GB561813A - Unit for controlling the elevator, rudder and ailerons of an aircraft - Google Patents
Unit for controlling the elevator, rudder and ailerons of an aircraftInfo
- Publication number
- GB561813A GB561813A GB1742042A GB1742042A GB561813A GB 561813 A GB561813 A GB 561813A GB 1742042 A GB1742042 A GB 1742042A GB 1742042 A GB1742042 A GB 1742042A GB 561813 A GB561813 A GB 561813A
- Authority
- GB
- United Kingdom
- Prior art keywords
- elevator
- aircraft
- rudder
- unit
- controlling
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
561,813. Aircraft controls. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR W. G., THOMPSON, J. A., and CAMPBELL, A. H. Dec. 8, 1942, No. 17420. [Class 4] A unit to be fitted to an aircraft for the control of the elevator, ailerons and rudder includes in the example shown a stationary casing 11 containing a telescopic control rod of which a tubular part 12 is axially movable for controlling through a rack 15 a sprocket E actuating the elevator and another part 32 is rotatable to actuate an aileron control sprocket A on its end remote from the controlling wheel 13. As shown in Fig. 7, the wheel 13 is secured on the reduced end of a tube 31 which is rotatable within the part 12 and axially movable with it ; the tube 31 communicates its rotary movement to the part 32 through a sliding splined connection including the balls 33. A shaft 36 carrying a rudder-control sprocket R is actuated through a gear-box 37 with foot-actuated bars 39 on each side, adjustment of the connections of these bars being effected by a handle 48 and jointed shaft 47. Automatic servo-controls may be added to the unit. To lock the elevator a clamping ring 23 is provided round the part 12.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1742042A GB561813A (en) | 1942-12-08 | 1942-12-08 | Unit for controlling the elevator, rudder and ailerons of an aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1742042A GB561813A (en) | 1942-12-08 | 1942-12-08 | Unit for controlling the elevator, rudder and ailerons of an aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB561813A true GB561813A (en) | 1944-06-06 |
Family
ID=10094886
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1742042A Expired GB561813A (en) | 1942-12-08 | 1942-12-08 | Unit for controlling the elevator, rudder and ailerons of an aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB561813A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2562974A (en) * | 1945-11-30 | 1951-08-07 | Sterry B Williams | Rudder pedal adjustment |
-
1942
- 1942-12-08 GB GB1742042A patent/GB561813A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2562974A (en) * | 1945-11-30 | 1951-08-07 | Sterry B Williams | Rudder pedal adjustment |
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