FR920910A - Improvements made to combustion devices, more especially to those in which gas streams circulate at high speed - Google Patents

Improvements made to combustion devices, more especially to those in which gas streams circulate at high speed

Info

Publication number
FR920910A
FR920910A FR920910DA FR920910A FR 920910 A FR920910 A FR 920910A FR 920910D A FR920910D A FR 920910DA FR 920910 A FR920910 A FR 920910A
Authority
FR
France
Prior art keywords
those
high speed
gas streams
improvements made
combustion devices
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
Other languages
French (fr)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR920910A publication Critical patent/FR920910A/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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR920910D 1945-02-01 1946-01-29 Improvements made to combustion devices, more especially to those in which gas streams circulate at high speed Expired FR920910A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB920910X 1945-02-01

Publications (1)

Publication Number Publication Date
FR920910A true FR920910A (en) 1947-04-22

Family

ID=10714639

Family Applications (1)

Application Number Title Priority Date Filing Date
FR920910D Expired FR920910A (en) 1945-02-01 1946-01-29 Improvements made to combustion devices, more especially to those in which gas streams circulate at high speed

Country Status (1)

Country Link
FR (1) FR920910A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2636553A (en) * 1949-11-08 1953-04-28 Rolls Royce Fuel system for gas turbine engines and the like with main and pilot fuel injectors
US2637972A (en) * 1948-04-09 1953-05-12 Mcdonnell Aircraft Corp Afterburner for turbojet engines and the like
US2659199A (en) * 1950-09-09 1953-11-17 William O Thompson Apparatus for avoiding hot starts in turbojet engine operation and for igniting fuel in the afterburner
US2679137A (en) * 1947-10-21 1954-05-25 Power Jets Res & Dev Ltd Apparatus for burning fuel in a fast moving gas stream
US2688840A (en) * 1947-12-29 1954-09-14 Phillips Petroleum Co Paraffin hydrocarbon fuel for and method of operating pulse jet engines
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US2697910A (en) * 1950-07-29 1954-12-28 Thermal Res And Engineering Co Fluid fuel burner with self-contained fuel vaporizing unit
US2698511A (en) * 1949-03-21 1955-01-04 Phillips Petroleum Co Method of operating turbojet engines
US2698513A (en) * 1947-12-29 1955-01-04 Phillips Petroleum Co Paraffin hydrocarbon fuel for and method of operating pulse-jet engines
US2705868A (en) * 1948-02-19 1955-04-12 Power Jets Res & Dev Ltd Combustion apparatus
US2708339A (en) * 1949-04-28 1955-05-17 Rolls Royce Combustion equipment for gas-turbine engine having main and pilot fuel injector means
US2720078A (en) * 1948-03-01 1955-10-11 Solar Aircraft Co Burner for use in high velocity ducts
US2725932A (en) * 1949-11-08 1955-12-06 Rolls Royce Fuel system for gas-turbine engines and the like
US2736166A (en) * 1956-02-28 Afterburning and exhaust nozzle
US2742755A (en) * 1949-11-14 1956-04-24 Rolls Royce Fuel system for pilot burners of gasturbine engines reheat equipment
US2881588A (en) * 1948-04-27 1959-04-14 Wilbur H Goss Injector and method for fuel injection
US3022630A (en) * 1948-04-29 1962-02-27 Sterling A Mccollum Pilot igniter for burners
EP0592223A1 (en) * 1992-10-07 1994-04-13 Westinghouse Electric Corporation Auto-ignition system and method for premixed gas turbine combustors
CH687780A5 (en) * 1993-04-08 1997-02-14 Asea Brown Boveri A method for operating a plant fired with houses on gaseous fuel combustor.

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736166A (en) * 1956-02-28 Afterburning and exhaust nozzle
US2679137A (en) * 1947-10-21 1954-05-25 Power Jets Res & Dev Ltd Apparatus for burning fuel in a fast moving gas stream
US2688840A (en) * 1947-12-29 1954-09-14 Phillips Petroleum Co Paraffin hydrocarbon fuel for and method of operating pulse jet engines
US2698513A (en) * 1947-12-29 1955-01-04 Phillips Petroleum Co Paraffin hydrocarbon fuel for and method of operating pulse-jet engines
US2705869A (en) * 1948-02-19 1955-04-12 Power Jets Res & Dev Ltd Combustion apparatus
US2705868A (en) * 1948-02-19 1955-04-12 Power Jets Res & Dev Ltd Combustion apparatus
US2720078A (en) * 1948-03-01 1955-10-11 Solar Aircraft Co Burner for use in high velocity ducts
US2637972A (en) * 1948-04-09 1953-05-12 Mcdonnell Aircraft Corp Afterburner for turbojet engines and the like
US2881588A (en) * 1948-04-27 1959-04-14 Wilbur H Goss Injector and method for fuel injection
US3022630A (en) * 1948-04-29 1962-02-27 Sterling A Mccollum Pilot igniter for burners
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US2698511A (en) * 1949-03-21 1955-01-04 Phillips Petroleum Co Method of operating turbojet engines
US2708339A (en) * 1949-04-28 1955-05-17 Rolls Royce Combustion equipment for gas-turbine engine having main and pilot fuel injector means
US2725932A (en) * 1949-11-08 1955-12-06 Rolls Royce Fuel system for gas-turbine engines and the like
US2636553A (en) * 1949-11-08 1953-04-28 Rolls Royce Fuel system for gas turbine engines and the like with main and pilot fuel injectors
US2742755A (en) * 1949-11-14 1956-04-24 Rolls Royce Fuel system for pilot burners of gasturbine engines reheat equipment
US2697910A (en) * 1950-07-29 1954-12-28 Thermal Res And Engineering Co Fluid fuel burner with self-contained fuel vaporizing unit
US2659199A (en) * 1950-09-09 1953-11-17 William O Thompson Apparatus for avoiding hot starts in turbojet engine operation and for igniting fuel in the afterburner
EP0592223A1 (en) * 1992-10-07 1994-04-13 Westinghouse Electric Corporation Auto-ignition system and method for premixed gas turbine combustors
CH687780A5 (en) * 1993-04-08 1997-02-14 Asea Brown Boveri A method for operating a plant fired with houses on gaseous fuel combustor.

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