GB2186849B - Variable camber leading edge arrangements for aircraft wings - Google Patents
Variable camber leading edge arrangements for aircraft wingsInfo
- Publication number
- GB2186849B GB2186849B GB8703502A GB8703502A GB2186849B GB 2186849 B GB2186849 B GB 2186849B GB 8703502 A GB8703502 A GB 8703502A GB 8703502 A GB8703502 A GB 8703502A GB 2186849 B GB2186849 B GB 2186849B
- Authority
- GB
- United Kingdom
- Prior art keywords
- leading edge
- aircraft wings
- variable camber
- edge arrangements
- camber leading
- 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
Links
Classifications
-
- 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
- B64C3/48—Varying camber by relatively-movable parts of wing structures
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Blinds (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8603669 | 1986-02-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8703502D0 GB8703502D0 (en) | 1987-03-25 |
GB2186849A GB2186849A (en) | 1987-08-26 |
GB2186849B true GB2186849B (en) | 1989-11-08 |
Family
ID=10593066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8703502A Expired GB2186849B (en) | 1986-02-19 | 1987-02-16 | Variable camber leading edge arrangements for aircraft wings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2186849B (en) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8702782D0 (en) * | 1987-02-07 | 1987-07-29 | British Aerospace | Aerodynamic control devices |
GB9607707D0 (en) * | 1996-04-13 | 1996-06-19 | Broadbent Michael C | A self-sealing parallelogram slat mechanism |
WO1997038900A1 (en) * | 1996-04-13 | 1997-10-23 | Michael Craig Broadbent | Variable camber wing mechanism |
GB0114634D0 (en) | 2001-06-15 | 2001-08-08 | Broadbent Michael C | Contiguous variable camber device |
DE102005027749B4 (en) | 2005-06-16 | 2011-07-28 | Airbus Operations GmbH, 21129 | Buoyancy-enhancing flap, in particular nose flap, for an aerodynamically effective wing |
US7753313B1 (en) * | 2006-09-19 | 2010-07-13 | The Boeing Company | Composite wing slat for aircraft |
GB0708641D0 (en) * | 2007-05-04 | 2007-06-13 | Goodrich Actuation Systems Ltd | Actuator |
DE102009026457A1 (en) | 2009-05-25 | 2010-12-09 | Eads Deutschland Gmbh | Aerodynamic component with deformable outer skin |
GB201006099D0 (en) | 2010-04-13 | 2010-05-26 | Airbus Operations Ltd | Slat support assembly |
US9296475B2 (en) | 2013-09-24 | 2016-03-29 | The Boeing Company | System and method for reducing the stopping distance of an aircraft |
US9359065B2 (en) | 2013-09-24 | 2016-06-07 | The Boeing Company | System and method for optimizing performance of an aircraft |
US9193440B2 (en) | 2013-09-24 | 2015-11-24 | The Boeing Company | Variable camber flap system and method |
US9656741B2 (en) | 2013-09-24 | 2017-05-23 | The Boeing Company | Control interface for leading and trailing edge devices |
US9771141B2 (en) | 2013-09-24 | 2017-09-26 | The Boeing Company | Leading edge system and method for approach noise reduction |
US9180962B2 (en) * | 2013-09-24 | 2015-11-10 | The Boeing Company | Leading edge variable camber system and method |
US9327827B2 (en) | 2013-09-24 | 2016-05-03 | The Boeing Company | Leading and trailing edge device deflections during descent of an aircraft |
US9821903B2 (en) | 2014-07-14 | 2017-11-21 | The Boeing Company | Closed loop control of aircraft control surfaces |
WO2021104940A1 (en) * | 2019-11-25 | 2021-06-03 | Airbus Operations Gmbh | A wing for an aircraft |
-
1987
- 1987-02-16 GB GB8703502A patent/GB2186849B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB8703502D0 (en) | 1987-03-25 |
GB2186849A (en) | 1987-08-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20050216 |