RU2597350C2 - Газотурбинный двигатель, внутренняя оболочка камеры сгорания для газотурбинного двигателя и роторный кожух для газотурбинного двигателя - Google Patents

Газотурбинный двигатель, внутренняя оболочка камеры сгорания для газотурбинного двигателя и роторный кожух для газотурбинного двигателя Download PDF

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Publication number
RU2597350C2
RU2597350C2 RU2014120759/06A RU2014120759A RU2597350C2 RU 2597350 C2 RU2597350 C2 RU 2597350C2 RU 2014120759/06 A RU2014120759/06 A RU 2014120759/06A RU 2014120759 A RU2014120759 A RU 2014120759A RU 2597350 C2 RU2597350 C2 RU 2597350C2
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RU
Russia
Prior art keywords
gas turbine
turbine engine
combustion chamber
conical
shell
Prior art date
Application number
RU2014120759/06A
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English (en)
Russian (ru)
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RU2014120759A (ru
Inventor
Ремиги ШУОР
Синиша НАРАНЧИЧ
Гюнтер ФИЛЬКОРН
Original Assignee
Дженерал Электрик Текнолоджи Гмбх
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Application filed by Дженерал Электрик Текнолоджи Гмбх filed Critical Дженерал Электрик Текнолоджи Гмбх
Publication of RU2014120759A publication Critical patent/RU2014120759A/ru
Application granted granted Critical
Publication of RU2597350C2 publication Critical patent/RU2597350C2/ru

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
RU2014120759/06A 2011-10-24 2012-10-23 Газотурбинный двигатель, внутренняя оболочка камеры сгорания для газотурбинного двигателя и роторный кожух для газотурбинного двигателя RU2597350C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP11186387 2011-10-24
EP11186387.4 2011-10-24
PCT/EP2012/070930 WO2013060663A2 (de) 2011-10-24 2012-10-23 Gasturbine

Publications (2)

Publication Number Publication Date
RU2014120759A RU2014120759A (ru) 2015-12-10
RU2597350C2 true RU2597350C2 (ru) 2016-09-10

Family

ID=47045047

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014120759/06A RU2597350C2 (ru) 2011-10-24 2012-10-23 Газотурбинный двигатель, внутренняя оболочка камеры сгорания для газотурбинного двигателя и роторный кожух для газотурбинного двигателя

Country Status (7)

Country Link
US (1) US9708920B2 (OSRAM)
EP (1) EP2852735B1 (OSRAM)
KR (1) KR101613096B1 (OSRAM)
CN (1) CN104246373B (OSRAM)
IN (1) IN2014DN03773A (OSRAM)
RU (1) RU2597350C2 (OSRAM)
WO (1) WO2013060663A2 (OSRAM)

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ES2637944T3 (es) * 2014-06-06 2017-10-18 MTU Aero Engines AG Disposición de los componentes de una turbina de gas
EP2998517B1 (en) * 2014-09-16 2019-03-27 Ansaldo Energia Switzerland AG Sealing arrangement at the interface between a combustor and a turbine of a gas turbine and gas turbine with such a sealing arrangement
EP3287610B1 (en) * 2016-08-22 2019-07-10 Ansaldo Energia Switzerland AG Gas turbine transition duct
US10697634B2 (en) 2018-03-07 2020-06-30 General Electric Company Inner cooling shroud for transition zone of annular combustor liner
US12094625B2 (en) * 2019-09-24 2024-09-17 Ls Electric Co., Ltd. Cooling apparatus for superconductor cooling container
EP3835657A1 (en) 2019-12-10 2021-06-16 Siemens Aktiengesellschaft Combustion chamber with wall cooling
CN112377946B (zh) * 2020-11-16 2022-02-11 四川航天中天动力装备有限责任公司 一种轴向浮动式回流环形燃烧室大弯管结构
CN114542292B (zh) * 2022-02-22 2024-07-02 中国联合重型燃气轮机技术有限公司 一种缸体支撑装置

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US3186168A (en) * 1962-09-11 1965-06-01 Lucas Industries Ltd Means for supporting the downstream end of a combustion chamber in a gas turbine engine
US3670497A (en) * 1970-09-02 1972-06-20 United Aircraft Corp Combustion chamber support
WO2002027168A1 (en) * 2000-09-29 2002-04-04 Turbec Ab Suspension device
US6860108B2 (en) * 2003-01-22 2005-03-01 Mitsubishi Heavy Industries, Ltd. Gas turbine tail tube seal and gas turbine using the same
RU2275554C2 (ru) * 2000-06-16 2006-04-27 Нуово Пиньоне Холдинг С.П.А. Переходный элемент для некольцевых камер сгорания газовой турбины
US7082766B1 (en) * 2005-03-02 2006-08-01 General Electric Company One-piece can combustor

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US3670467A (en) 1970-04-27 1972-06-20 Robert H Walker Method and apparatus for manufacturing tumbling media
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WO2009103658A1 (de) * 2008-02-20 2009-08-27 Alstom Technology Ltd Gasturbine mit ringförmiger brennkammer
JP5134680B2 (ja) * 2008-02-27 2013-01-30 三菱重工業株式会社 ガスタービン及びガスタービンの車室開放方法
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US8347636B2 (en) * 2010-09-24 2013-01-08 General Electric Company Turbomachine including a ceramic matrix composite (CMC) bridge
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Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3186168A (en) * 1962-09-11 1965-06-01 Lucas Industries Ltd Means for supporting the downstream end of a combustion chamber in a gas turbine engine
US3670497A (en) * 1970-09-02 1972-06-20 United Aircraft Corp Combustion chamber support
RU2275554C2 (ru) * 2000-06-16 2006-04-27 Нуово Пиньоне Холдинг С.П.А. Переходный элемент для некольцевых камер сгорания газовой турбины
WO2002027168A1 (en) * 2000-09-29 2002-04-04 Turbec Ab Suspension device
US6860108B2 (en) * 2003-01-22 2005-03-01 Mitsubishi Heavy Industries, Ltd. Gas turbine tail tube seal and gas turbine using the same
US7082766B1 (en) * 2005-03-02 2006-08-01 General Electric Company One-piece can combustor

Also Published As

Publication number Publication date
CN104246373B (zh) 2016-06-08
KR20140077978A (ko) 2014-06-24
KR101613096B1 (ko) 2016-04-20
US20140223921A1 (en) 2014-08-14
EP2852735A2 (de) 2015-04-01
WO2013060663A3 (de) 2015-02-26
RU2014120759A (ru) 2015-12-10
EP2852735B1 (de) 2016-04-27
CN104246373A (zh) 2014-12-24
IN2014DN03773A (OSRAM) 2015-07-10
US9708920B2 (en) 2017-07-18
WO2013060663A2 (de) 2013-05-02

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