GB585029A - Improvements in valves for internal combustion turbines - Google Patents

Improvements in valves for internal combustion turbines

Info

Publication number
GB585029A
GB585029A GB806343A GB806343A GB585029A GB 585029 A GB585029 A GB 585029A GB 806343 A GB806343 A GB 806343A GB 806343 A GB806343 A GB 806343A GB 585029 A GB585029 A GB 585029A
Authority
GB
United Kingdom
Prior art keywords
pressure
speed
valve
piston
delivery
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
GB806343A
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.)
GERALD WHITEHOUSE HIGGS WALKER
Metropolitan Vickers Electrical Co Ltd
Original Assignee
GERALD WHITEHOUSE HIGGS WALKER
Metropolitan Vickers Electrical Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by GERALD WHITEHOUSE HIGGS WALKER, Metropolitan Vickers Electrical Co Ltd filed Critical GERALD WHITEHOUSE HIGGS WALKER
Priority to GB806343A priority Critical patent/GB585029A/en
Publication of GB585029A publication Critical patent/GB585029A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Abstract

585,029. Gas turbines. ELDRED, R. J., WALKER, G. W. HIGGS-, and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. May 20, 1943, Nos. 8063 and 20739. [Class 110 (iii)] A control valve, for regulating fuel admission to a continuous combustion gas turbine during starting and running up to idling speed, comprises a piston valve 13 which opens ports G as it moves to the right. The whole delivery of the fuel pump passes through throttling passages B to a central space where a constant pressure is maintained by a relief valve. The pump used is of a type in which the delivery volume varies directly with the pump speed and accordingly the delivery pressure, obtaining in the spaces A, A<1>, varies with the speed. This pressure, applied to a piston 16 is opposed by a spring and moves the piston valve to the right as the speed increases. A single throttling orifice B may be used and when, as shown, other throttling orifices are uncovered as the speed increases, these are of such a size that the delivery pressure, as determined by the pressure-drop through the orifices, still increases with the pump speed. There is only a leakage flow out of the space A<1> and a fine filter is placed in front of that space. The device is also shown combined with a governor as described in Specification 585,032, [Group XXIX], and co-operating with a main fuel control valve as described in Specification 585,028, [Group XXIX]. The throttling orifice may be formed in the body of the piston valve or exterior to the valve casing and the operative pressure may be applied to one end of the piston valve which in such case is not formed with a piston 16.
GB806343A 1943-05-20 1943-05-20 Improvements in valves for internal combustion turbines Expired GB585029A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB806343A GB585029A (en) 1943-05-20 1943-05-20 Improvements in valves for internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB806343A GB585029A (en) 1943-05-20 1943-05-20 Improvements in valves for internal combustion turbines

Publications (1)

Publication Number Publication Date
GB585029A true GB585029A (en) 1947-01-29

Family

ID=9845067

Family Applications (1)

Application Number Title Priority Date Filing Date
GB806343A Expired GB585029A (en) 1943-05-20 1943-05-20 Improvements in valves for internal combustion turbines

Country Status (1)

Country Link
GB (1) GB585029A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941357A (en) * 1954-05-10 1960-06-21 Chrysler Corp Fuel control valve mechanism for use with a gas turbine power plant or the like
GB2510216A (en) * 2012-10-18 2014-07-30 Hamilton Sundstrand Corp A metering fluid flow valve

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941357A (en) * 1954-05-10 1960-06-21 Chrysler Corp Fuel control valve mechanism for use with a gas turbine power plant or the like
GB2510216A (en) * 2012-10-18 2014-07-30 Hamilton Sundstrand Corp A metering fluid flow valve
US9303563B2 (en) 2012-10-18 2016-04-05 Hamilton Sundstrand Corporation Modulating electric liquid metering valve with flow sensing
GB2510216B (en) * 2012-10-18 2019-12-25 Hamilton Sundstrand Corp Modulating electric liquid metering valve with flow sensing

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