JPH0423170B2 - - Google Patents

Info

Publication number
JPH0423170B2
JPH0423170B2 JP56208254A JP20825481A JPH0423170B2 JP H0423170 B2 JPH0423170 B2 JP H0423170B2 JP 56208254 A JP56208254 A JP 56208254A JP 20825481 A JP20825481 A JP 20825481A JP H0423170 B2 JPH0423170 B2 JP H0423170B2
Authority
JP
Japan
Prior art keywords
liner assembly
finger
downstream
outer shell
insert
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 - Lifetime
Application number
JP56208254A
Other languages
English (en)
Japanese (ja)
Other versions
JPS57136028A (en
Inventor
Josefu Deiin Girubaato
Haudon Howaito Rooren
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JPS57136028A publication Critical patent/JPS57136028A/ja
Publication of JPH0423170B2 publication Critical patent/JPH0423170B2/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers

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)
  • Gasket Seals (AREA)
JP56208254A 1980-12-29 1981-12-24 Liner assambly Granted JPS57136028A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/220,272 US4413477A (en) 1980-12-29 1980-12-29 Liner assembly for gas turbine combustor

Publications (2)

Publication Number Publication Date
JPS57136028A JPS57136028A (en) 1982-08-21
JPH0423170B2 true JPH0423170B2 (en]) 1992-04-21

Family

ID=22822857

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56208254A Granted JPS57136028A (en) 1980-12-29 1981-12-24 Liner assambly

Country Status (2)

Country Link
US (1) US4413477A (en])
JP (1) JPS57136028A (en])

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4984429A (en) * 1986-11-25 1991-01-15 General Electric Company Impingement cooled liner for dry low NOx venturi combustor
JP2585751B2 (ja) * 1988-09-30 1997-02-26 株式会社日立製作所 ガスタービン燃焼装置
US5117636A (en) * 1990-02-05 1992-06-02 General Electric Company Low nox emission in gas turbine system
DE19649486A1 (de) * 1996-11-29 1998-06-04 Abb Research Ltd Brennkammer
EP1312865A1 (de) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Ringbrennkammer für eine Gasturbine
US6865892B2 (en) * 2002-12-17 2005-03-15 Power Systems Mfg, Llc Combustion chamber/venturi configuration and assembly method
DE10336432A1 (de) * 2003-08-08 2005-03-10 Alstom Technology Ltd Baden Gasturbine und zugehöriges Kühlverfahren
FR2871846B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Chambre de combustion en cmc de turbine a gaz supportee dans un carter metallique par des organes de liaison en cmc
US7389643B2 (en) * 2005-01-31 2008-06-24 General Electric Company Inboard radial dump venturi for combustion chamber of a gas turbine
FR2887615B1 (fr) * 2005-06-22 2007-08-31 Snecma Moteurs Sa Carenage circulaire de chambre de combustion de turbomachine
US7421842B2 (en) * 2005-07-18 2008-09-09 Siemens Power Generation, Inc. Turbine spring clip seal
FR2896575B1 (fr) * 2006-01-26 2013-01-18 Snecma Chambre de combustion annulaire d'une turbomachine
EP2005067B1 (en) * 2006-03-14 2016-05-04 United Technologies Corporation Crack resistant combustor
US8141370B2 (en) * 2006-08-08 2012-03-27 General Electric Company Methods and apparatus for radially compliant component mounting
US7665960B2 (en) * 2006-08-10 2010-02-23 United Technologies Corporation Turbine shroud thermal distortion control
US7775050B2 (en) * 2006-10-31 2010-08-17 General Electric Company Method and apparatus for reducing stresses induced to combustor assemblies
FR2914707B1 (fr) * 2007-04-05 2009-10-30 Snecma Propulsion Solide Sa Procede d'assemblage avec recouvrement de deux pieces ayant des coefficients de dilatation differents et assemblage ainsi obtenu
US20090053054A1 (en) * 2007-08-20 2009-02-26 General Electric Company LEAKAGE REDUCING VENTURI FOR DRY LOW NITRIC OXIDES (NOx) COMBUSTORS
US7594401B1 (en) * 2008-04-10 2009-09-29 General Electric Company Combustor seal having multiple cooling fluid pathways
US8096133B2 (en) * 2008-05-13 2012-01-17 General Electric Company Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface
US8104290B2 (en) * 2008-10-15 2012-01-31 Alstom Technology Ltd. Combustion liner damper
US7712314B1 (en) * 2009-01-21 2010-05-11 Gas Turbine Efficiency Sweden Ab Venturi cooling system
US20100192587A1 (en) * 2009-02-03 2010-08-05 William Kirk Hessler Combustor assembly for use in a gas turbine engine and method of assembling same
US8863527B2 (en) * 2009-04-30 2014-10-21 Rolls-Royce Corporation Combustor liner
US8770933B2 (en) 2010-09-10 2014-07-08 Honeywell International Inc. Turbine nozzle assemblies and methods for repairing turbine nozzle assemblies
EP3022419B1 (en) * 2013-07-16 2020-04-29 United Technologies Corporation Rounded edges for a panel of a combustor
US9759427B2 (en) * 2013-11-01 2017-09-12 General Electric Company Interface assembly for a combustor
JP6485942B2 (ja) * 2014-09-25 2019-03-20 三菱日立パワーシステムズ株式会社 燃焼器、ガスタービン
US10215418B2 (en) * 2014-10-13 2019-02-26 Ansaldo Energia Ip Uk Limited Sealing device for a gas turbine combustor
DE102015207760A1 (de) * 2015-04-28 2016-11-03 Siemens Aktiengesellschaft Heißgasführendes Gehäuse
US10119473B2 (en) 2015-05-20 2018-11-06 General Electric Company Component, gas turbine component and method of forming
CN116265810A (zh) * 2021-12-16 2023-06-20 通用电气公司 利用成形冷却栅栏的旋流器反稀释
US11747019B1 (en) 2022-09-02 2023-09-05 General Electric Company Aerodynamic combustor liner design for emissions reductions
US11788724B1 (en) 2022-09-02 2023-10-17 General Electric Company Acoustic damper for combustor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1420217A (en) * 1918-12-11 1922-06-20 Francis H Richards Expansion joint
US3175361A (en) * 1959-08-05 1965-03-30 Phillips Petroleum Co Turbojet engine and its operation
US3064425A (en) * 1959-10-05 1962-11-20 Gen Motors Corp Combustion liner
US3326041A (en) * 1965-04-14 1967-06-20 Zink Co John Apparatus for developing differential pressures in a conduit line
US3702058A (en) * 1971-01-13 1972-11-07 Westinghouse Electric Corp Double wall combustion chamber
US3938324A (en) * 1974-12-12 1976-02-17 General Motors Corporation Premix combustor with flow constricting baffle between combustion and dilution zones
US4006589A (en) * 1975-04-14 1977-02-08 Phillips Petroleum Company Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows

Also Published As

Publication number Publication date
US4413477A (en) 1983-11-08
JPS57136028A (en) 1982-08-21

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