JP2001193692A5 - - Google Patents

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Publication number
JP2001193692A5
JP2001193692A5 JP2000369362A JP2000369362A JP2001193692A5 JP 2001193692 A5 JP2001193692 A5 JP 2001193692A5 JP 2000369362 A JP2000369362 A JP 2000369362A JP 2000369362 A JP2000369362 A JP 2000369362A JP 2001193692 A5 JP2001193692 A5 JP 2001193692A5
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JP
Japan
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JP2000369362A
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JP2001193692A (ja
JP4771585B2 (ja
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Priority claimed from US09/455,826 external-priority patent/US6331100B1/en
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Publication of JP2001193692A publication Critical patent/JP2001193692A/ja
Publication of JP2001193692A5 publication Critical patent/JP2001193692A5/ja
Application granted granted Critical
Publication of JP4771585B2 publication Critical patent/JP4771585B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2000369362A 1999-12-06 2000-12-05 二重に湾曲した圧縮機翼形部 Expired - Fee Related JP4771585B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/455,826 US6331100B1 (en) 1999-12-06 1999-12-06 Doubled bowed compressor airfoil
US09/455826 1999-12-06

Publications (3)

Publication Number Publication Date
JP2001193692A JP2001193692A (ja) 2001-07-17
JP2001193692A5 true JP2001193692A5 (ja) 2008-01-31
JP4771585B2 JP4771585B2 (ja) 2011-09-14

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JP2000369362A Expired - Fee Related JP4771585B2 (ja) 1999-12-06 2000-12-05 二重に湾曲した圧縮機翼形部

Country Status (9)

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US (1) US6331100B1 (ja)
EP (1) EP1106836B1 (ja)
JP (1) JP4771585B2 (ja)
KR (1) KR100827055B1 (ja)
CN (1) CN1311144C (ja)
CA (1) CA2326424C (ja)
DE (1) DE60039957D1 (ja)
PL (1) PL196777B1 (ja)
RU (1) RU2228461C2 (ja)

