GB1020131A - Combustion apparatus - Google Patents

Combustion apparatus

Info

Publication number
GB1020131A
GB1020131A GB3430762A GB3430762A GB1020131A GB 1020131 A GB1020131 A GB 1020131A GB 3430762 A GB3430762 A GB 3430762A GB 3430762 A GB3430762 A GB 3430762A GB 1020131 A GB1020131 A GB 1020131A
Authority
GB
United Kingdom
Prior art keywords
air
valve
vaporizer
compressor
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
GB3430762A
Inventor
John Stanley Clark
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph 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, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB3430762A priority Critical patent/GB1020131A/en
Publication of GB1020131A publication Critical patent/GB1020131A/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
    • 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
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel

Landscapes

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

Abstract

1,020,131. Vapour burners. JOSEPH LUCAS (INDUSTRIES) Ltd. Nov. 28, 1963 [Sept. 7, 1962], No. 34307/62. Heading F4T. [Also in Divisions F1 and G3] A gas turbine plant comprising a turbine driving a compressor supplying a combustion chamber discharging through the turbine to a heat-exchanger has a fuel vaporizer disposed in the combustion chamber and means for adjusting a valve through which air is supplied to the vaporizer so as to maintain the fuel to air ratio in the vaporizer substantially constant. A gas turbine engine comprises a turbine 13 driving a compressor 12 supplying air to a combustion chamber 10 feeding through the turbine 13 to a heat-exchanger 14. A subsidiary compressor 17 receiving air from compressor 12, or atmosphere, supplies air to vaporizer 11 through a valve 21. A servomotor 43 controls valve 21 in response to liquid fuel flow, i.e. pressure, to spray nozzle 34 sensed by device 25, so as to maintain the fuel to air ratio in the vaporizer 11 substantially constant. A diaphragm 28 in device 25 senses the air supply pressure and causes adjustment of valve 21 with changes in that pressure. Fuel is supplied to nozzle 34 by a variable swashplate pump 29 through a throttle valve 32. A device 36 adjusts the output of the pump 29 so as to maintain the pressure drop across throttle 32 constant. When valve 21 is not fully open part of the air from compressor 17 is passed back through duct 23.
GB3430762A 1962-09-07 1962-09-07 Combustion apparatus Expired GB1020131A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3430762A GB1020131A (en) 1962-09-07 1962-09-07 Combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3430762A GB1020131A (en) 1962-09-07 1962-09-07 Combustion apparatus

Publications (1)

Publication Number Publication Date
GB1020131A true GB1020131A (en) 1966-02-16

Family

ID=10364002

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3430762A Expired GB1020131A (en) 1962-09-07 1962-09-07 Combustion apparatus

Country Status (1)

Country Link
GB (1) GB1020131A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101761395A (en) * 2009-12-26 2010-06-30 姜文岐 Hot gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101761395A (en) * 2009-12-26 2010-06-30 姜文岐 Hot gas turbine

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