BE810902A - COMBUSTION CHAMBER COOLING SYSTEM - Google Patents

COMBUSTION CHAMBER COOLING SYSTEM

Info

Publication number
BE810902A
BE810902A BE140804A BE140804A BE810902A BE 810902 A BE810902 A BE 810902A BE 140804 A BE140804 A BE 140804A BE 140804 A BE140804 A BE 140804A BE 810902 A BE810902 A BE 810902A
Authority
BE
Belgium
Prior art keywords
combustion chamber
cooling system
chamber cooling
combustion
cooling
Prior art date
Application number
BE140804A
Other languages
French (fr)
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 filed Critical
Publication of BE810902A publication Critical patent/BE810902A/en

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
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections

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)
BE140804A 1973-02-12 1974-02-12 COMBUSTION CHAMBER COOLING SYSTEM BE810902A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00331519A US3845620A (en) 1973-02-12 1973-02-12 Cooling film promoter for combustion chambers

Publications (1)

Publication Number Publication Date
BE810902A true BE810902A (en) 1974-05-29

Family

ID=23294307

Family Applications (1)

Application Number Title Priority Date Filing Date
BE140804A BE810902A (en) 1973-02-12 1974-02-12 COMBUSTION CHAMBER COOLING SYSTEM

Country Status (8)

Country Link
US (1) US3845620A (en)
JP (1) JPS5743813B2 (en)
BE (1) BE810902A (en)
CA (1) CA1004047A (en)
DE (1) DE2406277C2 (en)
FR (1) FR2217548B1 (en)
GB (1) GB1459500A (en)
IT (1) IT1006333B (en)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3978662A (en) * 1975-04-28 1976-09-07 General Electric Company Cooling ring construction for combustion chambers
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure
US4184326A (en) * 1975-12-05 1980-01-22 United Technologies Corporation Louver construction for liner of gas turbine engine combustor
US4050241A (en) * 1975-12-22 1977-09-27 General Electric Company Stabilizing dimple for combustion liner cooling slot
JPS6115418Y2 (en) * 1977-09-12 1986-05-13
FR2450349A1 (en) * 1979-03-01 1980-09-26 Snecma IMPROVEMENT IN COOLING OF COMBUSTION CHAMBER WALLS BY AIR FILM
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
FR2490728A1 (en) * 1980-09-25 1982-03-26 Snecma AIR FILM COOLING DEVICE FOR FLAME TUBE OF GAS TURBINE ENGINE
US4380906A (en) * 1981-01-22 1983-04-26 United Technologies Corporation Combustion liner cooling scheme
US4485630A (en) * 1982-12-08 1984-12-04 General Electric Company Combustor liner
US4566280A (en) * 1983-03-23 1986-01-28 Burr Donald N Gas turbine engine combustor splash ring construction
DE3540942A1 (en) * 1985-11-19 1987-05-21 Mtu Muenchen Gmbh REVERSE COMBUSTION CHAMBER, ESPECIALLY REVERSE RING COMBUSTION CHAMBER, FOR GAS TURBINE ENGINES, WITH AT LEAST ONE FLAME TUBE FILM COOLING DEVICE
FR2604509B1 (en) * 1986-09-25 1988-11-18 Snecma PROCESS FOR PRODUCING A COOLING FILM FOR A TURBOMACHINE COMBUSTION CHAMBER, FILM THUS PRODUCED AND COMBUSTION CHAMBER COMPRISING SAME
US4896510A (en) * 1987-02-06 1990-01-30 General Electric Company Combustor liner cooling arrangement
US5651662A (en) * 1992-10-29 1997-07-29 General Electric Company Film cooled wall
US5363654A (en) * 1993-05-10 1994-11-15 General Electric Company Recuperative impingement cooling of jet engine components
JPH08278029A (en) * 1995-02-06 1996-10-22 Toshiba Corp Liner for combustor and manufacture thereof
US5680767A (en) * 1995-09-11 1997-10-28 General Electric Company Regenerative combustor cooling in a gas turbine engine
US6675582B2 (en) * 2001-05-23 2004-01-13 General Electric Company Slot cooled combustor line
US6554563B2 (en) * 2001-08-13 2003-04-29 General Electric Company Tangential flow baffle
US7007481B2 (en) * 2003-09-10 2006-03-07 General Electric Company Thick coated combustor liner
US9121609B2 (en) * 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10436039B2 (en) * 2013-11-11 2019-10-08 United Technologies Corporation Gas turbine engine turbine blade tip cooling
JP2022150946A (en) * 2021-03-26 2022-10-07 本田技研工業株式会社 Combustor for gas turbine
CN117091158A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor chamber mesh structure
CN117091159A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner
CN117091162A (en) 2022-05-13 2023-11-21 通用电气公司 Burner with dilution hole structure
CN117091161A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner hollow plate design and construction

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555965A (en) * 1950-03-24 1951-06-05 Gen Electric End cap for fluid fuel combustors
US2958194A (en) * 1951-09-24 1960-11-01 Power Jets Res & Dev Ltd Cooled flame tube
US3121996A (en) * 1961-10-02 1964-02-25 Lucas Industries Ltd Liquid fuel combustion apparatus
DE1270889B (en) * 1964-05-13 1968-06-20 Rolls Royce Cooling device for combustion chambers of gas turbine engines
US3369363A (en) * 1966-01-19 1968-02-20 Gen Electric Integral spacing rings for annular combustion chambers
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US3589128A (en) * 1970-02-02 1971-06-29 Avco Corp Cooling arrangement for a reverse flow gas turbine combustor
CH529916A (en) * 1970-10-01 1972-10-31 Bbc Sulzer Turbomaschinen Combustion chamber for a gas turbine plant
US3738106A (en) * 1971-10-26 1973-06-12 Avco Corp Variable geometry combustors

Also Published As

Publication number Publication date
FR2217548A1 (en) 1974-09-06
DE2406277C2 (en) 1986-06-26
GB1459500A (en) 1976-12-22
IT1006333B (en) 1976-09-30
JPS49112014A (en) 1974-10-25
CA1004047A (en) 1977-01-25
FR2217548B1 (en) 1980-11-21
DE2406277A1 (en) 1974-08-15
JPS5743813B2 (en) 1982-09-17
US3845620A (en) 1974-11-05

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