FR2425379B1 - - Google Patents
Info
- Publication number
- FR2425379B1 FR2425379B1 FR7814107A FR7814107A FR2425379B1 FR 2425379 B1 FR2425379 B1 FR 2425379B1 FR 7814107 A FR7814107 A FR 7814107A FR 7814107 A FR7814107 A FR 7814107A FR 2425379 B1 FR2425379 B1 FR 2425379B1
- Authority
- FR
- France
- 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
- B64C9/06—Adjustable control surfaces or members, e.g. rudders with two or more independent movements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7814107A FR2425379A1 (en) | 1978-05-08 | 1978-05-08 | Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7814107A FR2425379A1 (en) | 1978-05-08 | 1978-05-08 | Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2425379A1 FR2425379A1 (en) | 1979-12-07 |
| FR2425379B1 true FR2425379B1 (en) | 1983-08-19 |
Family
ID=9208163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7814107A Granted FR2425379A1 (en) | 1978-05-08 | 1978-05-08 | Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2425379A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2901537B1 (en) | 2006-05-29 | 2008-07-04 | Airbus France Sas | METHOD AND DEVICE FOR CONTROLLING AN AIRCRAFT OPTIMIZING THE CONTROL OF AILERONS IN HYPERSUSTENT CONFIGURATION |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR719771A (en) * | 1930-10-06 | 1932-02-10 | Mureaux Sa Des Atel Des | Surface mounting of control surfaces for aircraft |
| US2007964A (en) * | 1933-02-15 | 1935-07-16 | Carl J Crane | Airplane stabilizer |
| FR882978A (en) * | 1940-10-22 | 1943-06-21 | Luftfahrtgeratewerk Hakenfelde | Aircraft steering motor device |
| FR881541A (en) * | 1941-04-25 | 1943-04-28 | Messerschmitt Boelkow Blohm | Aircraft transverse control |
| DE1004934B (en) * | 1954-11-05 | 1957-03-21 | Bendix Aviat Corp | Device for controlling the rolling movement of a vehicle, in particular an aircraft |
| FR1141117A (en) * | 1956-01-16 | 1957-08-26 | Sncan | Advanced aerodyne |
| FR1207944A (en) * | 1958-07-29 | 1960-02-19 | Morane Saulnier | Aircraft warping device |
| DE2103639A1 (en) * | 1971-01-27 | 1972-09-07 | Messerschmitt-Bölkow-Blöhm GmbH, 8000 München | Airfoil for aircraft with one or more one-part or multi-part slotted flaps |
| DE2125971C3 (en) * | 1971-05-26 | 1978-08-03 | Vereinigte Flugtechnische Werkefokker Gmbh, 2800 Bremen | Flap arrangement for an aircraft wing |
-
1978
- 1978-05-08 FR FR7814107A patent/FR2425379A1/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| FR2425379A1 (en) | 1979-12-07 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |