GB619251A - Improvements relating to combustion-equipment - Google Patents

Improvements relating to combustion-equipment

Info

Publication number
GB619251A
GB619251A GB3523046A GB3523046A GB619251A GB 619251 A GB619251 A GB 619251A GB 3523046 A GB3523046 A GB 3523046A GB 3523046 A GB3523046 A GB 3523046A GB 619251 A GB619251 A GB 619251A
Authority
GB
United Kingdom
Prior art keywords
baffle
air
combustion
annular
spray
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
GB3523046A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3523046A priority Critical patent/GB619251A/en
Publication of GB619251A publication Critical patent/GB619251A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

619,251. Combustion chambers for gas turbines. MORDELL, D. L. Nov. 27, 1946, No 35230. [Class 51 (i)] A fuel spray from a nozzle 15 induced by compressed air is directed up-stream and impinges on a baffle 13 which deflects it downstream. Combustion air enters the flame tube 11 around the edge of the baffle and past swirlproducing vanes 22. Combustion takes place in the outer down-stream current and preheats the spray on its way towards the baffle. Secondary air passes around the flame tube and through a perforated plate 25. Additional primary air inlets may be provided in the baffle. The flame tube may be omitted and the baffle extended towards the wall of the combustion chamber 10. The air is taken from the main compressor and further compressed in a pump 19. Or, the air may be taken from the compressor at a high velocity and its pressure raised in a diffuser. Fuel may be mixed with the air in the pump 19. With an annular combustion chamber, a circular arrangement of spray nozzles or an annular spray nozzle may be used in conjunction with an annular baffle. Or, an annular combustion chamber may house a circular assembly of flame tubes.
GB3523046A 1946-11-27 1946-11-27 Improvements relating to combustion-equipment Expired GB619251A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3523046A GB619251A (en) 1946-11-27 1946-11-27 Improvements relating to combustion-equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3523046A GB619251A (en) 1946-11-27 1946-11-27 Improvements relating to combustion-equipment

Publications (1)

Publication Number Publication Date
GB619251A true GB619251A (en) 1949-03-07

Family

ID=10375338

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3523046A Expired GB619251A (en) 1946-11-27 1946-11-27 Improvements relating to combustion-equipment

Country Status (1)

Country Link
GB (1) GB619251A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807316A (en) * 1953-06-11 1957-09-24 Lucas Industries Ltd Liquid fuel combustion chambers for jet-propulsion engines, gas turbines, or other purposes
US2825205A (en) * 1953-07-15 1958-03-04 Snecma Combustion devices especially suitable for gas turbine engines and propulsion units for aircraft
US2938344A (en) * 1957-05-22 1960-05-31 United Aircraft Corp Aerodynamic flameholder
US2946510A (en) * 1954-08-04 1960-07-26 Hi Ro Heating Corp High temperature conduit radiant overhead heating
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
US2999358A (en) * 1957-10-21 1961-09-12 Sundstrand Corp Reaction chamber for monopropellant or bipropellant fuels
US3007310A (en) * 1955-05-25 1961-11-07 Daimler Benz Ag Combustion chamber with vorticity of the combustible mixture
US3046731A (en) * 1955-10-07 1962-07-31 Edward Pohlmann Flame stabilization in jet engines
US4466250A (en) * 1981-02-03 1984-08-21 Nissan Motor Company, Limited Air passageway to air injection valve for gas turbine engine
WO1999064791A1 (en) * 1998-06-08 1999-12-16 Solar Turbines Incorporated Combustor cooling method

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807316A (en) * 1953-06-11 1957-09-24 Lucas Industries Ltd Liquid fuel combustion chambers for jet-propulsion engines, gas turbines, or other purposes
US2825205A (en) * 1953-07-15 1958-03-04 Snecma Combustion devices especially suitable for gas turbine engines and propulsion units for aircraft
US2946510A (en) * 1954-08-04 1960-07-26 Hi Ro Heating Corp High temperature conduit radiant overhead heating
US3007310A (en) * 1955-05-25 1961-11-07 Daimler Benz Ag Combustion chamber with vorticity of the combustible mixture
US3046731A (en) * 1955-10-07 1962-07-31 Edward Pohlmann Flame stabilization in jet engines
US2938344A (en) * 1957-05-22 1960-05-31 United Aircraft Corp Aerodynamic flameholder
US2999358A (en) * 1957-10-21 1961-09-12 Sundstrand Corp Reaction chamber for monopropellant or bipropellant fuels
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
US4466250A (en) * 1981-02-03 1984-08-21 Nissan Motor Company, Limited Air passageway to air injection valve for gas turbine engine
WO1999064791A1 (en) * 1998-06-08 1999-12-16 Solar Turbines Incorporated Combustor cooling method
US6098397A (en) * 1998-06-08 2000-08-08 Caterpillar Inc. Combustor for a low-emissions gas turbine engine
JP2002517673A (en) * 1998-06-08 2002-06-18 ソウラー タービンズ インコーポレイテッド Combustor for low exhaust gas turbine engine

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