JPS56168040A - Circular combustor for gas turbine engine - Google Patents

Circular combustor for gas turbine engine

Info

Publication number
JPS56168040A
JPS56168040A JP5045981A JP5045981A JPS56168040A JP S56168040 A JPS56168040 A JP S56168040A JP 5045981 A JP5045981 A JP 5045981A JP 5045981 A JP5045981 A JP 5045981A JP S56168040 A JPS56168040 A JP S56168040A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
circular combustor
combustor
circular
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.)
Granted
Application number
JP5045981A
Other languages
English (en)
Other versions
JPH0229938B2 (ja
Inventor
Ansonii Mashiyuuzu Jiyon
Aran Uotsushiyubaan Debuitsudo
Jiyosefu Saari Buitoo
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS56168040A publication Critical patent/JPS56168040A/ja
Publication of JPH0229938B2 publication Critical patent/JPH0229938B2/ja
Granted 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP5045981A 1980-04-02 1981-04-02 Circular combustor for gas turbine engine Granted JPS56168040A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/136,655 US4365470A (en) 1980-04-02 1980-04-02 Fuel nozzle guide and seal for a gas turbine engine

Publications (2)

Publication Number Publication Date
JPS56168040A true JPS56168040A (en) 1981-12-24
JPH0229938B2 JPH0229938B2 (ja) 1990-07-03

Family

ID=22473785

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5045981A Granted JPS56168040A (en) 1980-04-02 1981-04-02 Circular combustor for gas turbine engine

Country Status (6)

Country Link
US (1) US4365470A (ja)
JP (1) JPS56168040A (ja)
CA (1) CA1147565A (ja)
DE (1) DE3113381A1 (ja)
FR (1) FR2479952A1 (ja)
GB (1) GB2073398B (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005121352A (ja) * 2003-10-17 2005-05-12 General Electric Co <Ge> ガスタービンエンジン燃焼器をフィルム冷却するための方法及び装置
JP2020076564A (ja) * 2018-10-17 2020-05-21 マン・エナジー・ソリューションズ・エスイーＭａｎ Ｅｎｅｒｇｙ Ｓｏｌｕｔｉｏｎｓ Ｓｅ ガスタービン燃焼室

Families Citing this family (67)

