GB0906270D0 - High lift devices for aircraft - Google Patents
High lift devices for aircraftInfo
- 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
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)
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 (en) | 2009-04-14 | 2010-04-13 | High lift devices for aircraft |
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 (en) |
WO (1) | WO2010119280A1 (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US9476434B2 (en) | 2013-02-27 | 2016-10-25 | Woodward, Inc. | Rotary piston type actuator with modular housing |
US9631645B2 (en) | 2013-02-27 | 2017-04-25 | Woodward, Inc. | Rotary piston actuator anti-rotation configurations |
US9234535B2 (en) | 2013-02-27 | 2016-01-12 | Woodward, Inc. | Rotary piston type actuator |
US8955425B2 (en) | 2013-02-27 | 2015-02-17 | Woodward, Inc. | Rotary piston type actuator with pin retention features |
WO2016203256A1 (en) | 2015-06-18 | 2016-12-22 | Bae Systems Plc | Aircraft wing system |
AU2016278098B2 (en) | 2015-06-18 | 2020-06-18 | Bae Systems Plc | Aircraft wing system |
EP3106385A1 (en) * | 2015-06-18 | 2016-12-21 | 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 (en) * | 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 | Power increases wing |
WO2021207482A1 (en) | 2020-04-08 | 2021-10-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
EP4030079A1 (en) | 2021-01-15 | 2022-07-20 | Goodrich Actuation Systems Limited | Rotary geared actuator |
Family Cites Families (12)
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 (en) | 1985-07-31 | 1987-02-12 | Airbus Gmbh | WING WITH EXTENDABLE FLAP AND CHANGEABLE BURNER |
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 (en) | 2003-02-26 | 2004-07-15 | Liebherr-Aerospace Lindenberg Gmbh | Aircraft landing flaps operating drive with overload protection provided by electrical load sensor at point of transmission of central drive energy to each individual flap body operating drive |
DE10313728B4 (en) * | 2003-03-27 | 2011-07-21 | Airbus Operations GmbH, 21129 | Flap system on the wing of a fixed-wing aircraft |
DE10361891A1 (en) | 2003-12-23 | 2005-08-04 | Airbus Deutschland Gmbh | Device for controlling and adjusting flaps on aircraft wings |
US7494094B2 (en) | 2004-09-08 | 2009-02-24 | The Boeing Company | Aircraft wing systems for providing differential motion to deployable lift devices |
DE102005017307A1 (en) * | 2005-04-14 | 2006-10-26 | Airbus Deutschland Gmbh | Landing flap drive system for use in aircraft, is connected to track of landing flap which is operated by drive motor |
-
2009
- 2009-04-14 GB GBGB0906270.4A patent/GB0906270D0/en not_active Ceased
-
2010
- 2010-04-13 WO PCT/GB2010/050612 patent/WO2010119280A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2010119280A1 (en) | 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) |