Families Citing this family (132)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6709239B2 (en) * 2001-06-27 2004-03-23 Bharat Heavy Electricals Ltd. Three dimensional blade
JP3836050B2 (ja) * 2002-06-07 2006-10-18 三菱重工業株式会社 タービン動翼
JP4318940B2 (ja) * 2002-10-08 2009-08-26 本田技研工業株式会社 圧縮機翼型
KR100484825B1 (ko) * 2002-11-22 2005-04-22 엘지전자 주식회사 축류팬
FR2851798B1 (fr) * 2003-02-27 2005-04-29 Snecma Moteurs Aube en fleche de turboreacteur
FR2853022B1 (fr) * 2003-03-27 2006-07-28 Snecma Moteurs Aube de redresseur a double courbure
US20040243360A1 (en) * 2003-05-30 2004-12-02 General Electric Company Persistent compressor airfoils
US6899526B2 (en) * 2003-08-05 2005-05-31 General Electric Company Counterstagger compressor airfoil
EP1582696A1 (de) * 2004-03-30 2005-10-05 Siemens Aktiengesellschaft Verdichterschaufel und ein Verfahren zum Konstruieren einer Verdichterschaufel
US7024744B2 (en) * 2004-04-01 2006-04-11 General Electric Company Frequency-tuned compressor stator blade and related method
US7204676B2 (en) * 2004-05-14 2007-04-17 Pratt & Whitney Canada Corp. Fan blade curvature distribution for high core pressure ratio fan
US7186090B2 (en) * 2004-08-05 2007-03-06 General Electric Company Air foil shape for a compressor blade
DE102004054752A1 (de) 2004-11-12 2006-05-18 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe
US7476086B2 (en) * 2005-04-07 2009-01-13 General Electric Company Tip cambered swept blade
US7374403B2 (en) * 2005-04-07 2008-05-20 General Electric Company Low solidity turbofan
CH698109B1 (de) * 2005-07-01 2009-05-29 Alstom Technology Ltd Turbomaschinenschaufel.
DE102005042115A1 (de) 2005-09-05 2007-03-08 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit blockweise definierter Profilskelettlinie
DE102005060699A1 (de) 2005-12-19 2007-06-21 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Verstellstator
US7517190B2 (en) * 2006-10-25 2009-04-14 General Electric Company Airfoil shape for a compressor
US7534093B2 (en) * 2006-10-25 2009-05-19 General Electric Company Airfoil shape for a compressor
US7572104B2 (en) * 2006-10-25 2009-08-11 General Electric Company Airfoil shape for a compressor
US7572105B2 (en) * 2006-10-25 2009-08-11 General Electric Company Airfoil shape for a compressor
US7534092B2 (en) * 2006-10-25 2009-05-19 General Electric Company Airfoil shape for a compressor
US7566202B2 (en) * 2006-10-25 2009-07-28 General Electric Company Airfoil shape for a compressor
US7513749B2 (en) * 2006-10-25 2009-04-07 General Electric Company Airfoil shape for a compressor
US7540715B2 (en) * 2006-10-25 2009-06-02 General Electric Company Airfoil shape for a compressor
US7494322B2 (en) * 2006-10-25 2009-02-24 General Electric Company Airfoil shape for a compressor
US7494321B2 (en) * 2006-10-25 2009-02-24 General Electric Company Airfoil shape for a compressor
US7534094B2 (en) * 2006-10-25 2009-05-19 General Electric Company Airfoil shape for a compressor
US7517196B2 (en) * 2006-10-25 2009-04-14 General Electric Company Airfoil shape for a compressor
US7513748B2 (en) * 2006-10-25 2009-04-07 General Electric Company Airfoil shape for a compressor
US7517188B2 (en) * 2006-10-25 2009-04-14 General Electric Company Airfoil shape for a compressor
US7537434B2 (en) * 2006-11-02 2009-05-26 General Electric Company Airfoil shape for a compressor
US7497665B2 (en) * 2006-11-02 2009-03-03 General Electric Company Airfoil shape for a compressor
JP4664890B2 (ja) * 2006-11-02 2011-04-06 三菱重工業株式会社 遷音速翼及び軸流回転機
US7568892B2 (en) * 2006-11-02 2009-08-04 General Electric Company Airfoil shape for a compressor
US7524170B2 (en) * 2006-11-02 2009-04-28 General Electric Company Airfoil shape for a compressor
US7537435B2 (en) * 2006-11-02 2009-05-26 General Electric Company Airfoil shape for a compressor
FR2908152B1 (fr) * 2006-11-08 2009-02-06 Snecma Sa Aube en fleche de turbomachine
US8292574B2 (en) 2006-11-30 2012-10-23 General Electric Company Advanced booster system
US7967571B2 (en) * 2006-11-30 2011-06-28 General Electric Company Advanced booster rotor blade
US8087884B2 (en) * 2006-11-30 2012-01-03 General Electric Company Advanced booster stator vane
US7806653B2 (en) * 2006-12-22 2010-10-05 General Electric Company Gas turbine engines including multi-curve stator vanes and methods of assembling the same
US7794201B2 (en) * 2006-12-22 2010-09-14 General Electric Company Gas turbine engines including lean stator vanes and methods of assembling the same
JP4659008B2 (ja) * 2007-09-13 2011-03-30 ルネサスエレクトロニクス株式会社 ホスト負荷調整機能付周辺回路
DE102008055824B4 (de) * 2007-11-09 2016-08-11 Alstom Technology Ltd. Dampfturbine
