GB1219909A - Hot gas generators - Google Patents

Hot gas generators

Info

Publication number
GB1219909A
GB1219909A GB43231/67A GB4323167A GB1219909A GB 1219909 A GB1219909 A GB 1219909A GB 43231/67 A GB43231/67 A GB 43231/67A GB 4323167 A GB4323167 A GB 4323167A GB 1219909 A GB1219909 A GB 1219909A
Authority
GB
United Kingdom
Prior art keywords
compressor
air
combustion
turbine
combustion chamber
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
GB43231/67A
Inventor
Eric Kellett
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.)
CAV Ltd
Original Assignee
CAV 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 CAV Ltd filed Critical CAV Ltd
Priority to GB43231/67A priority Critical patent/GB1219909A/en
Priority to US759691A priority patent/US3543511A/en
Priority to FR1580026D priority patent/FR1580026A/fr
Priority to DE6608297U priority patent/DE6608297U/en
Publication of GB1219909A publication Critical patent/GB1219909A/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
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

1,219,909. Gas turbine type gas generators. C.A.V. Ltd. Aug.28, 1968 [Sept.22, 1967], No.43231/67. Heading FIG. The invention relates to a combustion gas generator which comprises a combustion chamber, a turbine driven by gases from the combustion chamber, there being means for supplying combustion air, dilution air and fuel to the combustion chamber, such means comprising first and second compressors driven by the turbine, the first compressor supplying an air/fuel mixture to a burner disposed in the combustion chamber, and the second compressor supplying dilution air to the combustion chamber, there being means for controlling the quantity of air supplied by the second compressor. The gas generator shown comprises a shaft 11 on which are mounted a first compressor rotor 16, a second compressor rotor 17 and a turbine rotor 12, the first compressor having an inlet 22 to which fuel/air mixture is supplied, and an outlet 20 through which fuel/air mixture is delivered under pressure to a burner 29 disposed in a flame tube 28 of combustion equipment 24, while the second compressor has an inlet 23 and an outlet 21 through which dilution air is delivered to the combustion equipment, the air entering the flame tube through openings 30. Combustion gases from the combustion equipment are directed on to the turbine 12 the exhaust gases from which are passed to a point of use. A carburettor 33 is provided in the inlet line to the compressor 16. A throttle 35 is provided in the inlet line to the dilution air compressor 17, the throttle being controlled by a device 36 responsive to the pressure at the outlet of the first compressor 16.
GB43231/67A 1967-09-22 1967-09-22 Hot gas generators Expired GB1219909A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB43231/67A GB1219909A (en) 1967-09-22 1967-09-22 Hot gas generators
US759691A US3543511A (en) 1967-09-22 1968-09-13 Control arrangement for a hot gas generator
FR1580026D FR1580026A (en) 1967-09-22 1968-09-19
DE6608297U DE6608297U (en) 1967-09-22 1968-09-20 GENERATOR FOR GENERATING A HOT FUEL-AIR MIXTURE FOR GAS TURBINES.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB43231/67A GB1219909A (en) 1967-09-22 1967-09-22 Hot gas generators

Publications (1)

Publication Number Publication Date
GB1219909A true GB1219909A (en) 1971-01-20

Family

ID=10427838

Family Applications (1)

Application Number Title Priority Date Filing Date
GB43231/67A Expired GB1219909A (en) 1967-09-22 1967-09-22 Hot gas generators

Country Status (4)

Country Link
US (1) US3543511A (en)
DE (1) DE6608297U (en)
FR (1) FR1580026A (en)
GB (1) GB1219909A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3978658A (en) * 1972-03-21 1976-09-07 Westinghouse Canada Limited Variable load gas turbine
US5586429A (en) * 1994-12-19 1996-12-24 Northern Research & Engineering Corporation Brayton cycle industrial air compressor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2358815A (en) * 1935-03-28 1944-09-26 Jarvis C Marble Compressor apparatus
CH256077A (en) * 1942-02-26 1948-07-31 Jendrassik Georg Control process for gas turbine plants and equipment for carrying out the process.
US2616252A (en) * 1946-02-09 1952-11-04 Allis Chalmers Mfg Co Method of producing a gaseous motive fluid with pulverized fuel
US2595505A (en) * 1946-04-20 1952-05-06 Continental Aviat & Engineerin Coaxial combustion products generator, turbine, and compressor
FR1006102A (en) * 1947-10-25 1952-04-21 Method and control device for gas turbines
US2812637A (en) * 1951-12-21 1957-11-12 Phillips Petroleum Co Fuel air ratio regulation for combustion systems

Also Published As

Publication number Publication date
FR1580026A (en) 1969-08-29
US3543511A (en) 1970-12-01
DE6608297U (en) 1971-08-19

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