JP2009511811A5 - - Google Patents

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Publication number
JP2009511811A5
JP2009511811A5 JP2008535014A JP2008535014A JP2009511811A5 JP 2009511811 A5 JP2009511811 A5 JP 2009511811A5 JP 2008535014 A JP2008535014 A JP 2008535014A JP 2008535014 A JP2008535014 A JP 2008535014A JP 2009511811 A5 JP2009511811 A5 JP 2009511811A5
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JP
Japan
Prior art keywords
blade
chord length
wing
tip
leg
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
JP2008535014A
Other languages
English (en)
Japanese (ja)
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JP2009511811A (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from PCT/EP2006/067250 external-priority patent/WO2007042522A1/de
Publication of JP2009511811A publication Critical patent/JP2009511811A/ja
Publication of JP2009511811A5 publication Critical patent/JP2009511811A5/ja
Pending legal-status Critical Current

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JP2008535014A 2005-10-11 2006-10-11 ターボ機械用翼 Pending JP2009511811A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH16432005 2005-10-11
PCT/EP2006/067250 WO2007042522A1 (de) 2005-10-11 2006-10-11 Turbomaschinenschaufel

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2012166361A Division JP5420729B2 (ja) 2005-10-11 2012-07-26 ターボ機械用翼

Publications (2)

Publication Number Publication Date
JP2009511811A JP2009511811A (ja) 2009-03-19
JP2009511811A5 true JP2009511811A5 (enExample) 2012-01-12

Family

ID=35583515

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2008535014A Pending JP2009511811A (ja) 2005-10-11 2006-10-11 ターボ機械用翼
JP2012166361A Active JP5420729B2 (ja) 2005-10-11 2012-07-26 ターボ機械用翼

Family Applications After (1)

Application Number Title Priority Date Filing Date
JP2012166361A Active JP5420729B2 (ja) 2005-10-11 2012-07-26 ターボ機械用翼

Country Status (5)

Country Link
US (1) US8221065B2 (enExample)
JP (2) JP2009511811A (enExample)
CN (1) CN101326342B (enExample)
DE (1) DE112006002658B4 (enExample)
WO (1) WO2007042522A1 (enExample)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7686567B2 (en) * 2005-12-16 2010-03-30 United Technologies Corporation Airfoil embodying mixed loading conventions
DE102006055869A1 (de) 2006-11-23 2008-05-29 Rolls-Royce Deutschland Ltd & Co Kg Schaufelblattdesign für die Lauf- und Leitschaufeln einer Turbomaschine
DE102009023100A1 (de) * 2009-05-28 2010-12-02 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit einer Schaufelreihengruppe mit meridionalem Kantenabstand
US8573945B2 (en) * 2009-11-13 2013-11-05 Alstom Technology Ltd. Compressor stator vane
JP5603800B2 (ja) * 2011-02-22 2014-10-08 株式会社日立製作所 タービン静翼、およびそれを用いた蒸気タービン設備
GB201108001D0 (en) * 2011-05-13 2011-06-29 Rolls Royce Plc A method of reducing asymmetric fluid flow effect in a passage
JP5866802B2 (ja) 2011-05-26 2016-02-17 株式会社Ihi ノズル翼
CH705171A1 (de) * 2011-06-21 2012-12-31 Alstom Technology Ltd Turbinenschaufel mit einem Schaufelblatt aus Verbundwerkstoff und Verfahren zum Herstellen davon.
FR2991373B1 (fr) * 2012-05-31 2014-06-20 Snecma Aube de soufflante pour turboreacteur d'avion a profil cambre en sections de pied
JP5946707B2 (ja) * 2012-07-06 2016-07-06 三菱日立パワーシステムズ株式会社 軸流タービン動翼
EP2696042B1 (de) 2012-08-09 2015-01-21 MTU Aero Engines GmbH Strömungsmaschine mit mindestens einem Leitschaufelkranz
EP2921647A1 (en) 2014-03-20 2015-09-23 Alstom Technology Ltd Gas turbine blade comprising bended leading and trailing edges
US20150275675A1 (en) * 2014-03-27 2015-10-01 General Electric Company Bucket airfoil for a turbomachine
US10508549B2 (en) * 2014-06-06 2019-12-17 United Technologies Corporation Gas turbine engine airfoil with large thickness properties
SG10201505408WA (en) * 2014-07-24 2016-02-26 United Technologies Corp Gas turbine engine blade with variable density and wide chord tip
US20160160874A1 (en) * 2014-12-04 2016-06-09 Solar Turbines Incorporated Airfoil for inlet guide vane (igv) of multistage compressor
US20170138202A1 (en) * 2015-11-16 2017-05-18 General Electric Company Optimal lift designs for gas turbine engines
CN105298546B (zh) * 2015-11-27 2017-07-28 东方电气集团东方汽轮机有限公司 一种透平叶片叶身结构
US10526894B1 (en) * 2016-09-02 2020-01-07 United Technologies Corporation Short inlet with low solidity fan exit guide vane arrangements
IL249408A0 (en) 2016-12-06 2017-03-30 Medimop Medical Projects Ltd Liquid transfer device for use with infusion liquid container and pincers-like hand tool for use therewith for releasing intact drug vial therefrom
EP3358134B1 (en) * 2017-02-02 2021-07-14 General Electric Company Steam turbine with rotor blade
US20190106989A1 (en) * 2017-10-09 2019-04-11 United Technologies Corporation Gas turbine engine airfoil
CN109117552B (zh) * 2018-08-09 2022-04-12 东方电气集团东方汽轮机有限公司 一种涡轮机叶片变载荷流型设计方法
DE102019202388A1 (de) * 2019-02-21 2020-08-27 MTU Aero Engines AG Deckbandlose Schaufel für eine schnelllaufende Turbinenstufe
US11220910B2 (en) * 2019-07-26 2022-01-11 Pratt & Whitney Canada Corp. Compressor stator
KR102411655B1 (ko) * 2019-08-23 2022-06-21 두산에너빌리티 주식회사 베인과 이를 포함하는 압축기 및 가스 터빈
US11566530B2 (en) 2019-11-26 2023-01-31 General Electric Company Turbomachine nozzle with an airfoil having a circular trailing edge
US11629599B2 (en) 2019-11-26 2023-04-18 General Electric Company Turbomachine nozzle with an airfoil having a curvilinear trailing edge
US11286779B2 (en) * 2020-06-03 2022-03-29 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor
WO2022064674A1 (ja) * 2020-09-28 2022-03-31 三菱パワー株式会社 蒸気タービン

