EA200400201A1 - Вкладыш блока камеры сгорания газотурбинного двигателя - Google Patents

Вкладыш блока камеры сгорания газотурбинного двигателя

Info

Publication number
EA200400201A1
EA200400201A1 EA200400201A EA200400201A EA200400201A1 EA 200400201 A1 EA200400201 A1 EA 200400201A1 EA 200400201 A EA200400201 A EA 200400201A EA 200400201 A EA200400201 A EA 200400201A EA 200400201 A1 EA200400201 A1 EA 200400201A1
Authority
EA
Eurasian Patent Office
Prior art keywords
receiver
insert
gas turbine
combustion gas
turbine engine
Prior art date
Application number
EA200400201A
Other languages
English (en)
Inventor
Роберт Дж. Крэфт
Винсент С. Мартлинг
Брайан Р. Мэк
Марк А. Миннич
Original Assignee
Пауэ Системс Мфг., Ллс
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 Пауэ Системс Мфг., Ллс filed Critical Пауэ Системс Мфг., Ллс
Publication of EA200400201A1 publication Critical patent/EA200400201A1/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G3/00—Combustion-product positive-displacement engine plants
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • 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
    • F05B2220/00—Application
    • F05B2220/30—Application in turbines
    • F05B2220/302—Application in turbines in gas turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

Описан вкладыш блока камеры сгорания, предназначенный для снижения выбросов оксида азота (NOx). В этом вкладыше блока камеры сгорания используют кольцевой ресивер снаружи от оболочки вкладыша, который содержит предварительно подогретый охлаждающий воздух, вводимый в процесс горения. Воздушный ресивер может быть расширен для увеличения количества содержащегося в нем охлаждающего воздуха, что все еще позволяет устанавливать блок вкладыша в проточную трубу за счет использования выемок, которые позволяют локально уменьшать диаметр воздушного ресивера, что позволяет ресиверу проходить вдоль оси за установочные штифты вкладыша в блоке камеры сгорания.Отчет о международном поиске был опубликован 2003.04.17.
EA200400201A 2001-07-19 2002-04-25 Вкладыш блока камеры сгорания газотурбинного двигателя EA200400201A1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/909,029 US6430932B1 (en) 2001-07-19 2001-07-19 Low NOx combustion liner with cooling air plenum recesses
PCT/US2002/013032 WO2003008791A2 (en) 2001-07-19 2002-04-25 Low nox combustion liner with cooling air plenum recesses

Publications (1)

Publication Number Publication Date
EA200400201A1 true EA200400201A1 (ru) 2004-06-24

Family

ID=25426541

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200400201A EA200400201A1 (ru) 2001-07-19 2002-04-25 Вкладыш блока камеры сгорания газотурбинного двигателя

Country Status (13)

