FR921144A - Profil de fuite perfectionné - Google Patents
Profil de fuite perfectionnéInfo
- Publication number
- FR921144A FR921144A FR921144DA FR921144A FR 921144 A FR921144 A FR 921144A FR 921144D A FR921144D A FR 921144DA FR 921144 A FR921144 A FR 921144A
- Authority
- FR
- France
- Prior art keywords
- leak profile
- advanced leak
- advanced
- profile
- leak
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR921144T | 1945-10-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR921144A true FR921144A (fr) | 1947-04-28 |
Family
ID=9433881
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR921144D Expired FR921144A (fr) | 1945-10-30 | 1945-10-30 | Profil de fuite perfectionné |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR921144A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0275056A2 (fr) * | 1987-01-12 | 1988-07-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif de réglage pour volets sur profils d'aile |
US4867396A (en) * | 1983-05-18 | 1989-09-19 | Lockheed Corporation | Micro flap trailing edge device for an aircraft wing |
US6641089B2 (en) | 2001-09-27 | 2003-11-04 | Airbus Deutschland Gmbh | Flap arrangement for varying the aerodynamic lift generated by an aerodynamic element of an aircraft |
-
1945
- 1945-10-30 FR FR921144D patent/FR921144A/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4867396A (en) * | 1983-05-18 | 1989-09-19 | Lockheed Corporation | Micro flap trailing edge device for an aircraft wing |
EP0275056A2 (fr) * | 1987-01-12 | 1988-07-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif de réglage pour volets sur profils d'aile |
EP0275056A3 (fr) * | 1987-01-12 | 1989-12-06 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif de réglage pour volets sur profils d'aile |
US6641089B2 (en) | 2001-09-27 | 2003-11-04 | Airbus Deutschland Gmbh | Flap arrangement for varying the aerodynamic lift generated by an aerodynamic element of an aircraft |
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