FR1054402A - Perfectionnements aux moteurs à turbine à gaz - Google Patents

Perfectionnements aux moteurs à turbine à gaz

Info

Publication number
FR1054402A
FR1054402A FR1054402DA FR1054402A FR 1054402 A FR1054402 A FR 1054402A FR 1054402D A FR1054402D A FR 1054402DA FR 1054402 A FR1054402 A FR 1054402A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
gas
turbine
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
English (en)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1054402A publication Critical patent/FR1054402A/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
    • F23R3/02—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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F23R3/04—Air inlet arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1054402D 1951-02-14 1952-02-14 Perfectionnements aux moteurs à turbine à gaz Expired FR1054402A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3632/51A GB703002A (en) 1951-02-14 1951-02-14 Improvements in or relating to gas turbines

Publications (1)

Publication Number Publication Date
FR1054402A true FR1054402A (fr) 1954-02-10

Family

ID=9761977

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054402D Expired FR1054402A (fr) 1951-02-14 1952-02-14 Perfectionnements aux moteurs à turbine à gaz

Country Status (4)

Country Link
US (1) US2780060A (fr)
CH (1) CH325607A (fr)
FR (1) FR1054402A (fr)
GB (1) GB703002A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1198130B (de) * 1958-08-22 1965-08-05 Snecma Brenner fuer ringfoermige Brennkammern

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB780493A (en) * 1954-07-20 1957-08-07 Rolls Royce Improvements relating to combustion equipment for gas-turbine engines
BE540594A (fr) * 1954-08-18
DE1060667B (de) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Verbrennungseinrichtung fuer Gasturbinen
US3182453A (en) * 1956-03-26 1965-05-11 Power Jets Res & Dev Ltd Combustion system
US2997847A (en) * 1957-12-20 1961-08-29 Hollingsworth R Lee Combustion engines for rockets and aeroplanes
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
DE1108518B (de) * 1959-07-28 1961-06-08 Daimler Benz Ag Flammenhalter fuer Brennkammern von Gasturbinentriebwerken
US3999378A (en) * 1974-01-02 1976-12-28 General Electric Company Bypass augmentation burner arrangement for a gas turbine engine
US4199936A (en) * 1975-12-24 1980-04-29 The Boeing Company Gas turbine engine combustion noise suppressor
US4167097A (en) * 1977-09-09 1979-09-11 International Harvester Company Gas turbine engines with improved compressor-combustor interfaces
US4733538A (en) * 1978-10-02 1988-03-29 General Electric Company Combustion selective temperature dilution
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
US9482432B2 (en) * 2012-09-26 2016-11-01 United Technologies Corporation Gas turbine engine combustor with integrated combustor vane having swirler
US11067277B2 (en) * 2016-10-07 2021-07-20 General Electric Company Component assembly for a gas turbine engine
US11686210B2 (en) * 2021-03-24 2023-06-27 General Electric Company Component assembly for variable airfoil systems

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH210655A (de) * 1938-09-16 1940-07-31 Sulzer Ag Axial arbeitende Brennkraftturbine.
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like
US2563744A (en) * 1942-03-06 1951-08-07 Lockheed Aircraft Corp Gas turbine power plant having internal cooling means
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
BE463919A (fr) * 1943-11-05
US2592748A (en) * 1944-02-17 1952-04-15 Rateau Soc Annular combustion chamber with hollow air guide vanes with radial gasiform fuel slots for gas turbines
US2565308A (en) * 1945-01-17 1951-08-21 Research Corp Combustion chamber with conical air diffuser
US2625792A (en) * 1947-09-10 1953-01-20 Rolls Royce Flame tube having telescoping walls with fluted ends to admit air
US2603948A (en) * 1947-10-31 1952-07-22 Mims Lisso Stewart Multistage gas turbine blade cooling with air in high-pressure turbine stages
GB723015A (en) * 1952-01-17 1955-02-02 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine plant

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1198130B (de) * 1958-08-22 1965-08-05 Snecma Brenner fuer ringfoermige Brennkammern

Also Published As

Publication number Publication date
CH325607A (fr) 1957-11-15
US2780060A (en) 1957-02-05
GB703002A (en) 1954-01-27

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