Country Link
US (1) US6430932B1 (ru)
EP (1) EP1415078A2 (ru)
JP (1) JP2004536273A (ru)
KR (1) KR20040018480A (ru)
BR (1) BR0211283A (ru)
CA (1) CA2454309A1 (ru)
CZ (1) CZ200493A3 (ru)
EA (1) EA200400201A1 (ru)
HU (1) HUP0401114A2 (ru)
IL (1) IL159938A0 (ru)
PL (1) PL366615A1 (ru)
SK (1) SK1042004A3 (ru)
WO (1) WO2003008791A2 (ru)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100831772B1 (ko) * 2001-11-30 2008-05-27 파워 시스템즈 엠에프지., 엘엘씨 질소산화물 저 배출 연소기용 연소 챔버/벤츄리 냉각장치및 방법
US7574865B2 (en) * 2004-11-18 2009-08-18 Siemens Energy, Inc. Combustor flow sleeve with optimized cooling and airflow distribution
US7389643B2 (en) * 2005-01-31 2008-06-24 General Electric Company Inboard radial dump venturi for combustion chamber of a gas turbine
US7716931B2 (en) * 2006-03-01 2010-05-18 General Electric Company Method and apparatus for assembling gas turbine engine
US8707704B2 (en) * 2007-05-31 2014-04-29 General Electric Company Method and apparatus for assembling turbine engines
US20090019854A1 (en) * 2007-07-16 2009-01-22 General Electric Company APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR
KR100890823B1 (ko) 2007-11-13 2009-03-30 한국기계연구원 가스터빈 시스템
US7712314B1 (en) 2009-01-21 2010-05-11 Gas Turbine Efficiency Sweden Ab Venturi cooling system
US8931280B2 (en) 2011-04-26 2015-01-13 General Electric Company Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
US8904802B2 (en) * 2011-06-30 2014-12-09 General Electric Company Turbomachine combustor assembly including a vortex modification system
US9181813B2 (en) 2012-07-05 2015-11-10 Siemens Aktiengesellschaft Air regulation for film cooling and emission control of combustion gas structure
AU2018229962B2 (en) * 2017-03-07 2023-02-16 8 Rivers Capital, Llc System and method for combustion of solid fuels and derivatives thereof
US11248797B2 (en) 2018-11-02 2022-02-15 Chromalloy Gas Turbine Llc Axial stop configuration for a combustion liner
EP3874129A4 (en) * 2018-11-02 2022-10-05 Chromalloy Gas Turbine LLC SYSTEM AND METHOD FOR SUPPLYING COMPRESSED AIR TO A GAS TURBINE COMBUSTOR
US11377970B2 (en) 2018-11-02 2022-07-05 Chromalloy Gas Turbine Llc System and method for providing compressed air to a gas turbine combustor
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

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2692478A (en) * 1951-02-24 1954-10-26 Boeing Co Turbine burner incorporating removable burner liner
US4292801A (en) 1979-07-11 1981-10-06 General Electric Company Dual stage-dual mode low nox combustor
US4984429A (en) 1986-11-25 1991-01-15 General Electric Company Impingement cooled liner for dry low NOx venturi combustor
US4982570A (en) 1986-11-25 1991-01-08 General Electric Company Premixed pilot nozzle for dry low Nox combustor
US5117636A (en) 1990-02-05 1992-06-02 General Electric Company Low nox emission in gas turbine system
US5233828A (en) 1990-11-15 1993-08-10 General Electric Company Combustor liner with circumferentially angled film cooling holes
US5181379A (en) 1990-11-15 1993-01-26 General Electric Company Gas turbine engine multi-hole film cooled combustor liner and method of manufacture
CA2056592A1 (en) 1990-12-21 1992-06-22 Phillip D. Napoli Multi-hole film cooled combustor liner with slotted film starter
US5307637A (en) 1992-07-09 1994-05-03 General Electric Company Angled multi-hole film cooled single wall combustor dome plate
US5282631A (en) 1992-09-22 1994-02-01 Baker Dorothee A Cross-word board game construction system and method
US5261223A (en) 1992-10-07 1993-11-16 General Electric Company Multi-hole film cooled combustor liner with rectangular film restarting holes
US5454221A (en) 1994-03-14 1995-10-03 General Electric Company Dilution flow sleeve for reducing emissions in a gas turbine combustor

Also Published As

Publication number Publication date
KR20040018480A (ko) 2004-03-03
CA2454309A1 (en) 2003-01-30
PL366615A1 (en) 2005-02-07
EP1415078A2 (en) 2004-05-06
SK1042004A3 (en) 2004-10-05
WO2003008791A3 (en) 2003-04-17
HUP0401114A2 (en) 2004-09-28
US6430932B1 (en) 2002-08-13
JP2004536273A (ja) 2004-12-02
CZ200493A3 (cs) 2004-05-12
BR0211283A (pt) 2004-08-03
IL159938A0 (en) 2004-06-20
WO2003008791A2 (en) 2003-01-30

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