JP2004204844A5 - - Google Patents

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Publication number
JP2004204844A5
JP2004204844A5 JP2003421872A JP2003421872A JP2004204844A5 JP 2004204844 A5 JP2004204844 A5 JP 2004204844A5 JP 2003421872 A JP2003421872 A JP 2003421872A JP 2003421872 A JP2003421872 A JP 2003421872A JP 2004204844 A5 JP2004204844 A5 JP 2004204844A5
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JP
Japan
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.)
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Application number
JP2003421872A
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JP4515086B2 (ja
JP2004204844A (ja
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Priority claimed from US10/324,849 external-priority patent/US6893217B2/en
Application filed filed Critical
Publication of JP2004204844A publication Critical patent/JP2004204844A/ja
Publication of JP2004204844A5 publication Critical patent/JP2004204844A5/ja
Application granted granted Critical
Publication of JP4515086B2 publication Critical patent/JP4515086B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2003421872A 2002-12-20 2003-12-19 ガスタービンノズルを組み立てるための方法及び装置 Expired - Fee Related JP4515086B2 (ja)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
JP2004204844A JP2004204844A (ja) 2004-07-22
JP2004204844A5 true JP2004204844A5 (ja) 2007-02-08
JP4515086B2 JP4515086B2 (ja) 2010-07-28

Family

ID=32393080

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003421872A Expired - Fee Related JP4515086B2 (ja) 2002-12-20 2003-12-19 ガスタービンノズルを組み立てるための方法及び装置

Country Status (4)

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

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* Cited by examiner, † Cited by third party
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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
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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
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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
WO2014197042A2 (en) * 2013-03-13 2014-12-11 United Technologies Corporation Stator segment
WO2014165182A1 (en) * 2013-03-13 2014-10-09 United Technologies Corporation Assembly for sealing a gap between components of a turbine engine
US10196911B2 (en) 2013-03-14 2019-02-05 United Technologioes 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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