FR846337A - Dispositif hypersustentateur - Google Patents
Dispositif hypersustentateurInfo
- Publication number
- FR846337A FR846337A FR846337DA FR846337A FR 846337 A FR846337 A FR 846337A FR 846337D A FR846337D A FR 846337DA FR 846337 A FR846337 A FR 846337A
- Authority
- FR
- France
- Prior art keywords
- lift device
- high lift
- 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.)
- Expired
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR846337T | 1938-05-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR846337A true FR846337A (fr) | 1939-09-14 |
Family
ID=9313273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR846337D Expired FR846337A (fr) | 1938-05-17 | 1938-05-17 | Dispositif hypersustentateur |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR846337A (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2668027A (en) * | 1948-08-10 | 1954-02-02 | Vincent J Burnelli | Airplane flap and ground contact control means therefor |
US2772058A (en) * | 1951-05-10 | 1956-11-27 | Charles H Grant | Aircraft wing with means to increase lift through control of air flow |
US2924399A (en) * | 1956-04-23 | 1960-02-09 | North American Aviation Inc | Aircraft flap structure |
US6601801B1 (en) * | 2002-04-24 | 2003-08-05 | The Boeing Company | Gapped trailing-edge control surface for an airfoil |
US8336829B2 (en) | 2005-09-23 | 2012-12-25 | Airbus Operations Gmbh | Advanced trailing edge control surface on the wing of an aircraft |
-
1938
- 1938-05-17 FR FR846337D patent/FR846337A/fr not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2668027A (en) * | 1948-08-10 | 1954-02-02 | Vincent J Burnelli | Airplane flap and ground contact control means therefor |
US2772058A (en) * | 1951-05-10 | 1956-11-27 | Charles H Grant | Aircraft wing with means to increase lift through control of air flow |
US2924399A (en) * | 1956-04-23 | 1960-02-09 | North American Aviation Inc | Aircraft flap structure |
US6601801B1 (en) * | 2002-04-24 | 2003-08-05 | The Boeing Company | Gapped trailing-edge control surface for an airfoil |
US8336829B2 (en) | 2005-09-23 | 2012-12-25 | Airbus Operations Gmbh | Advanced trailing edge control surface on the wing of an aircraft |
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