CN104619956B - 具有径向扩散器和缩短中段的燃气涡轮发动机 - Google Patents

具有径向扩散器和缩短中段的燃气涡轮发动机 Download PDF

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Publication number
CN104619956B
CN104619956B CN201380046059.8A CN201380046059A CN104619956B CN 104619956 B CN104619956 B CN 104619956B CN 201380046059 A CN201380046059 A CN 201380046059A CN 104619956 B CN104619956 B CN 104619956B
Authority
CN
China
Prior art keywords
gas turbine
industrial gas
diffuser
compressed air
turbine engine
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 - Fee Related
Application number
CN201380046059.8A
Other languages
English (en)
Chinese (zh)
Other versions
CN104619956A (zh
Inventor
R.C.查伦
M.D.蒙哥马利
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.)
Siemens Energy Inc
Original Assignee
Siemens Energy Inc
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 Siemens Energy Inc filed Critical Siemens Energy Inc
Publication of CN104619956A publication Critical patent/CN104619956A/zh
Application granted granted Critical
Publication of CN104619956B publication Critical patent/CN104619956B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201380046059.8A 2012-09-04 2013-08-20 具有径向扩散器和缩短中段的燃气涡轮发动机 Expired - Fee Related CN104619956B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/602,422 US9127554B2 (en) 2012-09-04 2012-09-04 Gas turbine engine with radial diffuser and shortened mid section
US13/602,422 2012-09-04
PCT/US2013/055792 WO2014039247A1 (en) 2012-09-04 2013-08-20 Gas turbine engine with radial diffuser and shortened mid section

Publications (2)

Publication Number Publication Date
CN104619956A CN104619956A (zh) 2015-05-13
CN104619956B true CN104619956B (zh) 2017-06-09

Family

ID=49083791

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380046059.8A Expired - Fee Related CN104619956B (zh) 2012-09-04 2013-08-20 具有径向扩散器和缩短中段的燃气涡轮发动机

Country Status (8)

Country Link
US (1) US9127554B2 (enExample)
EP (1) EP2893152A1 (enExample)
JP (1) JP6258325B2 (enExample)
CN (1) CN104619956B (enExample)
IN (1) IN2015DN00897A (enExample)
RU (1) RU2631181C2 (enExample)
SA (1) SA515360106B1 (enExample)
WO (1) WO2014039247A1 (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130081407A1 (en) * 2011-10-04 2013-04-04 David J. Wiebe Aero-derivative gas turbine engine with an advanced transition duct combustion assembly
US20140060001A1 (en) * 2012-09-04 2014-03-06 Alexander R. Beeck Gas turbine engine with shortened mid section
JP6625427B2 (ja) * 2015-12-25 2019-12-25 川崎重工業株式会社 ガスタービンエンジン
US10145251B2 (en) 2016-03-24 2018-12-04 General Electric Company Transition duct assembly
US10260752B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10260424B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10227883B2 (en) 2016-03-24 2019-03-12 General Electric Company Transition duct assembly
US10260360B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly
US11021977B2 (en) * 2018-11-02 2021-06-01 Chromalloy Gas Turbine Llc Diffuser guide vane with deflector panel having curved profile
CN113518850B (zh) * 2018-11-30 2023-08-29 西门子能源全球两合公司 燃气涡轮发动机的中间框架区段和调节径向转子间隙的相应方法
EP3845740B1 (en) * 2019-12-31 2024-04-03 ANSALDO ENERGIA S.p.A. Gas turbine assembly

Citations (9)

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US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
US4896499A (en) * 1978-10-26 1990-01-30 Rice Ivan G Compression intercooled gas turbine combined cycle
US5252860A (en) * 1989-12-11 1993-10-12 Westinghouse Electric Corp. Gas turbine control system having maximum instantaneous load-pickup limiter
CN1112664A (zh) * 1993-12-15 1995-11-29 株式会社日立制作所 燃气涡轮燃烧室与燃气涡轮
CN1392331A (zh) * 2001-06-18 2003-01-22 西门子公司 带有空气压缩机的燃气轮机
CN101275750A (zh) * 2008-04-25 2008-10-01 北京航空航天大学 一种径向旋流器拐弯区直接喷射预混预蒸发低污染燃烧室
JP2008544211A (ja) * 2005-06-27 2008-12-04 シーメンス パワー ジェネレイション インコーポレイテッド タービンエンジンの第１段に接線方向の方向転換を生じさせる燃焼移行ダクト
CN101737801A (zh) * 2008-11-12 2010-06-16 通用电气公司 燃气轮机中的一体化的燃烧器和一级喷嘴以及方法
US20110203282A1 (en) * 2008-09-29 2011-08-25 Charron Richard C Assembly for directing combustion gas