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DE560687C (de) * 1930-08-28 1932-10-06 Escher Wyss Maschf Ag Schaufelung fuer Dampf- und Gasturbinen
US2801790A (en) * 1950-06-21 1957-08-06 United Aircraft Corp Compressor blading
DE2034890A1 (de) * 1969-07-21 1971-02-04 Rolls Royce Ltd Derby, Derbyshire (Großbritannien) Schaufel fur Axialstromungsmaschinen
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
JPH08114199A (ja) * 1994-10-19 1996-05-07 Hitachi Ltd 軸流圧縮機
JP3867812B2 (ja) * 1995-07-17 2007-01-17 石川島播磨重工業株式会社 軸流圧縮機動翼
JPH10103002A (ja) * 1996-09-30 1998-04-21 Toshiba Corp 軸流流体機械用翼
JP3604533B2 (ja) * 1997-05-30 2004-12-22 株式会社東芝 軸流圧縮機用翼
US6312219B1 (en) * 1999-11-05 2001-11-06 General Electric Company Narrow waist vane
JP2002213206A (ja) * 2001-01-12 2002-07-31 Mitsubishi Heavy Ind Ltd ガスタービンにおける翼構造
US6508630B2 (en) * 2001-03-30 2003-01-21 General Electric Company Twisted stator vane
US6554572B2 (en) * 2001-05-17 2003-04-29 General Electric Company Gas turbine engine blade
US6554569B2 (en) * 2001-08-17 2003-04-29 General Electric Company Compressor outlet guide vane and diffuser assembly
US6851924B2 (en) * 2002-09-27 2005-02-08 Siemens Westinghouse Power Corporation Crack-resistance vane segment member
US7448455B2 (en) * 2004-11-04 2008-11-11 Smith International, Inc. Turbodrill with asymmetric stator and rotor vanes
US7686567B2 (en) * 2005-12-16 2010-03-30 United Technologies Corporation Airfoil embodying mixed loading conventions

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