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GB2114661B (en) * 1980-10-21 1984-08-01 Rolls Royce Casing structure for a gas turbine engine
US4454711A (en) * 1981-10-29 1984-06-19 Avco Corporation Self-aligning fuel nozzle assembly
GB2134243A (en) * 1983-01-27 1984-08-08 Rolls Royce Combustion equipment for a gas turbine engine
US4498617A (en) * 1983-03-31 1985-02-12 United Technologies Corporation Method for reshaping a gas turbine engine combustor part
US4870818A (en) * 1986-04-18 1989-10-03 United Technologies Corporation Fuel nozzle guide structure and retainer for a gas turbine engine
US4686823A (en) * 1986-04-28 1987-08-18 United Technologies Corporation Sliding joint for an annular combustor
GB2219653B (en) * 1987-12-18 1991-12-11 Rolls Royce Plc Improvements in or relating to combustors for gas turbine engines
US4914918A (en) * 1988-09-26 1990-04-10 United Technologies Corporation Combustor segmented deflector
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
FR2662784B1 (fr) * 1990-06-05 1992-08-14 Snecma Ensemble d'injection pour turbomachine, comprenant un bol de prevaporisation.
GB9018013D0 (en) * 1990-08-16 1990-10-03 Rolls Royce Plc Gas turbine engine combustor
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
FR2679010B1 (fr) * 1991-07-10 1993-09-24 Snecma Chambre de combustion de turbomachine a bols de prevaporisation demontables.
US5255508A (en) * 1991-11-01 1993-10-26 United Technologies Corporation Fuel nozzle assembly and method for making the assembly
CA2089272C (en) * 1992-03-23 2002-09-03 James Norman Reinhold, Jr. Impact resistant combustor
US5274991A (en) * 1992-03-30 1994-01-04 General Electric Company Dry low NOx multi-nozzle combustion liner cap assembly
US5463864A (en) * 1993-12-27 1995-11-07 United Technologies Corporation Fuel nozzle guide for a gas turbine engine combustor
GB2287310B (en) * 1994-03-01 1997-12-03 Rolls Royce Plc Gas turbine engine combustor heatshield
US5419115A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber
DE4432558A1 (de) * 1994-09-13 1996-03-14 Bmw Rolls Royce Gmbh Gasturbinen-Brennkammer mit Hitzeschild
US6032457A (en) * 1996-06-27 2000-03-07 United Technologies Corporation Fuel nozzle guide
US5916142A (en) * 1996-10-21 1999-06-29 General Electric Company Self-aligning swirler with ball joint
GB2355784B (en) * 1999-10-27 2004-05-05 Abb Alstom Power Uk Ltd Gas turbine
US6347508B1 (en) 2000-03-22 2002-02-19 Allison Advanced Development Company Combustor liner support and seal assembly
US6735950B1 (en) * 2000-03-31 2004-05-18 General Electric Company Combustor dome plate and method of making the same
US6792757B2 (en) * 2002-11-05 2004-09-21 Honeywell International Inc. Gas turbine combustor heat shield impingement cooling baffle
US6880341B2 (en) * 2002-12-18 2005-04-19 Pratt & Whitney Canada Corp. Low cost combustor floating collar with improved sealing and damping
US7093419B2 (en) * 2003-07-02 2006-08-22 General Electric Company Methods and apparatus for operating gas turbine engine combustors
US7134286B2 (en) * 2004-08-24 2006-11-14 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7140189B2 (en) * 2004-08-24 2006-11-28 Pratt & Whitney Canada Corp. Gas turbine floating collar
US7628019B2 (en) * 2005-03-21 2009-12-08 United Technologies Corporation Fuel injector bearing plate assembly and swirler assembly
US7617689B2 (en) * 2006-03-02 2009-11-17 Honeywell International Inc. Combustor dome assembly including retaining ring
US7827800B2 (en) * 2006-10-19 2010-11-09 Pratt & Whitney Canada Corp. Combustor heat shield
US7861530B2 (en) * 2007-03-30 2011-01-04 Pratt & Whitney Canada Corp. Combustor floating collar with louver
US7926280B2 (en) * 2007-05-16 2011-04-19 Pratt & Whitney Canada Corp. Interface between a combustor and fuel nozzle
US20090090110A1 (en) * 2007-10-04 2009-04-09 Honeywell International, Inc. Faceted dome assemblies for gas turbine engine combustors
US8266912B2 (en) * 2008-09-16 2012-09-18 General Electric Company Reusable weld joint for syngas fuel nozzles
US8863527B2 (en) * 2009-04-30 2014-10-21 Rolls-Royce Corporation Combustor liner
US8215115B2 (en) 2009-09-28 2012-07-10 Hamilton Sundstrand Corporation Combustor interface sealing arrangement
US8661823B2 (en) * 2010-01-05 2014-03-04 General Electric Company Integral flange connection fuel nozzle body for gas turbine
US8991188B2 (en) 2011-01-05 2015-03-31 General Electric Company Fuel nozzle passive purge cap flow
US9021675B2 (en) 2011-08-15 2015-05-05 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
US20130174562A1 (en) * 2012-01-11 2013-07-11 Marcus Timothy Holcomb Gas turbine engine, combustor and dome panel
US20130298564A1 (en) * 2012-05-14 2013-11-14 General Electric Company Cooling system and method for turbine system
US9175857B2 (en) * 2012-07-23 2015-11-03 General Electric Company Combustor cap assembly
US9097130B2 (en) * 2012-09-13 2015-08-04 General Electric Company Seal for use between injector and combustion chamber in gas turbine
EP3039340B1 (en) * 2013-08-30 2018-11-28 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
US10670272B2 (en) * 2014-12-11 2020-06-02 Raytheon Technologies Corporation Fuel injector guide(s) for a turbine engine combustor
US9810427B2 (en) * 2015-03-26 2017-11-07 Ansaldo Energia Switzerland AG Fuel nozzle with hemispherical dome air inlet
GB201515883D0 (en) 2015-09-08 2015-10-21 Rolls Royce Plc Cooling apparatus for a fuel injector
US10428736B2 (en) * 2016-02-25 2019-10-01 General Electric Company Combustor assembly
GB2548585B (en) * 2016-03-22 2020-05-27 Rolls Royce Plc A combustion chamber assembly
US10247106B2 (en) * 2016-06-15 2019-04-02 General Electric Company Method and system for rotating air seal with integral flexible heat shield
DE102016212649A1 (de) * 2016-07-12 2018-01-18 Rolls-Royce Deutschland Ltd & Co Kg Brennerdichtung einer Gasturbine und Verfahren zu deren Herstellung
GB201617369D0 (en) 2016-10-13 2016-11-30 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
US10724740B2 (en) * 2016-11-04 2020-07-28 General Electric Company Fuel nozzle assembly with impingement purge
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
US10634353B2 (en) 2017-01-12 2020-04-28 General Electric Company Fuel nozzle assembly with micro channel cooling
US10801726B2 (en) * 2017-09-21 2020-10-13 General Electric Company Combustor mixer purge cooling structure
US10330204B2 (en) 2017-11-10 2019-06-25 Rolls-Royce Deutschland Ltd & Co Kg Burner seal of a gas turbine and method for manufacturing the same
GB201802251D0 (en) 2018-02-12 2018-03-28 Rolls Royce Plc An air swirler arrangement for a fuel injector of a combustion chamber
US11125436B2 (en) 2019-07-03 2021-09-21 Pratt & Whitney Canada Corp. Combustor floating collar mounting arrangement
US11525577B2 (en) * 2020-04-27 2022-12-13 Raytheon Technologies Corporation Extended bulkhead panel
EP4177522B1 (en) * 2021-11-04 2024-06-26 Rolls-Royce plc Combustor arrangement
CN114135901A (zh) * 2021-11-08 2022-03-04 中国航发四川燃气涡轮研究院 一种防烧蚀的火焰筒大孔射流套筒
GB202211589D0 (en) * 2022-08-09 2022-09-21 Rolls Royce Plc A combustor assembly

