GB586279A - Improvements in and relating to aircraft control devices - Google Patents
Improvements in and relating to aircraft control devicesInfo
- Publication number
- GB586279A GB586279A GB6789/43A GB678943A GB586279A GB 586279 A GB586279 A GB 586279A GB 6789/43 A GB6789/43 A GB 6789/43A GB 678943 A GB678943 A GB 678943A GB 586279 A GB586279 A GB 586279A
- Authority
- GB
- United Kingdom
- Prior art keywords
- servomotor
- rudder
- pipes
- aircraft
- april
- 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
- 238000011084 recovery Methods 0.000 abstract 1
- 201000009482 yaws Diseases 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Prostheses (AREA)
Abstract
586,279. Fluid-pressure servomotorcontrol systems. JACK & HEINTZ, Inc. April 29, 1943, No. 6789. Convention date, April 16, 1942. [Class 135] The aircraft control device described in Specification 572,201 is modified by the provision of an airspun horizon gyro 51 controlling, through an air relay 55, the valve 61 of a hydraulic servomotor 64 for aileron operation. This servomotor is connected with the rudder servomotor 24 by pipes connected to cylinders having spring-balanced pistons 72, 74. The pressures in the pipes 20, 21 connected to the servomotor 24 are communicated through pipes 69, 68 respectively to the pistons 72, 74 so that the operation of the rudder is accompanied by corresponding operation of the servomotor 64 and thus of the ailerons 1 which automatically aid recovery of the aircraft from violent yaws or, in making turns, assist the rudder by giving the aircraft the correct angle of bank.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US586279XA | 1942-04-16 | 1942-04-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB586279A true GB586279A (en) | 1947-03-13 |
Family
ID=22017975
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6789/43A Expired GB586279A (en) | 1942-04-16 | 1943-04-29 | Improvements in and relating to aircraft control devices |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB586279A (en) |
-
1943
- 1943-04-29 GB GB6789/43A patent/GB586279A/en not_active Expired
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