JP2004003486A5 - - Google Patents

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Publication number
JP2004003486A5
JP2004003486A5 JP2003144217A JP2003144217A JP2004003486A5 JP 2004003486 A5 JP2004003486 A5 JP 2004003486A5 JP 2003144217 A JP2003144217 A JP 2003144217A JP 2003144217 A JP2003144217 A JP 2003144217A JP 2004003486 A5 JP2004003486 A5 JP 2004003486A5
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JP
Japan
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.)
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Application number
JP2003144217A
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JP2004003486A (ja
JP4458772B2 (ja
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Priority claimed from US10/155,452 external-priority patent/US6932570B2/en
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Publication of JP2004003486A publication Critical patent/JP2004003486A/ja
Publication of JP2004003486A5 publication Critical patent/JP2004003486A5/ja
Application granted granted Critical
Publication of JP4458772B2 publication Critical patent/JP4458772B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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JP2003144217A 2002-05-23 2003-05-22 ガスタービンエンジンのエーロフォイルの有効寿命を延ばすための方法及び装置 Expired - Lifetime JP4458772B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/155,452 US6932570B2 (en) 2002-05-23 2002-05-23 Methods and apparatus for extending gas turbine engine airfoils useful life

Publications (3)

Publication Number Publication Date
JP2004003486A JP2004003486A (ja) 2004-01-08
JP2004003486A5 true JP2004003486A5 (ja) 2006-06-29
JP4458772B2 JP4458772B2 (ja) 2010-04-28

Family

ID=29400578

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003144217A Expired - Lifetime JP4458772B2 (ja) 2002-05-23 2003-05-22 ガスタービンエンジンのエーロフォイルの有効寿命を延ばすための方法及び装置

Country Status (4)

Country Link
US (1) US6932570B2 (ja)
EP (1) EP1365108A3 (ja)
JP (1) JP4458772B2 (ja)
CN (1) CN100572757C (ja)

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FR2898384B1 (fr) * 2006-03-08 2011-09-16 Snecma Aube mobile de turbomachine a cavite commune d'alimentation en air de refroidissement
US8622702B1 (en) 2010-04-21 2014-01-07 Florida Turbine Technologies, Inc. Turbine blade with cooling air inlet holes
US9017027B2 (en) 2011-01-06 2015-04-28 Siemens Energy, Inc. Component having cooling channel with hourglass cross section
US8764394B2 (en) 2011-01-06 2014-07-01 Siemens Energy, Inc. Component cooling channel
JP5713769B2 (ja) * 2011-04-07 2015-05-07 三菱重工業株式会社 シリンダジャケット
EP2535515A1 (en) 2011-06-16 2012-12-19 Siemens Aktiengesellschaft Rotor blade root section with cooling passage and method for supplying cooling fluid to a rotor blade
US8870525B2 (en) * 2011-11-04 2014-10-28 General Electric Company Bucket assembly for turbine system
US9243502B2 (en) 2012-04-24 2016-01-26 United Technologies Corporation Airfoil cooling enhancement and method of making the same
US9296039B2 (en) 2012-04-24 2016-03-29 United Technologies Corporation Gas turbine engine airfoil impingement cooling
JP6184172B2 (ja) 2013-05-29 2017-08-23 三菱日立パワーシステムズ株式会社 Ａｌコーティング方法とガスタービン翼の製造方法
US9777575B2 (en) * 2014-01-20 2017-10-03 Honeywell International Inc. Turbine rotor assemblies with improved slot cavities
EP3059394B1 (en) * 2015-02-18 2019-10-30 Ansaldo Energia Switzerland AG Turbine blade and set of turbine blades
US9733195B2 (en) * 2015-12-18 2017-08-15 General Electric Company System and method for inspecting turbine blades
FR3087479B1 (fr) 2018-10-23 2022-05-13 Safran Aircraft Engines Aube de turbomachine
US11021961B2 (en) * 2018-12-05 2021-06-01 General Electric Company Rotor assembly thermal attenuation structure and system
CN111156196B (zh) * 2020-01-10 2021-10-29 中国航空制造技术研究院 一种航空发动机风扇/压气机转子叶片结构及其设计方法

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US5498133A (en) * 1995-06-06 1996-03-12 General Electric Company Pressure regulated film cooling
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US6174135B1 (en) * 1999-06-30 2001-01-16 General Electric Company Turbine blade trailing edge cooling openings and slots
US6273678B1 (en) * 1999-08-11 2001-08-14 General Electric Company Modified diffusion aluminide coating for internal surfaces of gas turbine components
US6390774B1 (en) * 2000-02-02 2002-05-21 General Electric Company Gas turbine bucket cooling circuit and related process
EP1128023A1 (de) 2000-02-25 2001-08-29 Siemens Aktiengesellschaft Turbinenlaufschaufel
US6497920B1 (en) 2000-09-06 2002-12-24 General Electric Company Process for applying an aluminum-containing coating using an inorganic slurry mix
US6474946B2 (en) 2001-02-26 2002-11-05 United Technologies Corporation Attachment air inlet configuration for highly loaded single crystal turbine blades
US6485262B1 (en) * 2001-07-06 2002-11-26 General Electric Company Methods and apparatus for extending gas turbine engine airfoils useful life

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