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US3088279A (en) * 1960-08-26 1963-05-07 Gen Electric Radial flow gas turbine power plant
SU1311332A1 (ru) * 1984-03-01 1995-11-20 В.Е. Беляев Осарадиальный диффузор компрессора
KR940011861A (ko) * 1992-11-09 1994-06-22 한스 요트. 헤쩨르, 하아. 카이저 가스 터빈 연소실
US5737915A (en) 1996-02-09 1998-04-14 General Electric Co. Tri-passage diffuser for a gas turbine
US6796130B2 (en) * 2002-11-07 2004-09-28 Siemens Westinghouse Power Corporation Integrated combustor and nozzle for a gas turbine combustion system
RU2235921C1 (ru) * 2002-12-30 2004-09-10 Журавлев Юрий Иванович Напорный диффузор осевого компрессора
JP2005042973A (ja) * 2003-07-22 2005-02-17 Kawasaki Heavy Ind Ltd 旋回流型燃焼器を備えたガスタービン
US7870739B2 (en) * 2006-02-02 2011-01-18 Siemens Energy, Inc. Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions
US7600370B2 (en) * 2006-05-25 2009-10-13 Siemens Energy, Inc. Fluid flow distributor apparatus for gas turbine engine mid-frame section
JP5072278B2 (ja) * 2006-07-18 2012-11-14 三菱重工業株式会社 油圧着脱式カップリング
US7631499B2 (en) * 2006-08-03 2009-12-15 Siemens Energy, Inc. Axially staged combustion system for a gas turbine engine
US20090139199A1 (en) 2007-11-15 2009-06-04 General Electric Company Pulse detonation combustor valve for high temperature and high pressure operation
US8230688B2 (en) 2008-09-29 2012-07-31 Siemens Energy, Inc. Modular transvane assembly
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
US20140060001A1 (en) * 2012-09-04 2014-03-06 Alexander R. Beeck Gas turbine engine with shortened mid section

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
US4896499A (en) * 1978-10-26 1990-01-30 Rice Ivan G Compression intercooled gas turbine combined cycle
US4896499B1 (enExample) * 1978-10-26 1992-09-15 G Rice Ivan
US5252860A (en) * 1989-12-11 1993-10-12 Westinghouse Electric Corp. Gas turbine control system having maximum instantaneous load-pickup limiter
CN1112664A (zh) * 1993-12-15 1995-11-29 株式会社日立制作所 燃气涡轮燃烧室与燃气涡轮
CN1392331A (zh) * 2001-06-18 2003-01-22 西门子公司 带有空气压缩机的燃气轮机
JP2008544211A (ja) * 2005-06-27 2008-12-04 シーメンス パワー ジェネレイション インコーポレイテッド タービンエンジンの第１段に接線方向の方向転換を生じさせる燃焼移行ダクト
CN101275750A (zh) * 2008-04-25 2008-10-01 北京航空航天大学 一种径向旋流器拐弯区直接喷射预混预蒸发低污染燃烧室
US20110203282A1 (en) * 2008-09-29 2011-08-25 Charron Richard C Assembly for directing combustion gas
CN101737801A (zh) * 2008-11-12 2010-06-16 通用电气公司 燃气轮机中的一体化的燃烧器和一级喷嘴以及方法

Also Published As

Publication number Publication date
WO2014039247A1 (en) 2014-03-13
EP2893152A1 (en) 2015-07-15
RU2631181C2 (ru) 2017-09-19
US9127554B2 (en) 2015-09-08
IN2015DN00897A (enExample) 2015-06-12
RU2015107382A (ru) 2016-10-27
JP2015532699A (ja) 2015-11-12
SA515360106B1 (ar) 2016-06-16
CN104619956A (zh) 2015-05-13
JP6258325B2 (ja) 2018-01-10
US20140060000A1 (en) 2014-03-06

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Granted publication date: 20170609

Termination date: 20190820