GB490572A - Improvements in or relating to automatic steering devices for vehicles, in particular aircraft - Google Patents
Improvements in or relating to automatic steering devices for vehicles, in particular aircraftInfo
- Publication number
- GB490572A GB490572A GB25488/37A GB2548837A GB490572A GB 490572 A GB490572 A GB 490572A GB 25488/37 A GB25488/37 A GB 25488/37A GB 2548837 A GB2548837 A GB 2548837A GB 490572 A GB490572 A GB 490572A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- lever
- rudder
- pressure
- cylinder
- 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
- 230000001419 dependent effect Effects 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
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)
- Power Steering Mechanism (AREA)
Abstract
490,572. Fluid-pressure servomotorcontrol systems. SIEMENS APPARATE UND MASCHINEN GES. Sept. 20, 1937, No. 25488. Convention date, Sept. 18, 1936. [Class 135] In automatic steering devices for vehicles, especially aircraft, in which the rudder or other steering member 20 is adjusted by a pneumatic or hydraulic servomotor 17 provided with return or follow - up mechanism 15, a pressure responsive member 22 which is subject to a pressure differential dependent upon the control force is interposed between the servomotor 17 and the mechanism 15. As shown, a floating lever 15 is linked to a control valve 16 and to a further floating lever 12 connected at one end to a gyroscopic turn indicator 2 and at the other end to a rotary magnet 10 connected to contacts 7, 8, 9 on a compass 1. The lever 15, instead of being directly connected to the piston-rod 19 so that the inclination of the rudder or the travel of the servomotor bears a linear relation to the steering impulse or the travel of the end of the lever 15, is connected to a piston 22 normally centralized by springs 23, 24 which may be inside or outside the cylinder 21. The deflection of the rudder is thereby increased so as to produce the necessary moment for righting the craft after the deviation which produced this rudder deflection. This is shown graphically in the Specification. The compass housing 6 is adjusted by a worm 5 on a shaft 4 which also operates an indicator 3. The piston and cylinder 22, 21 may be replaced by a bellows subject to the differential pressure on its opposite sides. An isodromic device consisting of a dashpot piston and cylinder may be interposed between the piston 22 and the lever 15. The resultant pressure acting on the piston 22 may alternatively be converted into an electrical valve for controlling the valve 16.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE490572X | 1936-09-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB490572A true GB490572A (en) | 1938-08-17 |
Family
ID=6544130
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25488/37A Expired GB490572A (en) | 1936-09-18 | 1937-09-20 | Improvements in or relating to automatic steering devices for vehicles, in particular aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB490572A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2773659A (en) * | 1952-04-19 | 1956-12-11 | Northrop Aircraft Inc | Full powered human pilot-autopilot airplane control system |
US2832305A (en) * | 1952-09-15 | 1958-04-29 | Muirhead & Co Ltd | Stabilization of ships |
-
1937
- 1937-09-20 GB GB25488/37A patent/GB490572A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2773659A (en) * | 1952-04-19 | 1956-12-11 | Northrop Aircraft Inc | Full powered human pilot-autopilot airplane control system |
US2832305A (en) * | 1952-09-15 | 1958-04-29 | Muirhead & Co Ltd | Stabilization of ships |
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