DE602004017813D1 - Gasturbinenbrennkammer auf einem Falz montiert - Google Patents

Gasturbinenbrennkammer auf einem Falz montiert

Info

Publication number
DE602004017813D1
DE602004017813D1 DE602004017813T DE602004017813T DE602004017813D1 DE 602004017813 D1 DE602004017813 D1 DE 602004017813D1 DE 602004017813 T DE602004017813 T DE 602004017813T DE 602004017813 T DE602004017813 T DE 602004017813T DE 602004017813 D1 DE602004017813 D1 DE 602004017813D1
Authority
DE
Germany
Prior art keywords
rebate
gas turbine
turbine combustor
combustor mounted
gas
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
DE602004017813T
Other languages
English (en)
Inventor
Stephen John Howell
John Carl Jacobson
Timothy Patrick Mccaffrey
Barry Francis Barnes
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 DE602004017813D1 publication Critical patent/DE602004017813D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/04—Supports for linings
    • 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
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602004017813T 2003-06-27 2004-04-27 Gasturbinenbrennkammer auf einem Falz montiert Expired - Lifetime DE602004017813D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/608,609 US7152411B2 (en) 2003-06-27 2003-06-27 Rabbet mounted combuster

Publications (1)

Publication Number Publication Date
DE602004017813D1 true DE602004017813D1 (de) 2009-01-02

Family

ID=33418732

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004017813T Expired - Lifetime DE602004017813D1 (de) 2003-06-27 2004-04-27 Gasturbinenbrennkammer auf einem Falz montiert

Country Status (5)

Country Link
US (1) US7152411B2 (de)
EP (1) EP1491823B1 (de)
CN (1) CN100565014C (de)
CA (1) CA2464563C (de)
DE (1) DE602004017813D1 (de)

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DE50212871D1 (de) * 2001-09-07 2008-11-20 Alstom Technology Ltd Dämpfungsanordnung zur reduzierung von brennkammerpulsationen in einer gasturbinenanlage
US7093440B2 (en) * 2003-06-11 2006-08-22 General Electric Company Floating liner combustor
US7093419B2 (en) 2003-07-02 2006-08-22 General Electric Company Methods and apparatus for operating gas turbine engine combustors
US7036316B2 (en) * 2003-10-17 2006-05-02 General Electric Company Methods and apparatus for cooling turbine engine combustor exit temperatures
US7082770B2 (en) * 2003-12-24 2006-08-01 Martling Vincent C Flow sleeve for a low NOx combustor
US20060231531A1 (en) * 2005-04-13 2006-10-19 General Electric Company Weld prep joint for electron beam or laser welding
EP1744016A1 (de) * 2005-07-11 2007-01-17 Siemens Aktiengesellschaft Heissgasführendes Gehäuseelement, Wellenschutzmantel und Gasturbinenanlage
US7559203B2 (en) * 2005-09-16 2009-07-14 Pratt & Whitney Canada Corp. Cooled support boss for a combustor in a gas turbine engine
FR2899314B1 (fr) * 2006-03-30 2008-05-09 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US8109098B2 (en) * 2006-05-04 2012-02-07 Siemens Energy, Inc. Combustor liner for gas turbine engine
US7765809B2 (en) * 2006-11-10 2010-08-03 General Electric Company Combustor dome and methods of assembling such
US8590313B2 (en) * 2008-07-30 2013-11-26 Rolls-Royce Corporation Precision counter-swirl combustor
US8266914B2 (en) * 2008-10-22 2012-09-18 Pratt & Whitney Canada Corp. Heat shield sealing for gas turbine engine combustor
US8863527B2 (en) * 2009-04-30 2014-10-21 Rolls-Royce Corporation Combustor liner
US8429916B2 (en) * 2009-11-23 2013-04-30 Honeywell International Inc. Dual walled combustors with improved liner seals
US8713945B2 (en) * 2010-06-29 2014-05-06 Nuovo Pignone S.P.A. Liner aft end support mechanisms and spring loaded liner stop mechanisms
US8844260B2 (en) * 2010-11-09 2014-09-30 Opra Technologies B.V. Low calorific fuel combustor for gas turbine
US9625153B2 (en) * 2010-11-09 2017-04-18 Opra Technologies B.V. Low calorific fuel combustor for gas turbine
US8899051B2 (en) 2010-12-30 2014-12-02 Rolls-Royce Corporation Gas turbine engine flange assembly including flow circuit
FR2976346B1 (fr) * 2011-06-08 2013-07-05 Turbomeca Chambre de combustion annulaire de turbomachine
US20130081397A1 (en) * 2011-10-04 2013-04-04 Brandon Taylor Overby Forward casing with a circumferential sloped surface and a combustor assembly including same
KR101613096B1 (ko) * 2011-10-24 2016-04-20 제네럴 일렉트릭 테크놀러지 게엠베하 가스 터빈
CN103486619B (zh) * 2012-06-13 2016-02-24 中国航空工业集团公司沈阳发动机设计研究所 一种火焰筒固定结构
WO2015038293A1 (en) * 2013-09-11 2015-03-19 United Technologies Corporation Combustor liner
US20160245518A1 (en) * 2013-10-04 2016-08-25 United Technologies Corporation Combustor panel with multiple attachments
US20150107256A1 (en) * 2013-10-17 2015-04-23 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9625158B2 (en) 2014-02-18 2017-04-18 Dresser-Rand Company Gas turbine combustion acoustic damping system
DE102014204466A1 (de) * 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
DE102014204481A1 (de) * 2014-03-11 2015-09-17 Rolls-Royce Deutschland Ltd & Co Kg Brennkammer einer Gasturbine
FR3022613B1 (fr) * 2014-06-24 2019-04-19 Safran Helicopter Engines Bossage pour chambre de combustion.
CN105003932A (zh) * 2015-07-10 2015-10-28 中国航空工业集团公司沈阳发动机设计研究所 一种重型燃气轮机旋流器安装结构
US10465907B2 (en) * 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
US10738646B2 (en) 2017-06-12 2020-08-11 Raytheon Technologies Corporation Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
US10612555B2 (en) 2017-06-16 2020-04-07 United Technologies Corporation Geared turbofan with overspeed protection
US11131458B2 (en) * 2018-04-10 2021-09-28 Delavan Inc. Fuel injectors for turbomachines
US11377970B2 (en) 2018-11-02 2022-07-05 Chromalloy Gas Turbine Llc System and method for providing compressed air to a gas turbine combustor
US11248797B2 (en) * 2018-11-02 2022-02-15 Chromalloy Gas Turbine Llc Axial stop configuration for a combustion liner
CN113719862B (zh) * 2021-09-10 2022-08-12 中国航发湖南动力机械研究所 回流燃烧室的分体式双层壁小弯管及与火焰筒搭接结构
CN114543116B (zh) * 2022-02-24 2023-04-21 江苏科技大学 一种海上石油快速收集燃烧利用装置
CN116928695A (zh) 2022-03-31 2023-10-24 通用电气公司 用于燃烧器的环形圆顶组件
CN117091158A (zh) 2022-05-13 2023-11-21 通用电气公司 燃烧器室网状结构
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
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
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
CN117091159A (zh) 2022-05-13 2023-11-21 通用电气公司 燃烧器衬里
CN117146296A (zh) * 2022-05-24 2023-12-01 通用电气公司 具有稀释冷却衬里的燃烧器

