GB742383A - Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraft - Google Patents
Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraftInfo
- Publication number
- GB742383A GB742383A GB23593/51A GB2359351A GB742383A GB 742383 A GB742383 A GB 742383A GB 23593/51 A GB23593/51 A GB 23593/51A GB 2359351 A GB2359351 A GB 2359351A GB 742383 A GB742383 A GB 742383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- machmeter
- levers
- secured
- feel
- 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
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/345—Transmitting means without power amplification or where power amplification is irrelevant mechanical with artificial feel
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
742,383. Controlling aircraft. BOULTON PAUL AIRCRAFT, Ltd. Oct. 9, 1952 [Oct. 10, 1951], No. 23593/51. Class 4. Means for providing " feel " in poweroperated flying control systems for aircraft include means for opposing the displacement of the control column in a direction to give lateral control, by a force controlled by a Machmeter on the aircraft so that the opposing force increases with increase in Mach number. The pilot's control column 1 is movable about axes a-a, e-e to operate links A and E connected respectively to servo mechanisms for operating the ailerons and elevators. Connected also to the column 1 are rods 2a, 2e, the free ends of which carry pins engaging in slots 7a, 7e in levers 3a, 3e respectively secured to torsion bars 4a, 4e. The pins on the ends of the rods 2a, 2e are secured to actuators 8a, 8e, the actuator 8e being controlled by a transmitter 9 driven by a rod 10 connected to the dynamic pressure capsule 11 of a Machmeter, and the actuator 8s being operated by a transmitter 12 into which is fed a signal derived from the divider and converter 13 of the Machmeter 15. Trimmer actuators 5a, 5e are connected to levers secured to the ends of the torque tubes 4a, 4e remote from the levers 3a, 3e.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23593/51A GB742383A (en) | 1951-10-10 | 1951-10-10 | Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23593/51A GB742383A (en) | 1951-10-10 | 1951-10-10 | Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB742383A true GB742383A (en) | 1955-12-30 |
Family
ID=10198190
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23593/51A Expired GB742383A (en) | 1951-10-10 | 1951-10-10 | Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB742383A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2912193A (en) * | 1955-08-23 | 1959-11-10 | Fairey Aviat Co Ltd | Aircraft controls |
US2955784A (en) * | 1956-02-27 | 1960-10-11 | Northrop Corp | Servo regulated elevator feel system |
US3119583A (en) * | 1960-01-15 | 1964-01-28 | English Electric Co Ltd | Linkage in aircraft power control systems |
US9381998B2 (en) | 2009-10-19 | 2016-07-05 | Bae Systems Plc | Tactile cueing apparatus |
-
1951
- 1951-10-10 GB GB23593/51A patent/GB742383A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2912193A (en) * | 1955-08-23 | 1959-11-10 | Fairey Aviat Co Ltd | Aircraft controls |
US2955784A (en) * | 1956-02-27 | 1960-10-11 | Northrop Corp | Servo regulated elevator feel system |
US3119583A (en) * | 1960-01-15 | 1964-01-28 | English Electric Co Ltd | Linkage in aircraft power control systems |
US9381998B2 (en) | 2009-10-19 | 2016-07-05 | Bae Systems Plc | Tactile cueing apparatus |
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