CN100339562C - 安装燃气轮机喷嘴的设备 - Google Patents

安装燃气轮机喷嘴的设备 Download PDF

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Publication number
CN100339562C
CN100339562C CNB2003101131026A CN200310113102A CN100339562C CN 100339562 C CN100339562 C CN 100339562C CN B2003101131026 A CNB2003101131026 A CN B2003101131026A CN 200310113102 A CN200310113102 A CN 200310113102A CN 100339562 C CN100339562 C CN 100339562C
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CN
China
Prior art keywords
gas turbine
turbine
track
clamp
turbine nozzle
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
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CNB2003101131026A
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English (en)
Chinese (zh)
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CN1512039A (zh
Inventor
G·S·布雷恩克
D·利纳恩
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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 CN1512039A publication Critical patent/CN1512039A/zh
Application granted granted Critical
Publication of CN100339562C publication Critical patent/CN100339562C/zh
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
CNB2003101131026A 2002-12-20 2003-12-22 安装燃气轮机喷嘴的设备 Expired - Lifetime CN100339562C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/324,849 US6893217B2 (en) 2002-12-20 2002-12-20 Methods and apparatus for assembling gas turbine nozzles
US10/324849 2002-12-20

Publications (2)

Publication Number Publication Date
CN1512039A CN1512039A (zh) 2004-07-14
CN100339562C true CN100339562C (zh) 2007-09-26

Family

ID=32393080

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2003101131026A Expired - Lifetime CN100339562C (zh) 2002-12-20 2003-12-22 安装燃气轮机喷嘴的设备

Country Status (4)

Country Link
US (1) US6893217B2 (enExample)
EP (1) EP1431517A3 (enExample)
JP (1) JP4515086B2 (enExample)
CN (1) CN100339562C (enExample)

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Publication number Priority date Publication date Assignee Title
JP4346412B2 (ja) * 2003-10-31 2009-10-21 株式会社東芝 タービン翼列装置
US7762761B2 (en) * 2005-11-30 2010-07-27 General Electric Company Methods and apparatus for assembling turbine nozzles
US7360988B2 (en) * 2005-12-08 2008-04-22 General Electric Company Methods and apparatus for assembling turbine engines
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines
FR2899275A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine
US7419352B2 (en) * 2006-10-03 2008-09-02 General Electric Company Methods and apparatus for assembling turbine engines
US7771164B2 (en) * 2006-12-18 2010-08-10 General Electric Company Method and system for assembling a turbine engine
GB0700142D0 (en) * 2007-01-05 2007-02-14 Rolls Royce Plc Nozzle guide vane arrangement
FR2923525B1 (fr) * 2007-11-13 2009-12-18 Snecma Etancheite d'un anneau de rotor dans un etage de turbine
FR2925107B1 (fr) * 2007-12-14 2010-01-22 Snecma Distributeur sectorise pour une turbomachine
FR2925572B1 (fr) * 2007-12-24 2010-02-12 Snecma Services Procede de choix d'un arrangement de secteurs pour un distributeur pour turbomachine
US8449249B2 (en) * 2010-04-09 2013-05-28 Williams International Co., L.L.C. Turbine nozzle apparatus and associated method of manufacture
US8668445B2 (en) * 2010-10-15 2014-03-11 General Electric Company Variable turbine nozzle system
US8651497B2 (en) 2011-06-17 2014-02-18 United Technologies Corporation Winged W-seal
FR2990719B1 (fr) * 2012-05-16 2016-07-22 Snecma Distributeur de turbomachine, et procede de fabrication
US9851008B2 (en) * 2012-06-04 2017-12-26 United Technologies Corporation Seal land for static structure of a gas turbine engine
US10598036B2 (en) 2013-03-13 2020-03-24 United Technologies Corporation Assembly for sealing a gap between components of a turbine engine
EP2971571B1 (en) * 2013-03-13 2019-12-04 United Technologies Corporation Stator segment
WO2014152209A1 (en) * 2013-03-14 2014-09-25 United Technologies Corporation Assembly for sealing a gap between components of a turbine engine
EP2984291B8 (en) * 2013-04-11 2021-04-07 Raytheon Technologies Corporation Nozzle segment for a gas turbine engine
EP3008309B1 (en) * 2013-06-14 2018-04-25 United Technologies Corporation Gas turbine engine flow control device
JP5717904B1 (ja) * 2014-08-04 2015-05-13 三菱日立パワーシステムズ株式会社 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法
EP3088691B1 (en) * 2015-04-27 2019-06-19 Ansaldo Energia Switzerland AG Gas turbine disassembly method
DE102015224378A1 (de) * 2015-12-04 2017-06-08 MTU Aero Engines AG Leitschaufelsegment mit Radialsicherung
FR3072718B1 (fr) * 2017-10-20 2020-10-16 Safran Aircraft Engines Secteur de distributeur pour turbomachine comprenant un rebord de fixation
JP7284737B2 (ja) * 2020-08-06 2023-05-31 三菱重工業株式会社 ガスタービン静翼
CN112324521A (zh) * 2020-11-03 2021-02-05 中国航发沈阳发动机研究所 一种串列静子结构
FR3116861B1 (fr) * 2020-11-27 2022-10-21 Safran Aircraft Engines Dispositif et procede de controle des secteurs pour l’assemblage de distributeurs d’une turbine
CN115142907B (zh) * 2022-09-02 2022-11-22 中国航发沈阳发动机研究所 一种航空发动机导叶内环一体结构

