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 combustionturbines

Info

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
Application number
GB1337445A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
H M Hobson Aircraft & Motor Co
Original Assignee
H M Hobson Aircraft & Motor Co
Filing date
Publication date
Application filed by H M Hobson Aircraft & Motor Co filed Critical H M Hobson Aircraft & Motor Co
Publication of GB592769A publication Critical patent/GB592769A/en
Expired legal-status Critical Current

Links

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.
GB1337445A 1945-05-28 Improvements in servo motors applicable, for example, to fuel systems for combustionturbines Expired GB592769A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1002051A (en) Improvements relating to internal combustion engines
GB592769A (en) Improvements in servo motors applicable, for example, to fuel systems for combustionturbines
GB1425913A (en) Device for regulating the delivery of a fuel injection pump of an internal combustion engine
GB634095A (en) Fuel feed and power control system of device for gas turbines, jet engines and the like
GB845269A (en) Improvements in fuel flow control apparatus for gas turbine engines
GB614106A (en) Improvements in or relating to gas turbine plants
GB735159A (en) Improvements in or relating to fuel control systems for gas-turbine power plants
GB615517A (en) Improvements in or relating to fuel metering systems
GB861601A (en) Control mechanism for aircraft power plants comprising a gas turbine engine driving a propeller
GB870834A (en) Fuel system for gas turbine powerplants with torque limiting mechanism
GB644212A (en) Improvements in or relating to gas turbine fuel systems
GB636115A (en) Improvements in or relating to pressure controls for turbines
GB635196A (en) Improvements in or relating to fluid flow control systems
GB567392A (en) Improvements in or relating to fluid pressure speed governing systems
GB599640A (en) An improved charging air-pressure regulator for internal combustion engines
GB599106A (en) Improvements relating to pump controlling means applicable to fuel pumps for internal combustion prime movers
GB791062A (en) Improvements in or relating to gas turbine engine power plants
GB806207A (en) Improvements in or relating to governors, more particularly for gas turbine engines
GB585028A (en) Improvements in valves for internal combustion plant
GB1471658A (en) Priming valve for liquid fuel supply system
GB577914A (en) Improvements in pressure sensitive capsules
GB504170A (en) Improvements in or relating to control apparatus for internal combustion engines
GB572787A (en) Improvements relating to liquid fuel supply systems for internal combustion engines
GB785305A (en) Improvements relating to fuel systems of gas turbine engines
GB566323A (en) Improvements in regulating devices for controlling the supply of fuel to internal combustion engines