GB587427A - Improvements in or relating to fluid-pressure servomotors - Google Patents
Improvements in or relating to fluid-pressure servomotorsInfo
- Publication number
- GB587427A GB587427A GB23230/44A GB2323044A GB587427A GB 587427 A GB587427 A GB 587427A GB 23230/44 A GB23230/44 A GB 23230/44A GB 2323044 A GB2323044 A GB 2323044A GB 587427 A GB587427 A GB 587427A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- vane
- pressure
- vanes
- fluid
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
- F15B9/02—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
- F15B9/08—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
- F15B9/10—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor in which the controlling element and the servomotor each controls a separate member, these members influencing different fluid passages or the same passage
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluid-Pressure Circuits (AREA)
- Servomotors (AREA)
Abstract
587,427. Fluid-pressure servomotorcontrol systems. STAUDE, E. G., and STAUDE, O. B. Nov. 22, 1944, No. 23230. Convention date, Dec. 8, 1943. [Class 135] A fluid-pressure servomotor comprises a pump 98, Fig. 3, normally circulating pressure liquid continuously through apertures in vanes 66, 67, which apertures can be closed by valves 74, 77 operable selectively to cause the pressure to build up behind a vane to move the latter. As applied to the actuation of an aircraft control surface, cables 1,2, Fig. 1, are connected to the pilot's control, and when moved to the left, for example, cause a lever 7 to swing anti-clockwise about its pivot 8 on a lever 10, the latter being connected through cables 14, 15 to the control surface. Besides swinging lever 7, the pull on cable 1 will also be transmitted directly throughpivot 8 to cable 14 and will cause the latter to start moving to the left. The lower end of lever 7 carries a tooth 31 engaging in a recess in a lever 33 keyed to a shaft 34 rotating in a sleeve 39 on which the lever 10 is keyed, and the anticlockwise movement of lever 7 will rotate lever 33 in a clockwise direction. The latter lever carries a see-saw lever 50 which will depress ball valve 77 to close the aperture in vane 67, and the pressure liquid from pump outlet passage 107 will build up behind the vane and move it in a clockwise direction. As the vanes are carried by sleeve 39, lever 10 will be rotated and will move cable 14 to the left. Movable vanes 66, 67 co-operate with fixed vanes 80, 81, and the liquid on the upper side of vane 67 will be forced through port 117, pipe 118, and port 119, through the aperture in vane 66 and out through port 87 and pipe 88 to the inlet passage 90 of the pump. The valves are re-centred by a spring-pressed lever 25 pivoted on lever 10 and engaging in a recess 28 in lever 7. The fluid pressure acting on the ball valves when the latter are closed will be transmitted to the pilot to give " feel." A relief valve 113 between the inlet and outlet passages of the pump permits the liquid to circulate freely when the lower supply fails and direct manual actuation of the control surface through lever 7 is required.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23230/44A GB587427A (en) | 1944-11-22 | 1944-11-22 | Improvements in or relating to fluid-pressure servomotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23230/44A GB587427A (en) | 1944-11-22 | 1944-11-22 | Improvements in or relating to fluid-pressure servomotors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB587427A true GB587427A (en) | 1947-04-24 |
Family
ID=22018661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23230/44A Expired GB587427A (en) | 1944-11-22 | 1944-11-22 | Improvements in or relating to fluid-pressure servomotors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB587427A (en) |
-
1944
- 1944-11-22 GB GB23230/44A patent/GB587427A/en not_active Expired
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