GB9005906D0 - Gas turbine engine fuel control system and regulating valve therefor - Google Patents

Gas turbine engine fuel control system and regulating valve therefor

Info

Publication number
GB9005906D0
GB9005906D0 GBGB9005906.4A GB9005906A GB9005906D0 GB 9005906 D0 GB9005906 D0 GB 9005906D0 GB 9005906 A GB9005906 A GB 9005906A GB 9005906 D0 GB9005906 D0 GB 9005906D0
Authority
GB
United Kingdom
Prior art keywords
control system
gas turbine
turbine engine
regulating valve
fuel control
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.)
Granted
Application number
GBGB9005906.4A
Other versions
GB2432886A (en
GB2432886B (en
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.)
Goodrich Control Systems
Original Assignee
Lucas Industries 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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB9005906A priority Critical patent/GB2432886B/en
Publication of GB9005906D0 publication Critical patent/GB9005906D0/en
Publication of GB2432886A publication Critical patent/GB2432886A/en
Application granted granted Critical
Publication of GB2432886B publication Critical patent/GB2432886B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F02C7/00—Features, 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
    • F02C7/22—Fuel supply systems
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
GB9005906A 1990-03-16 1990-03-16 Gas turbine engine fuel control system and regulating valve therefor Expired - Fee Related GB2432886B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9005906A GB2432886B (en) 1990-03-16 1990-03-16 Gas turbine engine fuel control system and regulating valve therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9005906A GB2432886B (en) 1990-03-16 1990-03-16 Gas turbine engine fuel control system and regulating valve therefor

Publications (3)

Publication Number Publication Date
GB9005906D0 true GB9005906D0 (en) 2006-09-20
GB2432886A GB2432886A (en) 2007-06-06
GB2432886B GB2432886B (en) 2007-12-05

Family

ID=37056385

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9005906A Expired - Fee Related GB2432886B (en) 1990-03-16 1990-03-16 Gas turbine engine fuel control system and regulating valve therefor

Country Status (1)

Country Link
GB (1) GB2432886B (en)

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB657213A (en) * 1948-03-02 1951-09-12 Westinghouse Electric Int Co Improvements in or relating to fuel supply systems for combustion apparatus
GB853706A (en) * 1955-08-11 1960-11-09 Lucas Industries Ltd Valves for controlling re-heat fuel supply systems for an aircraft gas turbine engine
DE1802275C2 (en) * 1968-10-10 1971-03-25 Motoren Turbinen Union Pressure holding and drainage valve of a gas turbine engine
US3591968A (en) * 1969-12-15 1971-07-13 Bendix Corp Afterburner fuel manifold quick fill and flow distribution apparatus
GB1293672A (en) * 1970-03-05 1972-10-18 Hobson Ltd H M Improvements in fuel supply systems for aircraft gas turbine jet engines
GB1423361A (en) * 1972-04-06 1976-02-04 Lucas Industries Ltd Priming valve arrangement for liquid fuel supply system
GB1423362A (en) * 1972-06-21 1976-02-04 Lucas Industries Ltd Fuel control apparatus for gas turbine engine reheat systems
GB1395690A (en) * 1973-12-18 1975-05-29 Dynair Ltd Thermally actuated control valves
FR2404113A1 (en) * 1977-09-23 1979-04-20 Snecma TURBOREACTOR REGULATION DEVICE
GB2014758B (en) * 1978-02-17 1982-07-14 Lucas Industries Ltd Fuel control for a gas turbine engine reheat system
EP0192037B1 (en) * 1985-02-21 1990-01-10 Lonza Ag Shut-off device, especially for high-pressure fluids, and use of the device
DE3543908C1 (en) * 1985-12-12 1987-01-29 Mtu Muenchen Gmbh Device for controlling the fuel supply to the afterburner of a bypass gas turbine jet engine
GB8607720D0 (en) * 1986-03-27 1986-04-30 Dowty Boulton Paul Ltd Servovalve

Also Published As

Publication number Publication date
GB2432886A (en) 2007-06-06
GB2432886B (en) 2007-12-05

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Legal Events

Date Code Title Description
COOA Change in applicant's name or ownership of the application

Owner name: GOODRICH CONTROL SYSTEMS LIMITED

Free format text: FORMER APPLICANT(S): LUCAS INDUSTRIES LIMITED ;

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20080305