JPS5411844B2 - - Google Patents

Info

Publication number
JPS5411844B2
JPS5411844B2 JP6529173A JP6529173A JPS5411844B2 JP S5411844 B2 JPS5411844 B2 JP S5411844B2 JP 6529173 A JP6529173 A JP 6529173A JP 6529173 A JP6529173 A JP 6529173A JP S5411844 B2 JPS5411844 B2 JP S5411844B2
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
JP6529173A
Other languages
Japanese (ja)
Other versions
JPS4949012A (enrdf_load_stackoverflow
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 JPS4949012A publication Critical patent/JPS4949012A/ja
Publication of JPS5411844B2 publication Critical patent/JPS5411844B2/ja
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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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

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)
  • Gas Burners (AREA)
JP6529173A 1972-06-09 1973-06-09 Expired JPS5411844B2 (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2715472A GB1424197A (en) 1972-06-09 1972-06-09 Combustion chambers for gas turbine engines

Publications (2)

Publication Number Publication Date
JPS4949012A JPS4949012A (enrdf_load_stackoverflow) 1974-05-13
JPS5411844B2 true JPS5411844B2 (enrdf_load_stackoverflow) 1979-05-18

Family

ID=10255088

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6529173A Expired JPS5411844B2 (enrdf_load_stackoverflow) 1972-06-09 1973-06-09

Country Status (6)

Country Link
US (1) US3869864A (enrdf_load_stackoverflow)
JP (1) JPS5411844B2 (enrdf_load_stackoverflow)
DE (1) DE2329367C2 (enrdf_load_stackoverflow)
FR (1) FR2188055B1 (enrdf_load_stackoverflow)
GB (1) GB1424197A (enrdf_load_stackoverflow)
IT (1) IT989653B (enrdf_load_stackoverflow)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
JPS5638389Y2 (enrdf_load_stackoverflow) * 1976-12-09 1981-09-08
GB1571213A (en) * 1977-01-28 1980-07-09 Kainov G Combustion chamber for gas turbine engine
DE2723546A1 (de) * 1977-05-25 1978-11-30 Motoren Turbinen Union Brennkammer, insbesondere ringumkehrbrennkammer fuer gasturbinentriebwerke
DE2728399C2 (de) * 1977-06-24 1982-04-22 Brown, Boveri & Cie Ag, 6800 Mannheim Brennkammer für eine Gasturbine
US4195476A (en) * 1978-04-27 1980-04-01 General Motors Corporation Combustor construction
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
US4765136A (en) * 1985-11-25 1988-08-23 United Technologies Corporation Gas turbine engine augmentor
US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
US4944152A (en) * 1988-10-11 1990-07-31 Sundstrand Corporation Augmented turbine combustor cooling
US4949545A (en) * 1988-12-12 1990-08-21 Sundstrand Corporation Turbine wheel and nozzle cooling
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
JPH0387059U (enrdf_load_stackoverflow) * 1989-12-11 1991-09-04
US5069033A (en) * 1989-12-21 1991-12-03 Sundstrand Corporation Radial inflow combustor
US5113647A (en) * 1989-12-22 1992-05-19 Sundstrand Corporation Gas turbine annular combustor
US5165226A (en) * 1991-08-09 1992-11-24 Pratt & Whitney Canada, Inc. Single vortex combustor arrangement
US5237813A (en) * 1992-08-21 1993-08-24 Allied-Signal Inc. Annular combustor with outer transition liner cooling
US5271220A (en) * 1992-10-16 1993-12-21 Sundstrand Corporation Combustor heat shield for a turbine containment ring
US5746048A (en) * 1994-09-16 1998-05-05 Sundstrand Corporation Combustor for a gas turbine engine
US5628193A (en) * 1994-09-16 1997-05-13 Alliedsignal Inc. Combustor-to-turbine transition assembly
US6079199A (en) * 1998-06-03 2000-06-27 Pratt & Whitney Canada Inc. Double pass air impingement and air film cooling for gas turbine combustor walls
WO2001083963A1 (en) * 2000-05-01 2001-11-08 Elliott Energy Systems, Inc. Annular combustor for use with an energy system
US6405703B1 (en) 2001-06-29 2002-06-18 Brian Sowards Internal combustion engine
US6925810B2 (en) * 2002-11-08 2005-08-09 Honeywell International, Inc. Gas turbine engine transition liner assembly and repair
US7308794B2 (en) * 2004-08-27 2007-12-18 Pratt & Whitney Canada Corp. Combustor and method of improving manufacturing accuracy thereof
DE102005008421A1 (de) * 2005-02-24 2006-08-31 Alstom Technology Ltd. Verfahren zum Verbrennen eines Brennstoffs und zugehörige Brennkammer
JP2008536333A (ja) * 2005-04-13 2008-09-04 コーニング インコーポレイテッド 同調可能外部キャビティレーザのためのモード整合システム
US7954326B2 (en) * 2007-11-28 2011-06-07 Honeywell International Inc. Systems and methods for cooling gas turbine engine transition liners
US8640464B2 (en) 2009-02-23 2014-02-04 Williams International Co., L.L.C. Combustion system
US8864492B2 (en) * 2011-06-23 2014-10-21 United Technologies Corporation Reverse flow combustor duct attachment
US9879862B2 (en) * 2013-03-08 2018-01-30 Rolls-Royce North American Technologies, Inc. Gas turbine engine afterburner
US20150323185A1 (en) 2014-05-07 2015-11-12 General Electric Compamy Turbine engine and method of assembling thereof
US11674446B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for surface ignitors in torch ignition devices
US11674445B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for continuous ignition devices
US12222104B2 (en) * 2022-03-21 2025-02-11 General Electric Company Turbine engine combustor and combustor liner
US12298009B1 (en) * 2024-05-29 2025-05-13 General Electric Company Turbine engine having a reverse flow annular vortex combustor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
BE507258A (enrdf_load_stackoverflow) * 1950-12-02
US3333414A (en) * 1965-10-13 1967-08-01 United Aircraft Canada Aerodynamic-flow reverser and smoother
GB1289523A (enrdf_load_stackoverflow) * 1969-03-17 1972-09-20
US3613360A (en) * 1969-10-30 1971-10-19 Garrett Corp Combustion chamber construction
US3653207A (en) * 1970-07-08 1972-04-04 Gen Electric High fuel injection density combustion chamber for a gas turbine engine
US3671171A (en) * 1970-11-27 1972-06-20 Avco Corp Annular combustors

Also Published As

Publication number Publication date
US3869864A (en) 1975-03-11
DE2329367A1 (de) 1973-12-20
IT989653B (it) 1975-06-10
GB1424197A (en) 1976-02-11
FR2188055A1 (enrdf_load_stackoverflow) 1974-01-18
DE2329367C2 (de) 1981-12-24
JPS4949012A (enrdf_load_stackoverflow) 1974-05-13
FR2188055B1 (enrdf_load_stackoverflow) 1976-09-17

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