2007-10-31 2008-10-27 Betätigungssystem für vorderkantenhochauftriebsvorrichtung

Country Status (10)

Country Link
US (1) US8967549B2 (de)
EP (1) EP2214959B1 (de)
JP (1) JP5427786B2 (de)
CN (1) CN101842288B (de)
AT (1) ATE524380T1 (de)
BR (1) BRPI0818132A8 (de)
CA (1) CA2700427C (de)
GB (1) GB0721284D0 (de)
RU (1) RU2478521C2 (de)
WO (1) WO2009056873A1 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
US10400818B2 (en) 2007-12-06 2019-09-03 Roller Bearing Company Of America, Inc. Track roller bearings with rolling elements or liners
CN102180259B (zh) * 2011-04-15 2014-05-07 天津全华时代航天科技发展有限公司 抗扰流的小型无人机
GB201108450D0 (en) * 2011-05-20 2011-07-06 Airbus Operations Ltd Aircraft wing assembly
CN102642615A (zh) * 2012-05-11 2012-08-22 中国航空工业集团公司西安飞机设计研究所 一种带单缝襟翼的飞机增升装置
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
US9816537B2 (en) 2013-02-27 2017-11-14 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US9163648B2 (en) 2013-02-27 2015-10-20 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US9631645B2 (en) 2013-02-27 2017-04-25 Woodward, Inc. Rotary piston actuator anti-rotation configurations
US9593696B2 (en) 2013-02-27 2017-03-14 Woodward, Inc. Rotary piston type actuator with hydraulic supply
US9234535B2 (en) 2013-02-27 2016-01-12 Woodward, Inc. Rotary piston type actuator
US9476434B2 (en) 2013-02-27 2016-10-25 Woodward, Inc. Rotary piston type actuator with modular housing
US8955425B2 (en) 2013-02-27 2015-02-17 Woodward, Inc. Rotary piston type actuator with pin retention features
TR201910783T4 (tr) 2015-06-18 2019-08-21 Bae Systems Plc Hava aracı kanat sistemi.
ES2746872T3 (es) 2015-06-18 2020-03-09 Bae Systems Plc Sistema de ala de una aeronave
DE102015013611A1 (de) * 2015-10-21 2017-04-27 Liebherr-Aerospace Lindenberg Gmbh Stellantrieb für ein Hochauftriebssystem eines Luftfahrzeuges
EP3339164A1 (de) * 2016-12-22 2018-06-27 Airbus Operations GmbH Flügel für ein flugzeug
EP3339163A1 (de) * 2016-12-22 2018-06-27 Airbus Operations GmbH Flügel für ein flugzeug
EP3444182B1 (de) * 2017-08-18 2023-01-18 Airbus Operations GmbH Flügel für ein flugzeug
US10919614B2 (en) * 2017-09-06 2021-02-16 Airbus Operations Gmbh Airfoil with a main wing and a high-lift body
JP6929809B2 (ja) * 2018-03-02 2021-09-01 三菱重工業株式会社 高揚力装置、翼及び航空機
GB201806477D0 (en) * 2018-04-20 2018-06-06 Moog Wolverhampton Ltd System for an aircraft wing
WO2019212767A1 (en) * 2018-04-30 2019-11-07 Kimberly-Clark Worldwide, Inc. Energy apparatus and methods of providing energy to an item
GB2579221A (en) 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism
WO2020174084A1 (en) 2019-02-28 2020-09-03 Airbus Operations Gmbh A wing leading-edge device and a wing having such a wing leading-edge device
DE102019111118A1 (de) * 2019-04-30 2020-11-05 Airbus Operations Gmbh Hochauftriebsvorrichtung für ein Flugzeug
US11199248B2 (en) 2019-04-30 2021-12-14 Woodward, Inc. Compact linear to rotary actuator
CN110683033B (zh) * 2019-10-31 2023-03-21 哈尔滨工程大学 一种可调距式旋翼
GB2588899A (en) * 2019-11-12 2021-05-19 Airbus Operations Ltd Aircraft wings having moveable structures
EP4133186B1 (de) 2020-04-08 2025-10-01 Woodward, Inc. Rotationskolbenaktuator mit einer zentralen betätigungsanordnung
CN113135283B (zh) * 2021-04-18 2023-01-20 西北工业大学 一种小体积高精度的富勒襟翼作动机构
CN113212734B (zh) * 2021-06-20 2023-02-14 西北工业大学 一种小体积轻量化的机翼前缘缝翼作动机构
US12179919B2 (en) * 2023-04-12 2024-12-31 The Boeing Company Slat movement system for aircraft
US12565306B2 (en) 2023-09-07 2026-03-03 The Boeing Company Variable slat displacement using spanwise actuator
US12486020B2 (en) 2023-12-08 2025-12-02 The Boeing Company Leading-edge droop actuation system

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB410375A (en) 1932-09-03 1934-05-17 Eugen Nenninger Improvements in and relating to locking devices
DE748431C (de) 1941-07-08 1944-11-02 Steuerung fuer einen auf Spiessen gelagerten Vorfluegel
GB998895A (en) * 1960-08-04 1965-07-21 Dehavilland Aircraft Improvements relating to aircraft
US3089666A (en) * 1961-04-13 1963-05-14 Boeing Co Airplane having changeable thrust direction
US3987983A (en) * 1974-12-20 1976-10-26 The Boeing Company Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism
US4040579A (en) * 1975-08-25 1977-08-09 The United States Of America As Represented By The Secretary Of The Navy Variable camber leading edge airfoil system
US4189120A (en) 1977-12-14 1980-02-19 Boeing Commercial Airplane Company Variable camber leading edge flap
US4202519A (en) * 1978-09-08 1980-05-13 The Boeing Company Airfoil leading edge slat apparatus
US4283029A (en) * 1979-01-02 1981-08-11 Rudolph Peter K C Actuating apparatus for a flap system having an upper surface blowing powered lift system
US4398688A (en) 1979-12-26 1983-08-16 Lockheed Corporation Leading edge flap for an airfoil
US4399970A (en) 1980-11-13 1983-08-23 The Boeing Company Wing leading edge slat
US4470569A (en) * 1981-12-28 1984-09-11 Mcdonnell Douglas Corporation Locking, redundant slat drive mechanism
GB2137569B (en) * 1983-03-30 1986-03-12 British Aerospace Leading edge arrangements for aircraft wings
US4585192A (en) * 1983-03-30 1986-04-29 British Aerospace Public Limited Company Leading edge arrangements for aircraft wings
US4544117A (en) * 1983-11-14 1985-10-01 Lockheed Corporation Leading edge flap and boundary layer control system
US4650140A (en) * 1985-12-30 1987-03-17 The Boeing Company Wind edge movable airfoil having variable camber
US4753402A (en) * 1985-12-30 1988-06-28 The Boeing Company Biased leading edge slat apparatus
DE3721479A1 (de) * 1987-06-30 1989-01-19 Messerschmitt Boelkow Blohm Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels
RU2022879C1 (ru) * 1991-04-09 1994-11-15 Авиационный научно-технический комплекс им.О.К.Антонова Носок крыла самолета
UA18676A (uk) * 1991-04-09 1997-12-25 Київський Механічний Завод Ім. О.К.Антонова Hосок крила літака
FR2695905B1 (fr) * 1992-09-24 1994-12-16 Aerospatiale Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
US5927656A (en) 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
GB9816936D0 (en) * 1998-08-05 1998-09-30 British Aerospace An aerofoil having a slat
DE10019185C2 (de) * 2000-04-17 2003-06-05 Airbus Gmbh Anordnung zur aerodynamischen Lärmminderung von Vorflügeln eines Verkehrsflugzeuges
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
GB0410375D0 (en) 2004-05-10 2004-06-16 Airbus Uk Ltd High lift device for an aircraft
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
EP1972547A1 (de) * 2007-03-21 2008-09-24 Asco Industries Flügelvorderkantenvorrichtung
GB0708334D0 (en) * 2007-04-30 2007-06-06 Airbus Uk Ltd Method and apparatus for deploying an auxiliary airfoil
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device

Also Published As

Publication number Publication date
CN101842288B (zh) 2014-06-04
JP5427786B2 (ja) 2014-02-26
WO2009056873A1 (en) 2009-05-07
GB0721284D0 (en) 2007-12-12
US20100187368A1 (en) 2010-07-29
CA2700427A1 (en) 2009-05-07
US8967549B2 (en) 2015-03-03
CN101842288A (zh) 2010-09-22
BRPI0818132A2 (pt) 2015-03-31
JP2011500454A (ja) 2011-01-06
BRPI0818132A8 (pt) 2016-01-05
RU2478521C2 (ru) 2013-04-10
CA2700427C (en) 2016-06-28
EP2214959B1 (de) 2011-09-14
EP2214959A1 (de) 2010-08-11
RU2010117755A (ru) 2011-12-10

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