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US2548886A (en) * 1947-10-25 1951-04-17 Gen Electric Gas turbine power plant with axial flow compressor
US4912922A (en) * 1972-12-19 1990-04-03 General Electric Company Combustion chamber construction
US4785623A (en) * 1987-12-09 1988-11-22 United Technologies Corporation Combustor seal and support
FR2686683B1 (fr) * 1992-01-28 1994-04-01 Snecma Turbomachine a chambre de combustion demontable.
US5701733A (en) * 1995-12-22 1997-12-30 General Electric Company Double rabbet combustor mount
US6401447B1 (en) * 2000-11-08 2002-06-11 Allison Advanced Development Company Combustor apparatus for a gas turbine engine
JP3600911B2 (ja) * 2001-01-25 2004-12-15 川崎重工業株式会社 環状燃焼器のライナ支持構造
FR2825780B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Architecure de chambre de combustion de turbomachine en materiau a matrice ceramique
US6904757B2 (en) * 2002-12-20 2005-06-14 General Electric Company Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor
US6920762B2 (en) * 2003-01-14 2005-07-26 General Electric Company Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner
US6886343B2 (en) * 2003-01-15 2005-05-03 General Electric Company Methods and apparatus for controlling engine clearance closures
US6895757B2 (en) * 2003-02-10 2005-05-24 General Electric Company Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor
US7093440B2 (en) * 2003-06-11 2006-08-22 General Electric Company Floating liner combustor
US7093419B2 (en) * 2003-07-02 2006-08-22 General Electric Company Methods and apparatus for operating gas turbine engine combustors
US6955038B2 (en) * 2003-07-02 2005-10-18 General Electric Company Methods and apparatus for operating gas turbine engine combustors
US7036316B2 (en) * 2003-10-17 2006-05-02 General Electric Company Methods and apparatus for cooling turbine engine combustor exit temperatures
US7082765B2 (en) * 2004-09-01 2006-08-01 General Electric Company Methods and apparatus for reducing gas turbine engine emissions

Also Published As

Publication number Publication date
CA2464563A1 (en) 2004-12-27
EP1491823B1 (de) 2008-11-19
US20040261419A1 (en) 2004-12-30
CN100565014C (zh) 2009-12-02
CN1576699A (zh) 2005-02-09
EP1491823A1 (de) 2004-12-29
US7152411B2 (en) 2006-12-26
CA2464563C (en) 2009-10-20

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