JPS5743813B2 - - Google Patents

Info

Publication number
JPS5743813B2
JPS5743813B2 JP49017477A JP1747774A JPS5743813B2 JP S5743813 B2 JPS5743813 B2 JP S5743813B2 JP 49017477 A JP49017477 A JP 49017477A JP 1747774 A JP1747774 A JP 1747774A JP S5743813 B2 JPS5743813 B2 JP S5743813B2
Authority
JP
Japan
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
JP49017477A
Other languages
Japanese (ja)
Other versions
JPS49112014A (en:Method
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 JPS49112014A publication Critical patent/JPS49112014A/ja
Publication of JPS5743813B2 publication Critical patent/JPS5743813B2/ja
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • F23R3/08Arrangement 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)
JP49017477A 1973-02-12 1974-02-12 Expired JPS5743813B2 (en:Method)

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 (2)

Publication Number Publication Date
JPS49112014A JPS49112014A (en:Method) 1974-10-25
JPS5743813B2 true JPS5743813B2 (en:Method) 1982-09-17

Family

ID=23294307

Family Applications (1)

Application Number Title Priority Date Filing Date
JP49017477A Expired JPS5743813B2 (en:Method) 1973-02-12 1974-02-12

Country Status (8)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0182455U (en:Method) * 1987-11-18 1989-06-01

Families Citing this family (31)

* 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:Method) * 1977-09-12 1986-05-13
FR2450349A1 (fr) * 1979-03-01 1980-09-26 Snecma Perfectionnement au refroidissement des parois de chambres de combustion par pellicule d'air
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
FR2490728A1 (fr) * 1980-09-25 1982-03-26 Snecma Dispositif de refroidissement par film d'air pour tube a flamme de moteur a turbine a gaz
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 (de) * 1985-11-19 1987-05-21 Mtu Muenchen Gmbh Umkehrbrennkammer, insbesondere umkehrringbrennkammer, fuer gasturbinentriebwerke, mit mindestens einer flammrohrwandfilmkuehleinrichtung
FR2604509B1 (fr) * 1986-09-25 1988-11-18 Snecma Procede de realisation d'un film de refroidissement pour chambre de combustion de turbomachine, film ainsi realise et chambre de combustion le comportant
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 (ja) * 1995-02-06 1996-10-22 Toshiba Corp 燃焼器用ライナー及びその製造方法
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
EP3068975B1 (en) * 2013-11-11 2020-11-25 United Technologies Corporation Gas turbine engine component and corresponding methods of manufacturing
JP7393262B2 (ja) * 2020-03-23 2023-12-06 三菱重工業株式会社 燃焼器、及びこれを備えるガスタービン
JP7550694B2 (ja) * 2021-03-26 2024-09-13 本田技研工業株式会社 ガスタービン用燃焼器
CN117091157A (zh) 2022-05-13 2023-11-21 通用电气公司 用于耐用燃烧室衬里的板吊架结构
CN117091159A (zh) 2022-05-13 2023-11-21 通用电气公司 燃烧器衬里
CN117091158A (zh) 2022-05-13 2023-11-21 通用电气公司 燃烧器室网状结构
CN117091162A (zh) 2022-05-13 2023-11-21 通用电气公司 具有稀释孔结构的燃烧器
CN117091161A (zh) 2022-05-13 2023-11-21 通用电气公司 燃烧器衬里的中空板设计和结构

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 (de) * 1964-05-13 1968-06-20 Rolls Royce Kuehlvorrichtung fuer Brennkammern von Gasturbinentriebwerken
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 (de) * 1970-10-01 1972-10-31 Bbc Sulzer Turbomaschinen Brennkammer für eine Gasturbinenanlage
US3738106A (en) * 1971-10-26 1973-06-12 Avco Corp Variable geometry combustors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0182455U (en:Method) * 1987-11-18 1989-06-01

Also Published As

Publication number Publication date
DE2406277C2 (de) 1986-06-26
CA1004047A (en) 1977-01-25
BE810902A (fr) 1974-05-29
US3845620A (en) 1974-11-05
DE2406277A1 (de) 1974-08-15
FR2217548A1 (en:Method) 1974-09-06
GB1459500A (en) 1976-12-22
JPS49112014A (en:Method) 1974-10-25
FR2217548B1 (en:Method) 1980-11-21
IT1006333B (it) 1976-09-30

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