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GB585032A - Improvements in governors for internal combustion turbines - Google Patents

Improvements in governors for internal combustion turbines

Info

Publication number
GB585032A
GB585032A GB2074043A GB2074043A GB585032A GB 585032 A GB585032 A GB 585032A GB 2074043 A GB2074043 A GB 2074043A GB 2074043 A GB2074043 A GB 2074043A GB 585032 A GB585032 A GB 585032A
Authority
GB
United Kingdom
Prior art keywords
openings
speed
piston
turbine
fuel
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
GB2074043A
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 GB2074043A priority Critical patent/GB585032A/en
Publication of GB585032A publication Critical patent/GB585032A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/263—Control of fuel supply by means of fuel metering valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Abstract

585,032. Fluid-pressure servomotors. ELDRED, R. J.; WALKER, G. W. HIGGS-, and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Dec. 10, 1943, No. 20740. [Class 135] A speed governor for an internal combustion turbine comprises a pump driven by the turbine and supplying fuel through main control valve openings 2 to the atomisers and pressures on each side of the openings 2 are applied to each side of a spring-loaded piston 10 that controls the by-pass openings 3 to allow excess fuel to return to the suction of the fuel pump. When the speed of the turbine falls, the pressure difference across the openings 2 is reduced and the piston 10 moves to close the by-pass openings 3 and opens a port 14 whereby fuel passing through the throttle 14a builds up pressure in the space 15 and causes the cylinder 12 to follow the movement of the piston so that a constant pressure difference is maintained across the openings 2 and the speed is maintained constant for varying load condi-. tions on the turbine. The speed at which the cylinder 12 follows the piston 10 is determined by the adjustment of the throttle .19. The speed at which the turbine is to be controlled is adjusted by varying the openings 2 by a lever 1 connected to a control valve 4. To raise the speed, the control valve is moved to the right and pressure difference across the piston 7 causes it to move to enlarge the openings 2. The rate of movement is controlled by the throttle 9 and the fuel displaced by the piston passes to the atomisers and assists the acceleration required. The governor may be used with.the starting valve described in Specification 585,029, [Group XXVI], controlling acceleration up to idling speed.
GB2074043A 1943-12-10 1943-12-10 Improvements in governors for internal combustion turbines Expired GB585032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2074043A GB585032A (en) 1943-12-10 1943-12-10 Improvements in governors for internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2074043A GB585032A (en) 1943-12-10 1943-12-10 Improvements in governors for internal combustion turbines

Publications (1)

Publication Number Publication Date
GB585032A true GB585032A (en) 1947-01-29

Family

ID=10150855

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2074043A Expired GB585032A (en) 1943-12-10 1943-12-10 Improvements in governors for internal combustion turbines

Country Status (1)

Country Link
GB (1) GB585032A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2926883A (en) * 1957-01-03 1960-03-01 John R Prybylski Shut-off valve
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
US2968347A (en) * 1956-09-21 1961-01-17 United Aircraft Corp Fuel control
US2995008A (en) * 1953-02-26 1961-08-08 Phillips Petroleum Co Fuel and oxidant control system and process for variable thrust rocket and jet engines
US3007514A (en) * 1957-12-30 1961-11-07 Bendix Corp Fluid control device
US3089306A (en) * 1958-12-11 1963-05-14 Power Jets Res & Dev Ltd Limitation of thermal shock in engine components
US3106934A (en) * 1958-12-24 1963-10-15 Bendix Corp Integrating and proportional flow control apparatus
US3110229A (en) * 1956-09-21 1963-11-12 United Aircraft Corp Time delay device
US3128783A (en) * 1957-02-11 1964-04-14 Holley Carburetor Co Bypass valve with limited reset
US3144074A (en) * 1960-08-22 1964-08-11 Gen Motors Corp Fuel control
US3173468A (en) * 1961-03-30 1965-03-16 Bendix Corp Fuel control for combustion engines
US3246682A (en) * 1961-03-30 1966-04-19 Bendix Corp Fuel control for combustion engines
US20120174587A1 (en) * 2009-09-23 2012-07-12 Turbomeca fuel flowmeter having an improved regulator device

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2995008A (en) * 1953-02-26 1961-08-08 Phillips Petroleum Co Fuel and oxidant control system and process for variable thrust rocket and jet engines
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
US2968347A (en) * 1956-09-21 1961-01-17 United Aircraft Corp Fuel control
US3110229A (en) * 1956-09-21 1963-11-12 United Aircraft Corp Time delay device
US2926883A (en) * 1957-01-03 1960-03-01 John R Prybylski Shut-off valve
US3128783A (en) * 1957-02-11 1964-04-14 Holley Carburetor Co Bypass valve with limited reset
US3007514A (en) * 1957-12-30 1961-11-07 Bendix Corp Fluid control device
US3089306A (en) * 1958-12-11 1963-05-14 Power Jets Res & Dev Ltd Limitation of thermal shock in engine components
US3106934A (en) * 1958-12-24 1963-10-15 Bendix Corp Integrating and proportional flow control apparatus
US3144074A (en) * 1960-08-22 1964-08-11 Gen Motors Corp Fuel control
US3173468A (en) * 1961-03-30 1965-03-16 Bendix Corp Fuel control for combustion engines
US3246682A (en) * 1961-03-30 1966-04-19 Bendix Corp Fuel control for combustion engines
US20120174587A1 (en) * 2009-09-23 2012-07-12 Turbomeca fuel flowmeter having an improved regulator device
US9239010B2 (en) * 2009-09-23 2016-01-19 Turbomeca Fuel flowmeter having an improved regulator device

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