JP2004257389A5 - - Google Patents

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Publication number
JP2004257389A5
JP2004257389A5 JP2004050704A JP2004050704A JP2004257389A5 JP 2004257389 A5 JP2004257389 A5 JP 2004257389A5 JP 2004050704 A JP2004050704 A JP 2004050704A JP 2004050704 A JP2004050704 A JP 2004050704A JP 2004257389 A5 JP2004257389 A5 JP 2004257389A5
Authority
JP
Japan
Prior art keywords
airfoil
turbine nozzle
segment
nozzle segment
extending
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.)
Granted
Application number
JP2004050704A
Other languages
English (en)
Japanese (ja)
Other versions
JP4049754B2 (ja
JP2004257389A (ja
Filing date
Publication date
Priority claimed from US10/375,441 external-priority patent/US6932568B2/en
Application filed filed Critical
Publication of JP2004257389A publication Critical patent/JP2004257389A/ja
Publication of JP2004257389A5 publication Critical patent/JP2004257389A5/ja
Application granted granted Critical
Publication of JP4049754B2 publication Critical patent/JP4049754B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2004050704A 2003-02-27 2004-02-26 タービンノズルセグメントの片持ち式支持 Expired - Fee Related JP4049754B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/375,441 US6932568B2 (en) 2003-02-27 2003-02-27 Turbine nozzle segment cantilevered mount

Publications (3)

Publication Number Publication Date
JP2004257389A JP2004257389A (ja) 2004-09-16
JP2004257389A5 true JP2004257389A5 (cg-RX-API-DMAC7.html) 2007-04-12
JP4049754B2 JP4049754B2 (ja) 2008-02-20

Family

ID=32771458

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004050704A Expired - Fee Related JP4049754B2 (ja) 2003-02-27 2004-02-26 タービンノズルセグメントの片持ち式支持

Country Status (4)

Country Link
US (1) US6932568B2 (cg-RX-API-DMAC7.html)
EP (1) EP1452693B1 (cg-RX-API-DMAC7.html)
JP (1) JP4049754B2 (cg-RX-API-DMAC7.html)
CN (1) CN100460630C (cg-RX-API-DMAC7.html)

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US7798775B2 (en) * 2006-12-21 2010-09-21 General Electric Company Cantilevered nozzle with crowned flange to improve outer band low cycle fatigue
US8511983B2 (en) 2008-02-19 2013-08-20 United Technologies Corporation LPC exit guide vane and assembly
EP2093381A1 (en) * 2008-02-25 2009-08-26 Siemens Aktiengesellschaft Turbine blade or vane with cooled platform
US8172522B2 (en) * 2008-03-31 2012-05-08 General Electric Company Method and system for supporting stator components
US8092163B2 (en) * 2008-03-31 2012-01-10 General Electric Company Turbine stator mount
DE102009003638A1 (de) * 2008-03-31 2009-10-01 General Electric Co. System und Verfahren zur Halterung von Statorkomponenten
US8118550B2 (en) * 2009-03-11 2012-02-21 General Electric Company Turbine singlet nozzle assembly with radial stop and narrow groove
US8070429B2 (en) * 2009-03-11 2011-12-06 General Electric Company Turbine singlet nozzle assembly with mechanical and weld fabrication
US8978388B2 (en) 2011-06-03 2015-03-17 General Electric Company Load member for transition duct in turbine system
US20130004320A1 (en) * 2011-06-28 2013-01-03 United Technologies Corporation Method of rotated airfoils
US8944751B2 (en) 2012-01-09 2015-02-03 General Electric Company Turbine nozzle cooling assembly
US8864445B2 (en) 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US9133724B2 (en) 2012-01-09 2015-09-15 General Electric Company Turbomachine component including a cover plate
US9011078B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine vane seal carrier with slots for cooling and assembly
US9011079B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine nozzle compartmentalized cooling system
US9039350B2 (en) 2012-01-09 2015-05-26 General Electric Company Impingement cooling system for use with contoured surfaces
EP2626519A1 (en) * 2012-02-09 2013-08-14 Siemens Aktiengesellschaft Turbine assembly, corresponding impingement cooling tube and gas turbine engine
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US9371735B2 (en) 2012-11-29 2016-06-21 Solar Turbines Incorporated Gas turbine engine turbine nozzle impingement cover
WO2015009418A1 (en) 2013-07-15 2015-01-22 United Technologies Corporation Turbine vanes with variable fillets
US9745864B2 (en) * 2014-04-16 2017-08-29 United Technologies Corporation Systems and methods for anti-rotational features
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
US9915159B2 (en) 2014-12-18 2018-03-13 General Electric Company Ceramic matrix composite nozzle mounted with a strut and concepts thereof
US10012092B2 (en) * 2015-08-12 2018-07-03 United Technologies Corporation Low turn loss baffle flow diverter
US10253986B2 (en) * 2015-09-08 2019-04-09 General Electric Company Article and method of forming an article
US10344619B2 (en) * 2016-07-08 2019-07-09 United Technologies Corporation Cooling system for a gaspath component of a gas powered turbine
US10557362B2 (en) 2017-03-30 2020-02-11 General Electric Company Method and system for a pressure activated cap seal
US11149555B2 (en) * 2017-06-14 2021-10-19 General Electric Company Turbine engine component with deflector
US10774656B2 (en) * 2018-04-09 2020-09-15 General Electric Company Turbine airfoil multilayer exterior wall
GB201907545D0 (en) 2019-05-29 2019-07-10 Siemens Ag Heatshield for a gas turbine engine
US11230931B1 (en) * 2020-07-03 2022-01-25 Raytheon Technologies Corporation Inserts for airfoils of gas turbine engines
CN112228168B (zh) * 2020-10-21 2022-09-30 中国航发沈阳发动机研究所 一种静子叶片内腔冷却用集气引流结构
US11391162B2 (en) 2020-12-15 2022-07-19 Raytheon Technologies Corporation Spar with embedded plenum passage
US11536147B2 (en) 2021-03-30 2022-12-27 Raytheon Technologies Corporation Vane arc segment with flange and gusset
US12467366B2 (en) * 2023-12-01 2025-11-11 General Electric Company Turbine engine with a nozzle having cooling features

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