FR2902756B1 - SYSTEM FOR DEPORTING THE GROUND OF AN AIRCRAFT AND AEROPLANE COMPRISING SUCH A SYSTEM - Google Patents
SYSTEM FOR DEPORTING THE GROUND OF AN AIRCRAFT AND AEROPLANE COMPRISING SUCH A SYSTEMInfo
- Publication number
- FR2902756B1 FR2902756B1 FR0652569A FR0652569A FR2902756B1 FR 2902756 B1 FR2902756 B1 FR 2902756B1 FR 0652569 A FR0652569 A FR 0652569A FR 0652569 A FR0652569 A FR 0652569A FR 2902756 B1 FR2902756 B1 FR 2902756B1
- Authority
- FR
- France
- Prior art keywords
- deporting
- aeroplane
- aircraft
- ground
- 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
Links
Classifications
-
- 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
- B64C9/06—Adjustable control surfaces or members, e.g. rudders with two or more independent movements
-
- 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
- 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
- B64C9/32—Air braking surfaces
- B64C9/323—Air braking surfaces associated with wings
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652569A FR2902756B1 (en) | 2006-06-21 | 2006-06-21 | SYSTEM FOR DEPORTING THE GROUND OF AN AIRCRAFT AND AEROPLANE COMPRISING SUCH A SYSTEM |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652569A FR2902756B1 (en) | 2006-06-21 | 2006-06-21 | SYSTEM FOR DEPORTING THE GROUND OF AN AIRCRAFT AND AEROPLANE COMPRISING SUCH A SYSTEM |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2902756A1 FR2902756A1 (en) | 2007-12-28 |
FR2902756B1 true FR2902756B1 (en) | 2008-08-29 |
Family
ID=37734285
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0652569A Expired - Fee Related FR2902756B1 (en) | 2006-06-21 | 2006-06-21 | SYSTEM FOR DEPORTING THE GROUND OF AN AIRCRAFT AND AEROPLANE COMPRISING SUCH A SYSTEM |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2902756B1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9296475B2 (en) | 2013-09-24 | 2016-03-29 | The Boeing Company | System and method for reducing the stopping distance of an aircraft |
US9656741B2 (en) | 2013-09-24 | 2017-05-23 | The Boeing Company | Control interface for leading and trailing edge devices |
US9327827B2 (en) | 2013-09-24 | 2016-05-03 | The Boeing Company | Leading and trailing edge device deflections during descent of an aircraft |
US9193440B2 (en) | 2013-09-24 | 2015-11-24 | The Boeing Company | Variable camber flap system and method |
US9180962B2 (en) * | 2013-09-24 | 2015-11-10 | The Boeing Company | Leading edge variable camber system and method |
US9771141B2 (en) | 2013-09-24 | 2017-09-26 | The Boeing Company | Leading edge system and method for approach noise reduction |
US9359065B2 (en) | 2013-09-24 | 2016-06-07 | The Boeing Company | System and method for optimizing performance of an aircraft |
US9821903B2 (en) | 2014-07-14 | 2017-11-21 | The Boeing Company | Closed loop control of aircraft control surfaces |
EP3653494A1 (en) * | 2018-11-16 | 2020-05-20 | Bombardier Inc. | High-lift actuation system having independent actuation control |
DE102022123020B3 (en) * | 2022-09-09 | 2024-01-04 | Paul-Matthias Schlecht | Wing arrangement comprising a main wing and a slat attached to it in front of the main wing in the opposite direction of flow |
GB2622619A (en) * | 2022-09-23 | 2024-03-27 | Airbus Operations Ltd | Flight control surface |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE383260A (en) * | ||||
GB517422A (en) * | 1938-07-19 | 1940-01-30 | Westland Aircraft Ltd | Improvements in or relating to aircraft |
DE748431C (en) * | 1941-07-08 | 1944-11-02 | Control for a spike mounted leading wing | |
DE3412371A1 (en) * | 1984-04-03 | 1985-11-07 | Franz Albert 3012 Langenhagen Agethen | Boundary-layer suction without motor-driven units for winged aircraft |
GB9104370D0 (en) * | 1991-03-01 | 1991-04-17 | British Aerospace | Manufacture of track cans |
DE10019185C2 (en) * | 2000-04-17 | 2003-06-05 | Airbus Gmbh | Arrangement for aerodynamic noise reduction of slats in a commercial aircraft |
-
2006
- 2006-06-21 FR FR0652569A patent/FR2902756B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2902756A1 (en) | 2007-12-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
ST | Notification of lapse |
Effective date: 20220205 |