Family Cites Families (11)

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Publication number Priority date Publication date Assignee Title
US3032990A (en) * 1949-10-22 1962-05-08 Gen Electric Fuel nozzle for gas turbine engine
US2602292A (en) * 1951-03-31 1952-07-08 Gen Electric Fuel-air mixing device
US2840989A (en) * 1955-09-15 1958-07-01 Gen Electric End cap for combustor
GB826961A (en) * 1956-03-09 1960-01-27 Lucas Industries Ltd Liquid fuel combustion apparatus
US3372542A (en) * 1966-11-25 1968-03-12 United Aircraft Corp Annular burner for a gas turbine
US3721089A (en) * 1971-06-08 1973-03-20 United Aircraft Corp Crossover tube construction
US3742704A (en) * 1971-07-13 1973-07-03 Westinghouse Electric Corp Combustion chamber support structure
US3724207A (en) * 1971-08-05 1973-04-03 Gen Motors Corp Combustion apparatus
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
US3901446A (en) * 1974-05-09 1975-08-26 Us Air Force Induced vortex swirler
US4180974A (en) * 1977-10-31 1980-01-01 General Electric Company Combustor dome sleeve

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005121352A (ja) * 2003-10-17 2005-05-12 General Electric Co <Ge> ガスタービンエンジン燃焼器をフィルム冷却するための方法及び装置
JP4569952B2 (ja) * 2003-10-17 2010-10-27 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン燃焼器をフィルム冷却するための方法及び装置
JP2020076564A (ja) * 2018-10-17 2020-05-21 マン・エナジー・ソリューションズ・エスイーＭａｎ Ｅｎｅｒｇｙ Ｓｏｌｕｔｉｏｎｓ Ｓｅ ガスタービン燃焼室
US11592181B2 (en) 2018-10-17 2023-02-28 Man Energy Solutions Se Flow passages formed in a flame tube for a gas turbine combustor chamber

Also Published As

Publication number Publication date
GB2073398B (en) 1983-10-12
GB2073398A (en) 1981-10-14
US4365470A (en) 1982-12-28
CA1147565A (en) 1983-06-07
DE3113381A1 (de) 1982-04-22
JPH0229938B2 (ja) 1990-07-03
DE3113381C2 (ja) 1990-05-31
FR2479952B1 (ja) 1984-04-20
FR2479952A1 (fr) 1981-10-09

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