CN101182784B (zh) * 2007-12-03 2011-05-11 南京航空航天大学 应用于航空发动机的风扇/压气机的转子超声叶型的设计方法
EP2133573B1 (en) * 2008-06-13 2011-08-17 Siemens Aktiengesellschaft Vane or blade for an axial flow compressor
US8147207B2 (en) * 2008-09-04 2012-04-03 Siemens Energy, Inc. Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion
US8480372B2 (en) * 2008-11-06 2013-07-09 General Electric Company System and method for reducing bucket tip losses
US8167567B2 (en) * 2008-12-17 2012-05-01 United Technologies Corporation Gas turbine engine airfoil
US8202051B2 (en) 2009-02-03 2012-06-19 Ronald Paul Ackerman Turbine apparatus
EP2241761A1 (en) * 2009-04-09 2010-10-20 Alstom Technology Ltd Blade for an Axial Compressor and Manufacturing Method Thereof
EA015948B1 (ru) * 2009-07-20 2011-12-30 Феликс Мубаракович Давлетшин Лопасть вентилятора градирни
EA015947B1 (ru) * 2009-07-20 2011-12-30 Феликс Мубаракович Давлетшин Лопасть вентилятора градирни
EP2299124A1 (de) * 2009-09-04 2011-03-23 Siemens Aktiengesellschaft Verdichterlaufschaufel für einen Axialverdichter
EA015968B1 (ru) * 2009-10-12 2012-01-30 Феликс Мубаракович Давлетшин Лопасть вентилятора градирни
US8523531B2 (en) * 2009-12-23 2013-09-03 Alstom Technology Ltd Airfoil for a compressor blade
US9291059B2 (en) 2009-12-23 2016-03-22 Alstom Technology Ltd. Airfoil for a compressor blade
DE102010009615B4 (de) * 2010-02-27 2016-11-17 MTU Aero Engines AG Schaufelblatt mit gefädelten Profilschnitten
GB2483061A (en) * 2010-08-23 2012-02-29 Rolls Royce Plc A method of damping aerofoil structure vibrations
FR2969230B1 (fr) * 2010-12-15 2014-11-21 Snecma Aube de compresseur a loi d'empilage amelioree
US9309769B2 (en) 2010-12-28 2016-04-12 Rolls-Royce Corporation Gas turbine engine airfoil shaped component
CN102032214B (zh) * 2010-12-30 2012-07-04 北京理工大学 一种抑制分离的叶片前缘改型方法
US8702384B2 (en) * 2011-03-01 2014-04-22 General Electric Company Airfoil core shape for a turbomachine component
FR2983234B1 (fr) * 2011-11-29 2014-01-17 Snecma Aube pour disque aubage monobloc de turbomachine
CN102536327B (zh) * 2011-12-07 2014-09-10 北京航空航天大学 一种兼顾气动与结构特征的航空发动机风扇叶片三维几何结构
FR2989107B1 (fr) * 2012-04-04 2017-03-31 Snecma Aube de rotor de turbomachine
FR2993020B1 (fr) * 2012-07-06 2016-03-18 Snecma Redresseur de turbomachine avec aubes a profil ameliore
FR2993323B1 (fr) * 2012-07-12 2014-08-15 Snecma Aube de turbomachine ayant un profil configure de maniere a obtenir des proprietes aerodynamiques et mecaniques ameliorees
CN104471317B (zh) 2012-08-06 2016-09-07 西门子公司 在带有具有在外部区域内交叉的叶片端部的旋流生成器的燃烧器内的空气和燃料混合的局部改进
GB201217482D0 (en) * 2012-10-01 2012-11-14 Rolls Royce Plc Aerofoil for axial-flow machine
WO2014058478A1 (en) 2012-10-09 2014-04-17 United Technologies Corporation Geared low fan pressure ratio fan exit guide vane stagger angle
CN103148015B (zh) * 2013-01-15 2015-09-09 南京航空航天大学 尾缘负载荷扩压式叶轮机叶片
USD748054S1 (en) * 2013-02-19 2016-01-26 Tnp Co., Ltd. Wind turbine blade
US10221707B2 (en) 2013-03-07 2019-03-05 Pratt & Whitney Canada Corp. Integrated strut-vane
CN103498812A (zh) * 2013-05-23 2014-01-08 哈尔滨汽轮机厂有限责任公司 一种燃气轮机用压气机的低压中间级动叶片
CN103498813B (zh) * 2013-05-23 2016-08-10 哈尔滨汽轮机厂有限责任公司 一种20-30mw等级燃气轮机用压气机的低压首级动叶片
US9835038B2 (en) 2013-08-07 2017-12-05 Pratt & Whitney Canada Corp. Integrated strut and vane arrangements
EP3108121B1 (en) 2014-02-19 2023-09-06 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
US9163517B2 (en) 2014-02-19 2015-10-20 United Technologies Corporation Gas turbine engine airfoil
US10570915B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
US10584715B2 (en) 2014-02-19 2020-03-10 United Technologies Corporation Gas turbine engine airfoil
US10570916B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015175073A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126449A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126824A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126452A1 (en) * 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126450A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
WO2015127032A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108123B1 (en) * 2014-02-19 2023-10-04 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
US10605259B2 (en) 2014-02-19 2020-03-31 United Technologies Corporation Gas turbine engine airfoil
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
US10519971B2 (en) 2014-02-19 2019-12-31 United Technologies Corporation Gas turbine engine airfoil
US10393139B2 (en) 2014-02-19 2019-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015175043A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3108122B1 (en) 2014-02-19 2023-09-20 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
