JP2004325069A - ガスタービンエンジンにおいて流体を噴射するための方法及び装置 - Google Patents

ガスタービンエンジンにおいて流体を噴射するための方法及び装置 Download PDF

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Publication number
JP2004325069A
JP2004325069A JP2004130561A JP2004130561A JP2004325069A JP 2004325069 A JP2004325069 A JP 2004325069A JP 2004130561 A JP2004130561 A JP 2004130561A JP 2004130561 A JP2004130561 A JP 2004130561A JP 2004325069 A JP2004325069 A JP 2004325069A
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JP
Japan
Prior art keywords
plenum
injector
nozzle support
passage
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.)
Pending
Application number
JP2004130561A
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English (en)
Japanese (ja)
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JP2004325069A5 (enExample
Inventor
Christopher James Wilusz
クリストファー・ジェームズ・ウィラス
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 JP2004325069A publication Critical patent/JP2004325069A/ja
Publication of JP2004325069A5 publication Critical patent/JP2004325069A5/ja
Pending legal-status Critical Current

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F23R3/045—Air inlet arrangements using pipes
    • 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

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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)
  • Nozzles (AREA)
JP2004130561A 2003-04-28 2004-04-27 ガスタービンエンジンにおいて流体を噴射するための方法及び装置 Pending JP2004325069A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/424,440 US7052231B2 (en) 2003-04-28 2003-04-28 Methods and apparatus for injecting fluids in gas turbine engines

Publications (2)

Publication Number Publication Date
JP2004325069A true JP2004325069A (ja) 2004-11-18
JP2004325069A5 JP2004325069A5 (enExample) 2007-06-14

Family

ID=32990347

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004130561A Pending JP2004325069A (ja) 2003-04-28 2004-04-27 ガスタービンエンジンにおいて流体を噴射するための方法及び装置

Country Status (4)

Country Link
US (1) US7052231B2 (enExample)
EP (1) EP1473518A3 (enExample)
JP (1) JP2004325069A (enExample)
CN (1) CN100507236C (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101774094B1 (ko) * 2011-08-22 2017-09-04 마제드 토칸 가스 터빈 엔진에서 사용되는 예비혼합형 접선방향 연료-공기 노즐을 가진 캔-애뉼러형 연소실
KR101774093B1 (ko) * 2011-08-22 2017-09-12 마제드 토칸 가스 터빈 엔진에서 사용되는 스테이지가 형성되고 접선방향으로 형성된 연료-공기 노즐을 가진 캔-애뉼러형 연소실
KR101774630B1 (ko) * 2011-08-22 2017-09-19 마제드 토칸 가스 터빈 엔진에 사용되는 예비혼합된 연료와 공기를 가진 접선방향의 애뉼러형 연소실
KR101832026B1 (ko) * 2011-08-22 2018-02-23 마제드 토칸 가스 터빈 엔진에 사용되는 접선방향의 무염 애뉼러형 연소실

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008015207A1 (de) * 2008-03-20 2009-09-24 Rolls-Royce Deutschland Ltd & Co Kg Fluid-Injektor-Düse
DE102008017844A1 (de) * 2008-04-08 2009-10-15 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit Fluid-Injektorbaugruppe
DE102010027587A1 (de) 2010-07-19 2012-01-19 Rolls-Royce Deutschland Ltd & Co Kg Zapfluftauslass im Nebenstromkanal eines Turbofantriebwerks
US9377201B2 (en) 2013-02-08 2016-06-28 Solar Turbines Incorporated Forged fuel injector stem
EP3076084B1 (en) * 2015-03-30 2021-04-28 Ansaldo Energia Switzerland AG Fuel injector device
US10329941B2 (en) * 2016-05-06 2019-06-25 United Technologies Corporation Impingement manifold
DE102017125051A1 (de) * 2017-10-26 2019-05-02 Man Diesel & Turbo Se Strömungsmaschine
US11085641B2 (en) * 2018-11-27 2021-08-10 Honeywell International Inc. Plug resistant effusion holes for gas turbine engine
US11021963B2 (en) * 2019-05-03 2021-06-01 Raytheon Technologies Corporation Monolithic body including an internal passage with a generally teardrop shaped cross-sectional geometry