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US4425078A (en) * 1980-07-18 1984-01-10 United Technologies Corporation Axial flexible radially stiff retaining ring for sealing in a gas turbine engine
US5092735A (en) * 1990-07-02 1992-03-03 The United States Of America As Represented By The Secretary Of The Air Force Blade outer air seal cooling system
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
US5343694A (en) * 1991-07-22 1994-09-06 General Electric Company Turbine nozzle support
US5358379A (en) * 1993-10-27 1994-10-25 Westinghouse Electric Corporation Gas turbine vane
US6076835A (en) * 1997-05-21 2000-06-20 Allison Advanced Development Company Interstage van seal apparatus
US6227800B1 (en) * 1998-11-24 2001-05-08 General Electric Company Bay cooled turbine casing

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US3842595A (en) * 1972-12-26 1974-10-22 Gen Electric Modular gas turbine engine
US4126405A (en) 1976-12-16 1978-11-21 General Electric Company Turbine nozzle
US4297077A (en) 1979-07-09 1981-10-27 Westinghouse Electric Corp. Cooled turbine vane
US4531289A (en) 1983-01-28 1985-07-30 F. M. Brick Industries, Inc. High-power rescue tool
US4842249A (en) 1983-09-16 1989-06-27 Weigand George R Spreader type rescue tool
US4522054A (en) 1983-09-26 1985-06-11 Power Pry Corporation Emergency rescue apparatus
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US5289711A (en) 1991-05-15 1994-03-01 Spiegel Leo J Apparatus for spreading steel structures
US5243761A (en) 1992-03-18 1993-09-14 Hale Fire Pump Company Portable rescue tool
US5249920A (en) 1992-07-09 1993-10-05 General Electric Company Turbine nozzle seal arrangement
US5372476A (en) 1993-06-18 1994-12-13 General Electric Company Turbine nozzle support assembly
US5425260A (en) 1994-01-27 1995-06-20 Gehron; Michael A. Accident rescue tool
US5662160A (en) 1995-10-12 1997-09-02 General Electric Co. Turbine nozzle and related casting method for optimal fillet wall thickness control
US5620300A (en) 1995-11-16 1997-04-15 General Electric Co. Method of constructing a turbine nozzle to prevent structurally induced excitation forces
US5669757A (en) 1995-11-30 1997-09-23 General Electric Company Turbine nozzle retainer assembly
US5732932A (en) 1996-03-27 1998-03-31 American Rescue Technology Incorporated Hydraulic ram attachment for a rescue tool
US5953822A (en) 1996-12-24 1999-09-21 Rescue Technology, Inc. Rescue tool
US5875554A (en) 1996-12-24 1999-03-02 Rescue Technology, Inc. Rescue tool
US5810333A (en) 1997-02-06 1998-09-22 Curtiss Wright Flight Systems Inc. Ram device
US6193465B1 (en) 1998-09-28 2001-02-27 General Electric Company Trapped insert turbine airfoil
DE19848103A1 (de) * 1998-10-19 2000-04-20 Asea Brown Boveri Dichtungsanordnung
US6099245A (en) 1998-10-30 2000-08-08 General Electric Company Tandem airfoils
US6311537B1 (en) 1998-10-30 2001-11-06 Orlando C. Vigil Blade tip for a rescue tool
US6120242A (en) * 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
US6164656A (en) 1999-01-29 2000-12-26 General Electric Company Turbine nozzle interface seal and methods
US6272900B1 (en) 1999-04-21 2001-08-14 Matthew Kobel Extension ram tip
FR2803871B1 (fr) * 2000-01-13 2002-06-07 Snecma Moteurs Agencement de reglage de diametre d'un stator de turbine a gaz

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4314792A (en) * 1978-12-20 1982-02-09 United Technologies Corporation Turbine seal and vane damper
US4425078A (en) * 1980-07-18 1984-01-10 United Technologies Corporation Axial flexible radially stiff retaining ring for sealing in a gas turbine engine
US5092735A (en) * 1990-07-02 1992-03-03 The United States Of America As Represented By The Secretary Of The Air Force Blade outer air seal cooling system
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
US5343694A (en) * 1991-07-22 1994-09-06 General Electric Company Turbine nozzle support
US5358379A (en) * 1993-10-27 1994-10-25 Westinghouse Electric Corporation Gas turbine vane
US6076835A (en) * 1997-05-21 2000-06-20 Allison Advanced Development Company Interstage van seal apparatus
US6227800B1 (en) * 1998-11-24 2001-05-08 General Electric Company Bay cooled turbine casing

Also Published As

Publication number Publication date
US6893217B2 (en) 2005-05-17
JP2004204844A (ja) 2004-07-22
EP1431517A2 (en) 2004-06-23
CN1512039A (zh) 2004-07-14
US20040120814A1 (en) 2004-06-24
JP4515086B2 (ja) 2010-07-28
EP1431517A3 (en) 2005-10-12

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PB01 Publication
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SE01 Entry into force of request for substantive examination
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GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20070926

CX01 Expiry of patent term