EP3108117B2 (en) 2014-02-19 2023-10-11 Raytheon Technologies Corporation Gas turbine engine airfoil
WO2015175044A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
US9765795B2 (en) 2014-08-27 2017-09-19 Pratt & Whitney Canada Corp. Compressor rotor airfoil
US10443390B2 (en) * 2014-08-27 2019-10-15 Pratt & Whitney Canada Corp. Rotary airfoil
EP3051142B1 (de) 2015-01-28 2017-10-11 MTU Aero Engines GmbH Gasturbinen-axialverdichter
US9470093B2 (en) * 2015-03-18 2016-10-18 United Technologies Corporation Turbofan arrangement with blade channel variations
US9909434B2 (en) 2015-07-24 2018-03-06 Pratt & Whitney Canada Corp. Integrated strut-vane nozzle (ISV) with uneven vane axial chords
FR3040071B1 (fr) * 2015-08-11 2020-03-27 Safran Aircraft Engines Aube de rotor de turbomachine
GB201519946D0 (en) * 2015-11-12 2015-12-30 Rolls Royce Plc Compressor
DE102015224096A1 (de) * 2015-12-02 2017-06-08 Mahle International Gmbh Lüfterrad für einen Axiallüfter
US10221859B2 (en) 2016-02-08 2019-03-05 General Electric Company Turbine engine compressor blade
US10443451B2 (en) 2016-07-18 2019-10-15 Pratt & Whitney Canada Corp. Shroud housing supported by vane segments
JP6414197B2 (ja) * 2016-12-28 2018-10-31 ダイキン工業株式会社 軸流ファンおよび送風ユニット
CN107237777B (zh) * 2017-08-01 2023-10-27 中国农业大学 一种农用通风机弯掠叶片及其设计方法
KR102000281B1 (ko) 2017-10-11 2019-07-15 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
CN107965352A (zh) * 2017-12-26 2018-04-27 北京全四维动力科技有限公司 能降低水蚀危险性的弯叶片、采用其的叶栅及工业汽轮机
USD911512S1 (en) 2018-01-31 2021-02-23 Carrier Corporation Axial flow fan
US20190234419A1 (en) * 2018-01-31 2019-08-01 Carrier Corporation Axial fan with tip fences
JP6953322B2 (ja) * 2018-02-01 2021-10-27 本田技研工業株式会社 ファンブレードの形状決定方法
EP3760875B1 (en) * 2018-06-22 2022-06-15 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Rotor and centrifugal compression machine provided with said rotor
US10711615B2 (en) * 2018-08-21 2020-07-14 Chromalloy Gas Turbine Llc First stage turbine blade
WO2020095470A1 (ja) 2018-11-05 2020-05-14 株式会社Ihi 軸流流体機械の動翼
JP7032708B2 (ja) 2019-03-26 2022-03-09 株式会社Ihi 軸流タービンの静翼セグメント
CN110130995B (zh) * 2019-05-31 2023-10-20 南京赛达科技有限公司 一种高强度汽轮机叶片及其制备方法
DE102019210880A1 (de) * 2019-07-23 2021-01-28 MTU Aero Engines AG Laufschaufel für eine strömungsmaschine
RU195347U1 (ru) * 2019-09-16 2020-01-23 Акционерное общество (АО) "Научно-исследовательский институт "Лопастных машин" ("НИИ ЛМ") Рабочее колесо лопастной машины с радиальными наборными лопатками
CN111156195B (zh) * 2020-01-07 2023-11-17 哈尔滨工程大学 一种压气机叶片前缘结构
US11371354B2 (en) 2020-06-03 2022-06-28 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor
US11286779B2 (en) * 2020-06-03 2022-03-29 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor
FR3115322B1 (fr) * 2020-10-20 2022-10-14 Safran Aircraft Engines Aube de soufflante à dièdre nul en tête
CN114856831B (zh) 2021-02-03 2024-06-28 和谐工业有限责任公司 带成形轮叶的空气涡轮起动器
CN113439699B (zh) * 2021-06-03 2022-10-04 浙江海洋大学 一种深海智慧渔场养殖的阻流装置
CN114046269B (zh) * 2022-01-11 2022-05-03 中国航发上海商用航空发动机制造有限责任公司 轴流压气机的转子叶片及其设计方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663493A (en) 1949-04-26 1953-12-22 A V Roe Canada Ltd Blading for compressors, turbines, and the like
US3745629A (en) * 1972-04-12 1973-07-17 Secr Defence Method of determining optimal shapes for stator blades
US4585395A (en) 1983-12-12 1986-04-29 General Electric Company Gas turbine engine blade
US4682935A (en) 1983-12-12 1987-07-28 General Electric Company Bowed turbine blade
FR2603953B1 (fr) * 1986-09-12 1991-02-22 Peugeot Aciers Et Outillage Pale profilee d'helice et son application aux motoventilateurs
FR2643940B1 (fr) * 1989-03-01 1991-05-17 Snecma Aube mobile de turbomachine a moment de pied compense
US5088892A (en) 1990-02-07 1992-02-18 United Technologies Corporation Bowed airfoil for the compression section of a rotary machine
JP2753382B2 (ja) 1990-09-17 1998-05-20 株式会社日立製作所 軸流タービン静翼装置及び軸流タービン
US5641268A (en) 1991-09-17 1997-06-24 Rolls-Royce Plc Aerofoil members for gas turbine engines
DE4228879A1 (de) 1992-08-29 1994-03-03 Asea Brown Boveri Axialdurchströmte Turbine
GB9417406D0 (en) 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
JPH08312303A (ja) * 1995-05-18 1996-11-26 Mitsubishi Heavy Ind Ltd 軸流圧縮機静翼のカーブドスタッキング方法
GB9607316D0 (en) * 1996-04-09 1996-06-12 Rolls Royce Plc Swept fan blade
US6071077A (en) * 1996-04-09 2000-06-06 Rolls-Royce Plc Swept fan blade
ITTO980276A1 (it) * 1998-03-30 1999-09-30 Gate Spa Ventola assiale, particolarmente per autoveicoli.
US6299412B1 (en) * 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil

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