FR1231999A - Perfectionnements apportés aux dispositifs de combustion pour des installations motrices avec turbine à gaz - Google Patents

Perfectionnements apportés aux dispositifs de combustion pour des installations motrices avec turbine à gaz

Info

Publication number
FR1231999A
FR1231999A FR801600A FR801600A FR1231999A FR 1231999 A FR1231999 A FR 1231999A FR 801600 A FR801600 A FR 801600A FR 801600 A FR801600 A FR 801600A FR 1231999 A FR1231999 A FR 1231999A
Authority
FR
France
Prior art keywords
power plants
gas turbines
combustion devices
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
FR801600A
Other languages
English (en)
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 FR1231999A publication Critical patent/FR1231999A/fr
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • F23R3/02—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR801600A 1958-07-31 1959-07-30 Perfectionnements apportés aux dispositifs de combustion pour des installations motrices avec turbine à gaz Expired FR1231999A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24682/58A GB917704A (en) 1958-07-31 1958-07-31 Combustion apparatus

Publications (1)

Publication Number Publication Date
FR1231999A true FR1231999A (fr) 1960-10-04

Family

ID=10215618

Family Applications (1)

Application Number Title Priority Date Filing Date
FR801600A Expired FR1231999A (fr) 1958-07-31 1959-07-30 Perfectionnements apportés aux dispositifs de combustion pour des installations motrices avec turbine à gaz

Country Status (6)

Country Link
US (1) US3020718A (en:Method)
CH (1) CH373600A (en:Method)
DE (1) DE1179767B (en:Method)
FR (1) FR1231999A (en:Method)
GB (1) GB917704A (en:Method)
NL (1) NL108658C (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3826084A (en) * 1970-04-28 1974-07-30 United Aircraft Corp Turbine coolant flow system

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL252966A (en:Method) * 1959-06-23
GB2030653B (en) * 1978-10-02 1983-05-05 Gen Electric Gas turbine engine combustion gas temperature variation
US4733538A (en) * 1978-10-02 1988-03-29 General Electric Company Combustion selective temperature dilution
GB2089894B (en) * 1980-12-22 1985-08-14 Gen Electric Gas turbine engine air dispensing arrangement
US4416111A (en) * 1981-02-25 1983-11-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Air modulation apparatus
US5042256A (en) * 1986-07-28 1991-08-27 Teledyne Industries, Inc. Turbine shaft fuel pump
US5111655A (en) * 1989-12-22 1992-05-12 Sundstrand Corporation Single wall combustor assembly
US5323605A (en) * 1990-10-01 1994-06-28 General Electric Company Double dome arched combustor
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
FR2678714B1 (fr) * 1991-07-03 1993-09-17 Snecma Foyer de statoreacteur a pollution reduite.
US5239818A (en) * 1992-03-30 1993-08-31 General Electric Company Dilution pole combustor and method
US7036321B2 (en) * 2003-10-08 2006-05-02 Honeywell International, Inc. Auxiliary power unit having a rotary fuel slinger

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR785802A (fr) * 1935-02-18 1935-08-20 Brûleur à mazout et autre huile combustible
DE734101C (de) * 1941-06-26 1943-04-08 Maschf Augsburg Nuernberg Ag Brennkammer
DE847530C (de) * 1944-11-17 1952-08-25 Hellmut Weinrich Ringfoermige Brennkammer, insbesondere fuer Gasturbinen
US2720750A (en) * 1947-11-04 1955-10-18 Helmut R Schelp Revolving fuel injection system for jet engines and gas turbines
US2547959A (en) * 1948-01-27 1951-04-10 Westinghouse Electric Corp Centrifugal fuel feeding system for annular combustion chambers
FR1011066A (fr) * 1948-11-30 1952-06-18 Chambre de combustion
US2689457A (en) * 1949-03-15 1954-09-21 Hermann Oestrich Burner, particularly for gas turbines
BE507258A (en:Method) * 1950-12-02
DE959695C (de) * 1955-06-28 1957-03-07 Bmw Studiengesellschaft Fuer T Gasturbine mit Rotationszerstaeubung
DE1013467B (de) * 1955-07-30 1957-08-08 Daimler Benz Ag Brennkammer fuer Gasturbinen und Strahltriebwerke mit Zerstaeubungseinrichtung
BE560443A (en:Method) * 1956-09-01

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3826084A (en) * 1970-04-28 1974-07-30 United Aircraft Corp Turbine coolant flow system

Also Published As

Publication number Publication date
GB917704A (en) 1963-02-06
CH373600A (de) 1963-11-30
DE1179767B (de) 1964-10-15
NL108658C (en:Method)
US3020718A (en) 1962-02-13

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