JP2012172588A5 - - Google Patents

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Publication number
JP2012172588A5
JP2012172588A5 JP2011035305A JP2011035305A JP2012172588A5 JP 2012172588 A5 JP2012172588 A5 JP 2012172588A5 JP 2011035305 A JP2011035305 A JP 2011035305A JP 2011035305 A JP2011035305 A JP 2011035305A JP 2012172588 A5 JP2012172588 A5 JP 2012172588A5
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JP
Japan
Prior art keywords
blade
pressure difference
secondary flow
load
boundary layer
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
JP2011035305A
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English (en)
Japanese (ja)
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JP2012172588A (ja
JP5603800B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority to JP2011035305A priority Critical patent/JP5603800B2/ja
Priority claimed from JP2011035305A external-priority patent/JP5603800B2/ja
Priority to US13/396,798 priority patent/US20120210715A1/en
Priority to EP12156171.6A priority patent/EP2492440B1/en
Publication of JP2012172588A publication Critical patent/JP2012172588A/ja
Publication of JP2012172588A5 publication Critical patent/JP2012172588A5/ja
Application granted granted Critical
Publication of JP5603800B2 publication Critical patent/JP5603800B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011035305A 2011-02-22 2011-02-22 タービン静翼、およびそれを用いた蒸気タービン設備 Active JP5603800B2 (ja)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP2011035305A JP5603800B2 (ja) 2011-02-22 2011-02-22 タービン静翼、およびそれを用いた蒸気タービン設備
US13/396,798 US20120210715A1 (en) 2011-02-22 2012-02-15 Turbine Nozzle Blade and Steam Turbine Equipment Using Same
EP12156171.6A EP2492440B1 (en) 2011-02-22 2012-02-20 Turbine nozzle blade and steam turbine equipment using same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011035305A JP5603800B2 (ja) 2011-02-22 2011-02-22 タービン静翼、およびそれを用いた蒸気タービン設備

Publications (3)

Publication Number Publication Date
JP2012172588A JP2012172588A (ja) 2012-09-10
JP2012172588A5 true JP2012172588A5 (enExample) 2013-03-28
JP5603800B2 JP5603800B2 (ja) 2014-10-08

Family

ID=45656180

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011035305A Active JP5603800B2 (ja) 2011-02-22 2011-02-22 タービン静翼、およびそれを用いた蒸気タービン設備

Country Status (3)

Country Link
US (1) US20120210715A1 (enExample)
EP (1) EP2492440B1 (enExample)
JP (1) JP5603800B2 (enExample)

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EP2379276A4 (en) * 2008-12-19 2012-06-27 Volvo Aero Corp MEMORY FOR A STATOR COMPONENT, STATOR COMPONENT, AND METHOD FOR PRODUCING A STATOR COMPONENT
JP5936992B2 (ja) * 2012-11-06 2016-06-22 株式会社東芝 蒸気タービン
JP6125351B2 (ja) * 2013-06-27 2017-05-10 株式会社東芝 蒸気タービン
EP2827003B1 (de) * 2013-07-15 2019-04-10 MTU Aero Engines GmbH Gasturbinen-Verdichter-Leitgitter
EP3985226B1 (en) * 2014-02-19 2024-12-25 RTX Corporation Gas turbine engine airfoil
EP2921647A1 (en) 2014-03-20 2015-09-23 Alstom Technology Ltd Gas turbine blade comprising bended leading and trailing edges
US10060263B2 (en) * 2014-09-15 2018-08-28 United Technologies Corporation Incidence-tolerant, high-turning fan exit stator
US9995166B2 (en) * 2014-11-21 2018-06-12 General Electric Company Turbomachine including a vane and method of assembling such turbomachine
US20170138202A1 (en) * 2015-11-16 2017-05-18 General Electric Company Optimal lift designs for gas turbine engines
US9963985B2 (en) * 2015-12-18 2018-05-08 General Electric Company Turbomachine and turbine nozzle therefor
US10107104B2 (en) * 2016-01-29 2018-10-23 Rolls-Royce Corporation Airfoils for reducing secondary flow losses in gas turbine engines
US11092068B2 (en) * 2016-03-30 2021-08-17 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Variable geometry turbocharger
FR3059353B1 (fr) * 2016-11-29 2019-05-17 Safran Aircraft Engines Aube directrice de sortie pour turbomachine d'aeronef, comprenant une zone coudee de passage de lubrifiant presentant une conception amelioree
EP3358134B1 (en) * 2017-02-02 2021-07-14 General Electric Company Steam turbine with rotor blade
US10982549B2 (en) * 2017-04-17 2021-04-20 General Electric Company Stator vanes including curved trailing edges
US10392961B2 (en) * 2017-05-18 2019-08-27 Ford Global Technologies, Llc Nozzle blade design for a variable nozzle turbine
CN107489461A (zh) * 2017-09-15 2017-12-19 哈尔滨汽轮机厂有限责任公司 一种用于汽轮机叶片的高效宽负荷叶型
US20190106989A1 (en) * 2017-10-09 2019-04-11 United Technologies Corporation Gas turbine engine airfoil
CN108194150B (zh) * 2018-02-11 2023-06-09 杭州汽轮动力集团股份有限公司 一种工业汽轮机大负荷高效调节级静叶片
EP3569817B1 (en) * 2018-05-14 2020-10-14 ArianeGroup GmbH Guide vane arrangement for use in a turbine
PL3816397T3 (pl) * 2019-10-31 2023-06-19 General Electric Company Łopatki turbiny o kontrolowanym przepływie
CN111259559B (zh) * 2020-02-02 2023-03-24 上海交通大学 悬臂静子叶片前加载设计减小损失的流动控制方法
CN112610283B (zh) * 2020-12-17 2023-01-06 哈尔滨工业大学 一种采用端壁分区造型设计的涡轮叶栅

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Publication number Priority date Publication date Assignee Title
JPS5274706A (en) * 1975-12-19 1977-06-23 Hitachi Ltd Turbine vane train
JPS5925091B2 (ja) * 1979-11-09 1984-06-14 株式会社日立製作所 タ−ビン静翼
JPS59115500A (ja) * 1982-12-22 1984-07-03 Junji Uematsu 軸流旋転機械減速翼列の翼
US5383768A (en) * 1989-02-03 1995-01-24 Hitachi, Ltd. Steam turbine, rotor shaft thereof, and heat resisting steel
JPH1037703A (ja) * 1996-07-25 1998-02-10 Toshiba Corp タービンノズル
JPH10103002A (ja) * 1996-09-30 1998-04-21 Toshiba Corp 軸流流体機械用翼
JP4346412B2 (ja) * 2003-10-31 2009-10-21 株式会社東芝 タービン翼列装置
JP2006207556A (ja) * 2005-01-31 2006-08-10 Toshiba Corp タービン翼列
US7220100B2 (en) * 2005-04-14 2007-05-22 General Electric Company Crescentic ramp turbine stage
WO2007042522A1 (de) * 2005-10-11 2007-04-19 Alstom Technology Ltd Turbomaschinenschaufel
US7686567B2 (en) * 2005-12-16 2010-03-30 United Technologies Corporation Airfoil embodying mixed loading conventions
JP4869099B2 (ja) 2007-02-16 2012-02-01 株式会社東芝 ノズル翼および軸流タービン
GB0704426D0 (en) * 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine

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