JP2017122439A5 - - Google Patents

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Publication number
JP2017122439A5
JP2017122439A5 JP2016238971A JP2016238971A JP2017122439A5 JP 2017122439 A5 JP2017122439 A5 JP 2017122439A5 JP 2016238971 A JP2016238971 A JP 2016238971A JP 2016238971 A JP2016238971 A JP 2016238971A JP 2017122439 A5 JP2017122439 A5 JP 2017122439A5
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JP
Japan
Prior art keywords
blade
airfoil
throat
distribution
axial
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
JP2016238971A
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English (en)
Japanese (ja)
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JP2017122439A (ja
JP6929050B2 (ja
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Publication date
Priority claimed from US14/973,894 external-priority patent/US9957805B2/en
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Publication of JP2017122439A publication Critical patent/JP2017122439A/ja
Publication of JP2017122439A5 publication Critical patent/JP2017122439A5/ja
Application granted granted Critical
Publication of JP6929050B2 publication Critical patent/JP6929050B2/ja
Active legal-status Critical Current
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JP2016238971A 2015-12-18 2016-12-09 ターボ機械及びターボ機械用タービンブレード Active JP6929050B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/973,894 2015-12-18
US14/973,894 US9957805B2 (en) 2015-12-18 2015-12-18 Turbomachine and turbine blade therefor

Publications (3)

Publication Number Publication Date
JP2017122439A JP2017122439A (ja) 2017-07-13
JP2017122439A5 true JP2017122439A5 (enExample) 2021-07-29
JP6929050B2 JP6929050B2 (ja) 2021-09-01

Family

ID=58994626

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016238971A Active JP6929050B2 (ja) 2015-12-18 2016-12-09 ターボ機械及びターボ機械用タービンブレード

Country Status (5)

Country Link
US (1) US9957805B2 (enExample)
JP (1) JP6929050B2 (enExample)
CN (1) CN106948866B (enExample)
DE (1) DE102016124151A1 (enExample)
IT (1) IT201600127373A1 (enExample)

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US10655471B2 (en) * 2015-02-10 2020-05-19 Mitsubishi Hitachi Power Systems, Ltd. Turbine and gas turbine
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US10544681B2 (en) * 2015-12-18 2020-01-28 General Electric Company Turbomachine and turbine blade therefor
US9995144B2 (en) * 2016-02-18 2018-06-12 General Electric Company Turbine blade centroid shifting method and system
US10774650B2 (en) * 2017-10-12 2020-09-15 Raytheon Technologies Corporation Gas turbine engine airfoil
US11280199B2 (en) 2018-11-21 2022-03-22 Honeywell International Inc. Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution
US10859094B2 (en) 2018-11-21 2020-12-08 Honeywell International Inc. Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution
US20210381385A1 (en) * 2020-06-03 2021-12-09 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor
US11401816B1 (en) * 2021-04-30 2022-08-02 General Electric Company Compressor rotor blade airfoils
US11459892B1 (en) 2021-04-30 2022-10-04 General Electric Company Compressor stator vane airfoils
US11441427B1 (en) 2021-04-30 2022-09-13 General Electric Company Compressor rotor blade airfoils
US11326620B1 (en) 2021-04-30 2022-05-10 General Electric Company Compressor stator vane airfoils
US11293454B1 (en) 2021-04-30 2022-04-05 General Electric Company Compressor stator vane airfoils
CN115263804A (zh) 2021-04-30 2022-11-01 通用电气公司 压缩机转子叶片翼型件
US11480062B1 (en) 2021-04-30 2022-10-25 General Electric Company Compressor stator vane airfoils
US11519273B1 (en) * 2021-04-30 2022-12-06 General Electric Company Compressor rotor blade airfoils
US11519272B2 (en) * 2021-04-30 2022-12-06 General Electric Company Compressor rotor blade airfoils
US11414996B1 (en) 2021-04-30 2022-08-16 General Electric Company Compressor rotor blade airfoils
US11643932B2 (en) 2021-04-30 2023-05-09 General Electric Company Compressor rotor blade airfoils
GB202107128D0 (en) * 2021-05-19 2021-06-30 Rolls Royce Plc Nozzle guide vane
US11512595B1 (en) * 2022-02-04 2022-11-29 Pratt & Whitney Canada Corp. Turbine blade airfoil profile
US11867081B1 (en) * 2023-01-26 2024-01-09 Pratt & Whitney Canada Corp. Turbine blade airfoil profile
US12305529B1 (en) * 2024-05-21 2025-05-20 Ge Vernova Infrastructure Technology Llc Compressor stator vane airfoils

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