JP2004534922A5 - - Google Patents

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Publication number
JP2004534922A5
JP2004534922A5 JP2003512538A JP2003512538A JP2004534922A5 JP 2004534922 A5 JP2004534922 A5 JP 2004534922A5 JP 2003512538 A JP2003512538 A JP 2003512538A JP 2003512538 A JP2003512538 A JP 2003512538A JP 2004534922 A5 JP2004534922 A5 JP 2004534922A5
Authority
JP
Japan
Prior art keywords
airfoil
turbine
distance
nozzle
plane
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
JP2003512538A
Other languages
English (en)
Japanese (ja)
Other versions
JP2004534922A (ja
Filing date
Publication date
Priority claimed from US09/903,874 external-priority patent/US6461109B1/en
Application filed filed Critical
Publication of JP2004534922A publication Critical patent/JP2004534922A/ja
Publication of JP2004534922A5 publication Critical patent/JP2004534922A5/ja
Pending legal-status Critical Current

Links

JP2003512538A 2001-07-13 2002-07-10 第３段タービンノズル翼形部 Pending JP2004534922A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/903,874 US6461109B1 (en) 2001-07-13 2001-07-13 Third-stage turbine nozzle airfoil
PCT/US2002/022343 WO2003006798A1 (en) 2001-07-13 2002-07-10 Third-stage turbine nozzle airfoil

Publications (2)

Publication Number Publication Date
JP2004534922A JP2004534922A (ja) 2004-11-18
JP2004534922A5 true JP2004534922A5 (enExample) 2006-01-05

Family

ID=25418194

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003512538A Pending JP2004534922A (ja) 2001-07-13 2002-07-10 第３段タービンノズル翼形部

Country Status (5)

Country Link
US (1) US6461109B1 (enExample)
EP (1) EP1409848A1 (enExample)
JP (1) JP2004534922A (enExample)
KR (1) KR20040018240A (enExample)
WO (1) WO2003006798A1 (enExample)

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US7467926B2 (en) 2006-06-09 2008-12-23 General Electric Company Stator blade airfoil profile for a compressor
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US7572104B2 (en) * 2006-10-25 2009-08-11 General Electric Company Airfoil shape for a compressor
US7517197B2 (en) * 2006-10-25 2009-04-14 General Electric Company Airfoil shape for a compressor
US7510378B2 (en) * 2006-10-25 2009-03-31 General Electric Company Airfoil shape for a compressor
US7566202B2 (en) * 2006-10-25 2009-07-28 General Electric Company Airfoil shape for a compressor
US7572105B2 (en) * 2006-10-25 2009-08-11 General Electric Company Airfoil shape for a compressor
US7513748B2 (en) * 2006-10-25 2009-04-07 General Electric Company Airfoil shape for a compressor
US7568892B2 (en) * 2006-11-02 2009-08-04 General Electric Company Airfoil shape for a compressor
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US7837445B2 (en) * 2007-08-31 2010-11-23 General Electric Company Airfoil shape for a turbine nozzle
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US8573945B2 (en) * 2009-11-13 2013-11-05 Alstom Technology Ltd. Compressor stator vane
US8511979B2 (en) * 2010-03-30 2013-08-20 Pratt & Whitney Canada Corp. High pressure turbine vane airfoil profile
US8757968B2 (en) 2010-07-26 2014-06-24 Snecma Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine
US8734113B2 (en) * 2010-07-26 2014-05-27 Snecma Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine
US8393870B2 (en) 2010-09-08 2013-03-12 United Technologies Corporation Turbine blade airfoil
US8602740B2 (en) 2010-09-08 2013-12-10 United Technologies Corporation Turbine vane airfoil
US8585360B2 (en) 2010-09-09 2013-11-19 Siemens Energy, Inc. Turbine vane nominal airfoil profile
US8591193B2 (en) 2011-02-25 2013-11-26 General Electric Company Airfoil shape for a compressor blade
US8814511B2 (en) 2011-08-09 2014-08-26 General Electric Company Turbomachine component having an airfoil core shape
US8814526B2 (en) 2011-11-28 2014-08-26 General Electric Company Turbine nozzle airfoil profile
US8734116B2 (en) 2011-11-28 2014-05-27 General Electric Company Turbine bucket airfoil profile
US8827641B2 (en) * 2011-11-28 2014-09-09 General Electric Company Turbine nozzle airfoil profile
US8740570B2 (en) 2011-11-28 2014-06-03 General Electric Company Turbine bucket airfoil profile
US9011101B2 (en) 2011-11-28 2015-04-21 General Electric Company Turbine bucket airfoil profile
US10822976B2 (en) 2013-06-03 2020-11-03 General Electric Company Nozzle insert rib cap
CN103557034B (zh) * 2013-09-30 2015-07-15 哈尔滨汽轮机厂有限责任公司 一种应用于重型中低热值燃机的涡轮第二级导叶片
CN104295324B (zh) * 2014-09-30 2016-06-29 哈尔滨汽轮机厂有限责任公司 一种用于重型中低热值燃机的涡轮第三级导叶片
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JP6971564B2 (ja) 2015-12-18 2021-11-24 ゼネラル・エレクトリック・カンパニイ ターボ機械およびそのためのタービンノズル
US9957804B2 (en) 2015-12-18 2018-05-01 General Electric Company Turbomachine and turbine blade transfer
US9963985B2 (en) 2015-12-18 2018-05-08 General Electric Company Turbomachine and turbine nozzle therefor
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US10443393B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine
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US6450770B1 (en) * 2001-06-28 2002-09-17 General Electric Company Second-stage turbine bucket airfoil
US6461109B1 (en) * 2001-07-13 2002-10-08 General Electric Company Third-stage turbine nozzle airfoil

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