JP2004257390A5 - - Google Patents

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Publication number
JP2004257390A5
JP2004257390A5 JP2004050705A JP2004050705A JP2004257390A5 JP 2004257390 A5 JP2004257390 A5 JP 2004257390A5 JP 2004050705 A JP2004050705 A JP 2004050705A JP 2004050705 A JP2004050705 A JP 2004050705A JP 2004257390 A5 JP2004257390 A5 JP 2004257390A5
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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
JP2004050705A
Other versions
JP4559751B2 (ja
JP2004257390A (ja
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Publication date
Priority claimed from US10/375,415 external-priority patent/US7008185B2/en
Application filed filed Critical
Publication of JP2004257390A publication Critical patent/JP2004257390A/ja
Publication of JP2004257390A5 publication Critical patent/JP2004257390A5/ja
Application granted granted Critical
Publication of JP4559751B2 publication Critical patent/JP4559751B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2004050705A 2003-02-27 2004-02-26 ガスタービンエンジンのタービンノズルの二又状インピンジメントバッフル Expired - Fee Related JP4559751B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/375,415 US7008185B2 (en) 2003-02-27 2003-02-27 Gas turbine engine turbine nozzle bifurcated impingement baffle

Publications (3)

Publication Number Publication Date
JP2004257390A JP2004257390A (ja) 2004-09-16
JP2004257390A5 true JP2004257390A5 (ja) 2007-04-12
JP4559751B2 JP4559751B2 (ja) 2010-10-13

Family

ID=32771457

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004050705A Expired - Fee Related JP4559751B2 (ja) 2003-02-27 2004-02-26 ガスタービンエンジンのタービンノズルの二又状インピンジメントバッフル

Country Status (4)

Country Link
US (1) US7008185B2 (ja)
EP (1) EP1452690A3 (ja)
JP (1) JP4559751B2 (ja)
CN (2) CN102251814B (ja)

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US10787912B2 (en) 2018-04-25 2020-09-29 Raytheon Technologies Corporation Spiral cavities for gas turbine engine components
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US10883376B2 (en) * 2019-02-01 2021-01-05 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite vanes
US10767493B2 (en) * 2019-02-01 2020-09-08 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite vanes
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