GB471583A - Improvements in and relating to dual control devices of aircraft or of other machines - Google Patents
Improvements in and relating to dual control devices of aircraft or of other machinesInfo
- Publication number
- GB471583A GB471583A GB447237A GB447237A GB471583A GB 471583 A GB471583 A GB 471583A GB 447237 A GB447237 A GB 447237A GB 447237 A GB447237 A GB 447237A GB 471583 A GB471583 A GB 471583A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pulley
- arm
- aircraft
- relating
- machines
- 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
- B64C13/24—Transmitting means
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jib Cranes (AREA)
Abstract
471,583. Controlling aircraft. OPLINTER, J. G. M. J. DE W. D'. Feb. 15, 1937, No. 4472. [Class 4] In dual-control apparatus of the kind in which a hand wheel mounted on the control column is swingable sideways so as to be operable from either of two side-by-side seats, the foot-operated controls are similarly displaced. Fig. 2 shows a wheel 1 carried by an arm 2 pivotally mounted on a control column 3. Fast on the pivot axle of arm 2 is a pulley 10 around which passes Bowden cables 8 which also pass round a second pulley 10 concentric with the axis of a swinging arm 5 carrying rudder bar 4. Movement of bar 4 is transmitted by chain gearing to a pulley on a central two-armed lever 7 connected to the rudder by cables 11. Travel of arms 2 and 5 is limited by stops which are adjustable to suit the controls to pilots of differing height.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB447237A GB471583A (en) | 1937-02-15 | 1937-02-15 | Improvements in and relating to dual control devices of aircraft or of other machines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB447237A GB471583A (en) | 1937-02-15 | 1937-02-15 | Improvements in and relating to dual control devices of aircraft or of other machines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB471583A true GB471583A (en) | 1937-09-07 |
Family
ID=9777817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB447237A Expired GB471583A (en) | 1937-02-15 | 1937-02-15 | Improvements in and relating to dual control devices of aircraft or of other machines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB471583A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4114843A (en) * | 1976-10-04 | 1978-09-19 | Robinson Helicopter Co. | Control stick assembly |
| US5427336A (en) * | 1993-02-24 | 1995-06-27 | Haggerty; Matthew K. | Dual control mechanism for aircraft |
| US5527004A (en) * | 1993-02-24 | 1996-06-18 | Helix Air, Inc. | Control system for aircraft |
-
1937
- 1937-02-15 GB GB447237A patent/GB471583A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4114843A (en) * | 1976-10-04 | 1978-09-19 | Robinson Helicopter Co. | Control stick assembly |
| US5427336A (en) * | 1993-02-24 | 1995-06-27 | Haggerty; Matthew K. | Dual control mechanism for aircraft |
| US5527004A (en) * | 1993-02-24 | 1996-06-18 | Helix Air, Inc. | Control system for aircraft |
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