DE2329367C2 - Brennkammer für Gasturbine - Google Patents

Brennkammer für Gasturbine

Info

Publication number
DE2329367C2
DE2329367C2 DE2329367A DE2329367A DE2329367C2 DE 2329367 C2 DE2329367 C2 DE 2329367C2 DE 2329367 A DE2329367 A DE 2329367A DE 2329367 A DE2329367 A DE 2329367A DE 2329367 C2 DE2329367 C2 DE 2329367C2
Authority
DE
Germany
Prior art keywords
flame tube
wall
air
combustion chamber
openings
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
DE2329367A
Other languages
German (de)
English (en)
Other versions
DE2329367A1 (de
Inventor
George Edward Clitheroe Lancashire Bunn
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries 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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of DE2329367A1 publication Critical patent/DE2329367A1/de
Application granted granted Critical
Publication of DE2329367C2 publication Critical patent/DE2329367C2/de
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)
DE2329367A 1972-06-09 1973-06-08 Brennkammer für Gasturbine Expired DE2329367C2 (de)

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
DE2329367A1 DE2329367A1 (de) 1973-12-20
DE2329367C2 true DE2329367C2 (de) 1981-12-24

Family

ID=10255088

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2329367A Expired DE2329367C2 (de) 1972-06-09 1973-06-08 Brennkammer für Gasturbine

Country Status (6)

Country Link
US (1) US3869864A (US06373033-20020416-M00071.png)
JP (1) JPS5411844B2 (US06373033-20020416-M00071.png)
DE (1) DE2329367C2 (US06373033-20020416-M00071.png)
FR (1) FR2188055B1 (US06373033-20020416-M00071.png)
GB (1) GB1424197A (US06373033-20020416-M00071.png)
IT (1) IT989653B (US06373033-20020416-M00071.png)

Families Citing this family (35)

* 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 (US06373033-20020416-M00071.png) * 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 (US06373033-20020416-M00071.png) * 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
US11674445B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for continuous ignition devices
US11674446B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for surface ignitors in torch ignition devices
US20230296250A1 (en) * 2022-03-21 2023-09-21 General Electric Company Turbine engine combustor and combustor liner

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 (US06373033-20020416-M00071.png) * 1950-12-02
US3333414A (en) * 1965-10-13 1967-08-01 United Aircraft Canada Aerodynamic-flow reverser and smoother
GB1289523A (US06373033-20020416-M00071.png) * 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
GB1424197A (en) 1976-02-11
JPS5411844B2 (US06373033-20020416-M00071.png) 1979-05-18
FR2188055B1 (US06373033-20020416-M00071.png) 1976-09-17
US3869864A (en) 1975-03-11
FR2188055A1 (US06373033-20020416-M00071.png) 1974-01-18
IT989653B (it) 1975-06-10
DE2329367A1 (de) 1973-12-20
JPS4949012A (US06373033-20020416-M00071.png) 1974-05-13

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Legal Events

Date Code Title Description
D2 Grant after examination
8339 Ceased/non-payment of the annual fee