GB592769A - Improvements in servo motors applicable, for example, to fuel systems for combustionturbines - Google Patents
Improvements in servo motors applicable, for example, to fuel systems for combustionturbinesInfo
- Publication number
- GB592769A GB592769A GB1337445A GB1337445A GB592769A GB 592769 A GB592769 A GB 592769A GB 1337445 A GB1337445 A GB 1337445A GB 1337445 A GB1337445 A GB 1337445A GB 592769 A GB592769 A GB 592769A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pressure
- servo
- valve
- capsules
- piston
- 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
- 239000000446 fuel Substances 0.000 title abstract 3
- 239000002775 capsule Substances 0.000 abstract 2
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000006011 modification reaction Methods 0.000 abstract 1
Landscapes
- Hydraulic Motors (AREA)
- Fluid-Pressure Circuits (AREA)
- Actuator (AREA)
Abstract
592,769. Fluid-pressure servomotorcontrol systems. HOBSON (AIRCRAFT & MOTOR) COMPONENTS, Ltd., H. M., and GREENLAND, L. S. May 28, 1945, No. 13374. [Class 135] A hydraulic servomotor, suitable for controlling the fuel supply valve 12 of a combustion turbine engine, comprises a servo-member such as the piston 15 in a housing or cylinder 19 having a liquid pressure inlet conduit 20 and a return conduit 21 to the fuel pump 11, a restricted flow connection between the two ends of the housing, e.g. the aperture 22, a spring 23 for balancing the servo-member against the pressure difference acting thereon, a pressure or temperature responsive-device 16 for operating a valve 25 for controlling the flow through one of the conduits, and a follow-up lever 26 connecting the servo-member and the device 16. As shown, a stack of capsules 16 responsive to the air intake pressure in the pipe 18 operates the valve 25 in the return conduit. In modifications, the piston may be replaced by a vane and the capsules by a Bourdon tube connected to a thermometer bulb in the air intake. Specification 376,341 is referred to.
Publications (1)
Publication Number | Publication Date |
---|---|
GB592769A true GB592769A (en) | 1947-09-29 |
Family
ID=1727147
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1337445A Expired GB592769A (en) | 1945-05-28 | Improvements in servo motors applicable, for example, to fuel systems for combustionturbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB592769A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2667918A (en) * | 1947-05-03 | 1954-02-02 | Lucas Ltd Joseph | Means for effecting and controlling the supply of liquid fuel to prime movers |
US2700275A (en) * | 1948-12-21 | 1955-01-25 | Niles Bement Pond Co | Fuel control apparatus for turbojet engines |
US2718114A (en) * | 1953-11-17 | 1955-09-20 | Rolls Royce | Engine control system responsive to working fluid temperature and to atmospheric pressure |
US2725932A (en) * | 1949-11-08 | 1955-12-06 | Rolls Royce | Fuel system for gas-turbine engines and the like |
EP0056758A1 (en) * | 1981-01-19 | 1982-07-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Regulating device for a gas turbine liquid fuel supply system |
-
1945
- 1945-05-28 GB GB1337445A patent/GB592769A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2667918A (en) * | 1947-05-03 | 1954-02-02 | Lucas Ltd Joseph | Means for effecting and controlling the supply of liquid fuel to prime movers |
US2700275A (en) * | 1948-12-21 | 1955-01-25 | Niles Bement Pond Co | Fuel control apparatus for turbojet engines |
US2725932A (en) * | 1949-11-08 | 1955-12-06 | Rolls Royce | Fuel system for gas-turbine engines and the like |
US2718114A (en) * | 1953-11-17 | 1955-09-20 | Rolls Royce | Engine control system responsive to working fluid temperature and to atmospheric pressure |
EP0056758A1 (en) * | 1981-01-19 | 1982-07-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Regulating device for a gas turbine liquid fuel supply system |
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