GB644355A - Improvements in or relating to steering devices more particularly as used in aircraft - Google Patents
Improvements in or relating to steering devices more particularly as used in aircraftInfo
- Publication number
- GB644355A GB644355A GB26014/46A GB2601446A GB644355A GB 644355 A GB644355 A GB 644355A GB 26014/46 A GB26014/46 A GB 26014/46A GB 2601446 A GB2601446 A GB 2601446A GB 644355 A GB644355 A GB 644355A
- Authority
- GB
- United Kingdom
- Prior art keywords
- servomotor
- aircraft
- pilot
- rheostat
- speed
- 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
644,355. Controlling aircraft. SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU SUD-EST. Aug. 29, 1946, No. 26014. Convention date, Jan. 16. [Class 4] An aircraft control system, wherein manual operation of a relatively small control surface to give the pilot a sense of " feel " causes operation of an electric servomotor to operate a main control surface, is modified by controlling the speed of operation of the servomotor in accordance with the air pressure on the pilot surface to prevent too rapid operation of the motor. As shown, actuation of the primary member 40, of a follow-up switch, by the control lever 1, energizes relay 60 or 61 to drive the servomotor 7 in one direction or the other, the speed of operation being governed by a rheostat 55 controlled by a dynamometer system (not shown) measuring the stress applied to the pilot surface (not shown) by the control lever. In a modification, Fig. 5 (not shown) the followup switch controls the motor direct. The rheostat 55 may be operated in steps. Specification 25849/46, as open to inspection under Sect. 91, is referred to. The Specification as open to inspection under Sect. 91 states that the servomotor may be electric or hydraulic. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR644355X | 1946-01-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB644355A true GB644355A (en) | 1950-10-11 |
Family
ID=9000110
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB26014/46A Expired GB644355A (en) | 1946-01-16 | 1946-08-29 | Improvements in or relating to steering devices more particularly as used in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB644355A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2165706A (en) * | 1984-10-12 | 1986-04-16 | Dayle Rigby Smith | Alternating current sensor assembly and method of making same |
| US5418514A (en) * | 1984-10-12 | 1995-05-23 | Smith; Dayle R. | AC current sensor and method of making same |
| CN104527977A (en) * | 2014-12-30 | 2015-04-22 | 杨浩亮 | Dragon-head-shaped aircraft |
-
1946
- 1946-08-29 GB GB26014/46A patent/GB644355A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2165706A (en) * | 1984-10-12 | 1986-04-16 | Dayle Rigby Smith | Alternating current sensor assembly and method of making same |
| US5418514A (en) * | 1984-10-12 | 1995-05-23 | Smith; Dayle R. | AC current sensor and method of making same |
| CN104527977A (en) * | 2014-12-30 | 2015-04-22 | 杨浩亮 | Dragon-head-shaped aircraft |
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