GB371526A - Combined controlling device for steering and stabilising aircraft - Google Patents
Combined controlling device for steering and stabilising aircraftInfo
- Publication number
- GB371526A GB371526A GB5682/31A GB568231A GB371526A GB 371526 A GB371526 A GB 371526A GB 5682/31 A GB5682/31 A GB 5682/31A GB 568231 A GB568231 A GB 568231A GB 371526 A GB371526 A GB 371526A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- pillar
- pulley
- ailerons
- rudder
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
371,526. Aircraft control gear. BERNARDI, M. DE, 42, Via Della Mercede, Rome. Feb. 23, 1931, No. 5682. [Class 4.] The elevator, ailerons, rudder, and wheel brakes of an aeroplane are controlled by a single device comprising a hand-wheel 11 mounted on a pillar 37, 38 capable of fore and aft rocking movements. Rotation of the hand-wheel 11 moves the rudder, ailerons, and brakes, simultaneously, and rocking movements of the pillar control the elevator. A second control wheel may be provided mounted on another arm set on the pillar symmetrically to the part 38. The shaft of the wheel 11 has a sprocket 8 connected by a chain to a sprocket 5 on a shaft 4 to which a double grooved pulley 2 and a pulley 1 are keyed. A third pulley 3 is loose on the shaft but has a projection engaging abutments on the wheel 2. The pillar 37 is mounted on a transverse tube 17 carrying a lever 16 to which the elevator cables are connected, and cables from the pulleys 1, 2, 3 are led around the pulleys shown and through the tube 17 to the rudder, ailerons, and wheel brakes respectively. A fixed casing 39 encloses the pillar 37. An eccentric 40 with actuating lever 41 is mounted on a support 42 on the pillar to lock the pulley 1 in any adjusted position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5682/31A GB371526A (en) | 1931-02-23 | 1931-02-23 | Combined controlling device for steering and stabilising aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5682/31A GB371526A (en) | 1931-02-23 | 1931-02-23 | Combined controlling device for steering and stabilising aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB371526A true GB371526A (en) | 1932-04-28 |
Family
ID=9800660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5682/31A Expired GB371526A (en) | 1931-02-23 | 1931-02-23 | Combined controlling device for steering and stabilising aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB371526A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102564718A (en) * | 2010-12-10 | 2012-07-11 | 上海卫星工程研究所 | Steering device for satellite vibration test |
-
1931
- 1931-02-23 GB GB5682/31A patent/GB371526A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102564718A (en) * | 2010-12-10 | 2012-07-11 | 上海卫星工程研究所 | Steering device for satellite vibration test |
| CN102564718B (en) * | 2010-12-10 | 2015-05-27 | 上海卫星装备研究所 | Steering device for satellite vibration test |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2548481A (en) | Flying control for aircraft | |
| GB371526A (en) | Combined controlling device for steering and stabilising aircraft | |
| US2080067A (en) | Transmission | |
| US2045579A (en) | Automatic level control for aircraft | |
| US2167533A (en) | Torque compensator for airplanes | |
| US2207042A (en) | Propeller control mechanism for adjustable and reversible pitch propellers | |
| US2439393A (en) | Synchronized control unit | |
| US2826937A (en) | Actuator mechanical control system | |
| GB343630A (en) | Improvements relating to the control of aeroplanes | |
| GB546210A (en) | Improvements in vehicle and aircraft control columns | |
| US1373433A (en) | Control-column | |
| GB856267A (en) | Improvements in or relating to vehicles capable of travelling in opposite directions | |
| GB471583A (en) | Improvements in and relating to dual control devices of aircraft or of other machines | |
| GB173213A (en) | Improvements in and relating to means for controlling aeroplanes | |
| US2103933A (en) | Aeroplane control | |
| US1675935A (en) | Aeroplane steering device | |
| GB1116654A (en) | Recreational swing assembly | |
| GB130141A (en) | Improvements in or relating to Controls for Aeroplanes and the like. | |
| GB660825A (en) | Improvements in or relating to aircraft control members | |
| GB557259A (en) | A new or improved control mechanism for aeroplanes | |
| GB184317A (en) | Improvements in or relating to aileron control-mechanism | |
| GB299192A (en) | Improvements in or relating to controlling devices for aeroplanes and similar aircraft | |
| GB128040A (en) | Improvements in or relating to Stabilisers for Aeroplanes. | |
| GB622837A (en) | Improvements in or relating to helicopters | |
| GB431648A (en) | Improvements in or relating to control mechanism for aeroplanes |