GB527393A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB527393A GB527393A GB10959/39A GB1095939A GB527393A GB 527393 A GB527393 A GB 527393A GB 10959/39 A GB10959/39 A GB 10959/39A GB 1095939 A GB1095939 A GB 1095939A GB 527393 A GB527393 A GB 527393A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ailerons
- link
- shaft
- flap
- aileron
- 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
- B64C9/32—Air braking surfaces
- B64C9/323—Air braking surfaces associated with wings
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
527,393. Controlling aircraft. JUNKERS FLUGZEUG-UND-MOTORENWERKE AKT.- GES. April 11, 1939, No. 10959. Convention date, April 9, 1938. [Class 4] An aircraft having means for influencing the airflow about the wing to act as a brake has means whereby, when the retarding device is set in the operative position, the transmission members of the aileron control are adjusted to restrict or prevent the angular movement of such portions of the ailerons as lie in the wake of the retarding device. As shown, ailerons 2 are operated from a rod 5 through a bell-crank lever 6 and a link 7, further ailerons 3 disposed in the wake of adjustable flaps 1 are actuated from the shaft 5 through a rocking-shaft 8 a member 22 slidable on the shaft, links 9, 11 and a bell-crank lever 10. The link 9 is connected by a link 18 to the flap 1 so that upon adjustment of the flap through a rod 12 angular deflection of the aileron 3 is diminished or suppressed. When the flap 1 is brought into the braking position the link 9 may come into line with the pivot of the shaft 8 so that the aileron 3 is locked, preferably in a slightly depressed position. Alternatively, other locking means may be provided and the transmission to the ailerons 3 uncoupled when the flaps 1 are brought into use.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE527393X | 1938-04-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB527393A true GB527393A (en) | 1940-10-08 |
Family
ID=6553303
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10959/39A Expired GB527393A (en) | 1938-04-09 | 1939-04-11 | Improvements in and relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB527393A (en) |
-
1939
- 1939-04-11 GB GB10959/39A patent/GB527393A/en not_active Expired
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