GB0906270D0 - High lift devices for aircraft - Google Patents

High lift devices for aircraft

Info

Publication number
GB0906270D0
GB0906270D0 GBGB0906270.4A GB0906270A GB0906270D0 GB 0906270 D0 GB0906270 D0 GB 0906270D0 GB 0906270 A GB0906270 A GB 0906270A GB 0906270 D0 GB0906270 D0 GB 0906270D0
Authority
GB
United Kingdom
Prior art keywords
aircraft
high lift
lift devices
devices
lift
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
GBGB0906270.4A
Other languages
English (en)
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.)
Moog Wolverhampton Ltd
Original Assignee
GE Aviation Systems 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 GE Aviation Systems Ltd filed Critical GE Aviation Systems Ltd
Priority to GBGB0906270.4A priority Critical patent/GB0906270D0/en
Publication of GB0906270D0 publication Critical patent/GB0906270D0/en
Priority to PCT/GB2010/050612 priority patent/WO2010119280A1/fr
Ceased legal-status Critical Current

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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
    • 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)
  • Transmission Devices (AREA)
GBGB0906270.4A 2009-04-14 2009-04-14 High lift devices for aircraft Ceased GB0906270D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GBGB0906270.4A GB0906270D0 (en) 2009-04-14 2009-04-14 High lift devices for aircraft
PCT/GB2010/050612 WO2010119280A1 (fr) 2009-04-14 2010-04-13 Dispositifs hypersustentateurs pour avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0906270.4A GB0906270D0 (en) 2009-04-14 2009-04-14 High lift devices for aircraft

Publications (1)

Publication Number Publication Date
GB0906270D0 true GB0906270D0 (en) 2009-05-20

Family

ID=40750451

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0906270.4A Ceased GB0906270D0 (en) 2009-04-14 2009-04-14 High lift devices for aircraft

Country Status (2)

Country Link
GB (1) GB0906270D0 (fr)
WO (1) WO2010119280A1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9476434B2 (en) 2013-02-27 2016-10-25 Woodward, Inc. Rotary piston type actuator with modular housing
US9234535B2 (en) 2013-02-27 2016-01-12 Woodward, Inc. Rotary piston type actuator
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
US9163648B2 (en) 2013-02-27 2015-10-20 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US9816537B2 (en) 2013-02-27 2017-11-14 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US8955425B2 (en) 2013-02-27 2015-02-17 Woodward, Inc. Rotary piston type actuator with pin retention features
EP3106385A1 (fr) * 2015-06-18 2016-12-21 BAE Systems PLC Systeme d'aile d'aeronef
US10633079B2 (en) 2015-06-18 2020-04-28 Bae Systems Plc Aircraft wing system
AU2016278098B2 (en) 2015-06-18 2020-06-18 Bae Systems Plc Aircraft wing system
US11199248B2 (en) 2019-04-30 2021-12-14 Woodward, Inc. Compact linear to rotary actuator
US11866155B2 (en) 2019-09-17 2024-01-09 Airbus Operations Gmbh Actuator arrangement for a fixed leading edge member of an aircraft, wing assembly and aircraft equipped with said actuator arrangement
CN111017194B (zh) * 2019-12-24 2023-08-04 中国航空工业集团公司西安飞机设计研究所 一种动力增升机翼
CN115667734A (zh) 2020-04-08 2023-01-31 伍德沃德有限公司 带有中心致动组件的旋转活塞型致动器

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB470923A (en) * 1936-02-24 1937-08-24 Joseph Ksoll Supporting surface for flying machines
US3767140A (en) 1971-11-03 1973-10-23 Mc Donnell Douglas Corp Airplane flaps
GB1487077A (en) 1975-10-20 1977-09-28 Secr Defence Aircraft wing assemblies
DE3527497A1 (de) 1985-07-31 1987-02-12 Airbus Gmbh Tragfluegel mit ausfahrbarer klappe und veraenderbarer woelbung
US4784355A (en) 1986-11-10 1988-11-15 The United States Of America As Represented By The Secretary Of The Air Force Flap system for short takeoff and landing aircraft
US5628477A (en) * 1995-02-13 1997-05-13 The Boeing Company Auxiliary airfoil lost motion detector and actuator
US5719566A (en) * 1996-06-28 1998-02-17 Sundstrand Corporation Method and apparatus for detecting dormant actuator failure
DE10308301B3 (de) 2003-02-26 2004-07-15 Liebherr-Aerospace Lindenberg Gmbh Flugzeughochauftriebssystem mit Überlastsicherung
DE10313728B4 (de) * 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
DE10361891A1 (de) 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
DE102005017307A1 (de) * 2005-04-14 2006-10-26 Airbus Deutschland Gmbh Landeklappenantriebssystem

Also Published As

Publication number Publication date
WO2010119280A1 (fr) 2010-10-21

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Legal Events

Date Code Title Description
COOA Change in applicant's name or ownership of the application

Owner name: MOOG WOLVERHAMPTON LIMITED

Free format text: FORMER OWNER: GE AVIATION SYSTEMS LIMITED

AT Applications terminated before publication under section 16(1)