JP2007308798A5 - - Google Patents

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Publication number
JP2007308798A5
JP2007308798A5 JP2007127488A JP2007127488A JP2007308798A5 JP 2007308798 A5 JP2007308798 A5 JP 2007308798A5 JP 2007127488 A JP2007127488 A JP 2007127488A JP 2007127488 A JP2007127488 A JP 2007127488A JP 2007308798 A5 JP2007308798 A5 JP 2007308798A5
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JP
Japan
Prior art keywords
blade
airfoil
platform
turbine blade
fixing jig
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.)
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Application number
JP2007127488A
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English (en)
Japanese (ja)
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JP2007308798A (ja
JP5350603B2 (ja
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Publication date
Priority claimed from US11/383,783 external-priority patent/US20070267109A1/en
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Publication of JP2007308798A publication Critical patent/JP2007308798A/ja
Publication of JP2007308798A5 publication Critical patent/JP2007308798A5/ja
Application granted granted Critical
Publication of JP5350603B2 publication Critical patent/JP5350603B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2007127488A 2006-05-17 2007-05-14 超合金タービンブレードを熱処理するための固定治具の使用方法 Expired - Fee Related JP5350603B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/383,783 2006-05-17
US11/383,783 US20070267109A1 (en) 2006-05-17 2006-05-17 High pressure turbine airfoil recovery device and method of heat treatment

Publications (3)

Publication Number Publication Date
JP2007308798A JP2007308798A (ja) 2007-11-29
JP2007308798A5 true JP2007308798A5 (enExample) 2012-08-30
JP5350603B2 JP5350603B2 (ja) 2013-11-27

Family

ID=38420608

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007127488A Expired - Fee Related JP5350603B2 (ja) 2006-05-17 2007-05-14 超合金タービンブレードを熱処理するための固定治具の使用方法

Country Status (6)

Country Link
US (2) US20070267109A1 (enExample)
EP (1) EP1857217B1 (enExample)
JP (1) JP5350603B2 (enExample)
BR (1) BRPI0701724A (enExample)
CA (1) CA2587311C (enExample)
SG (3) SG137786A1 (enExample)

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US20180238173A1 (en) * 2017-02-22 2018-08-23 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US10625342B2 (en) 2017-02-22 2020-04-21 General Electric Company Method of repairing turbine component
US10717130B2 (en) 2017-02-22 2020-07-21 General Electric Company Method of manufacturing turbine airfoil and tip component thereof
US11154956B2 (en) 2017-02-22 2021-10-26 General Electric Company Method of repairing turbine component using ultra-thin plate
US10610933B2 (en) 2017-02-22 2020-04-07 General Electric Company Method of manufacturing turbine airfoil with open tip casting and tip component thereof
US10702958B2 (en) 2017-02-22 2020-07-07 General Electric Company Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature
US11371349B2 (en) 2019-04-05 2022-06-28 Raytheon Technologies Corporation Gas impingement in-process cooling system
US11242588B2 (en) * 2019-12-12 2022-02-08 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
US11199101B2 (en) 2019-12-12 2021-12-14 General Electric Company System and method to apply multiple thermal treatments to workpiece and related turbomachine components
CN111575671B (zh) * 2020-06-12 2022-03-29 中国人民解放军空军工程大学 用于叶片表面选区制备涂层的夹具及涂层的制备方法
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US11828190B2 (en) 2021-11-18 2023-11-28 General Electric Company Airfoil joining apparatus and methods
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