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791758A (en) * 1971-05-06 1974-02-12 Secr Defence Cooling of turbine blades
JPH07208208A (ja) * 1993-12-06 1995-08-08 United Technol Corp <Utc> ガスタービンエンジン用汚染防止スラスト釣り合いシステム
JPH10176547A (ja) * 1996-12-13 1998-06-30 Solar Turbines Inc タービンディスク侵入防止方法及び装置
JPH11132002A (ja) * 1997-10-28 1999-05-18 Mitsubishi Heavy Ind Ltd 流量調整プラグ
JP2001152806A (ja) * 1999-11-30 2001-06-05 General Electric Co <Ge> タービンノズルセグメント壁の冷却
JP2002201964A (ja) * 2000-11-03 2002-07-19 General Electric Co <Ge> ガス噴射器システム及びその製造
US20020122716A1 (en) * 2001-02-28 2002-09-05 Beacock Robert John Methods and apparatus for cooling gas turbine engine blade tips

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4966001A (en) * 1987-10-23 1990-10-30 General Electric Company Multiple venturi tube gas fuel injector for catalytic combustor
US5001895A (en) * 1987-12-14 1991-03-26 Sundstrand Corporation Fuel injector for turbine engines
US4891936A (en) * 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
CA2014999C (en) * 1989-04-24 1999-09-07 Kenneth William Bates Gas injector
DE69305326T2 (de) * 1992-02-10 1997-05-07 United Technologies Corp Ejektor für kühlfluid
US5727378A (en) * 1995-08-25 1998-03-17 Great Lakes Helicopters Inc. Gas turbine engine
US5988531A (en) * 1997-11-25 1999-11-23 Solar Turbines Method of making a fuel injector
TW513833B (en) * 1998-09-09 2002-12-11 Honda Motor Co Ltd Mounting method of sparking plug cap and sparking plug cap
US6224329B1 (en) * 1999-01-07 2001-05-01 Siemens Westinghouse Power Corporation Method of cooling a combustion turbine
US6234746B1 (en) * 1999-08-04 2001-05-22 General Electric Co. Apparatus and methods for cooling rotary components in a turbine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791758A (en) * 1971-05-06 1974-02-12 Secr Defence Cooling of turbine blades
JPH07208208A (ja) * 1993-12-06 1995-08-08 United Technol Corp <Utc> ガスタービンエンジン用汚染防止スラスト釣り合いシステム
JPH10176547A (ja) * 1996-12-13 1998-06-30 Solar Turbines Inc タービンディスク侵入防止方法及び装置
JPH11132002A (ja) * 1997-10-28 1999-05-18 Mitsubishi Heavy Ind Ltd 流量調整プラグ
JP2001152806A (ja) * 1999-11-30 2001-06-05 General Electric Co <Ge> タービンノズルセグメント壁の冷却
JP2002201964A (ja) * 2000-11-03 2002-07-19 General Electric Co <Ge> ガス噴射器システム及びその製造
US20020122716A1 (en) * 2001-02-28 2002-09-05 Beacock Robert John Methods and apparatus for cooling gas turbine engine blade tips

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101774094B1 (ko) * 2011-08-22 2017-09-04 마제드 토칸 가스 터빈 엔진에서 사용되는 예비혼합형 접선방향 연료-공기 노즐을 가진 캔-애뉼러형 연소실
KR101774093B1 (ko) * 2011-08-22 2017-09-12 마제드 토칸 가스 터빈 엔진에서 사용되는 스테이지가 형성되고 접선방향으로 형성된 연료-공기 노즐을 가진 캔-애뉼러형 연소실
KR101774630B1 (ko) * 2011-08-22 2017-09-19 마제드 토칸 가스 터빈 엔진에 사용되는 예비혼합된 연료와 공기를 가진 접선방향의 애뉼러형 연소실
KR101832026B1 (ko) * 2011-08-22 2018-02-23 마제드 토칸 가스 터빈 엔진에 사용되는 접선방향의 무염 애뉼러형 연소실

Also Published As

Publication number Publication date
US20040213664A1 (en) 2004-10-28
CN100507236C (zh) 2009-07-01
EP1473518A3 (en) 2012-10-31
EP1473518A2 (en) 2004-11-03
US7052231B2 (en) 2006-05-30
CN1542267A (zh) 2004-11-03

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