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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB987658A (en) | Rotary index table of a machine tool | |
US2396309A (en) | Airplane control | |
GB561813A (en) | Unit for controlling the elevator, rudder and ailerons of an aircraft | |
GB546210A (en) | Improvements in vehicle and aircraft control columns | |
US2399200A (en) | Range input and hand control unit for aircraft turret guns | |
GB592735A (en) | Improvements relating to linear actuating mechanisms | |
GB614658A (en) | Improvements in or relating to remote control means for gear change mechanisms | |
GB618773A (en) | Improvements in or relating to firing gear for guns | |
GB566311A (en) | Improvements relating to controlling means for variable speed power transmitting mechanisms | |
GB557464A (en) | Improvements in aircraft controls | |
FR882854A (en) | Improvements to central control clutches by single rod | |
GB608362A (en) | Improvements relating to screw and nut mechanisms | |
GB643010A (en) | Ladder control device | |
GB103918A (en) | Improvements relating to Duplicate Controlling Means applicable to Aeroplanes and the like. | |
GB599984A (en) | Improvements in hand-rakes | |
GB543559A (en) | Improvements in the adjustment and mounting of trimmer tabs on elevators, rudders and other parts of aeroplanes | |
GB558101A (en) | Improvements in aircraft control columns | |
GB519532A (en) | Improvements relating to operating gear for aircraft controls | |
GB645250A (en) | Improvements in or relating to chucks | |
GB573303A (en) | Improvements in and relating to power operated gun mountings or turrets | |
GB858740A (en) | Drilling and the like arrangement fitted on a lathe tailstock | |
AU132433B2 (en) | Improved control mechanism for variable pitch propellers | |
GB658302A (en) | Improvements in or relating to control mechanism for aircraft | |
GB570718A (en) | Improvements relating to engine starting mechanisms | |
GB954639A (en) | Gear-operating mechanism for lathes and other similar or suitable appliances |