JP2003301702A5 - - Google Patents

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Publication number
JP2003301702A5
JP2003301702A5 JP2003076724A JP2003076724A JP2003301702A5 JP 2003301702 A5 JP2003301702 A5 JP 2003301702A5 JP 2003076724 A JP2003076724 A JP 2003076724A JP 2003076724 A JP2003076724 A JP 2003076724A JP 2003301702 A5 JP2003301702 A5 JP 2003301702A5
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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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JP2003076724A
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JP4315245B2 (ja
JP2003301702A (ja
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Priority claimed from US10/104,211 external-priority patent/US6769865B2/en
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Publication of JP2003301702A publication Critical patent/JP2003301702A/ja
Publication of JP2003301702A5 publication Critical patent/JP2003301702A5/ja
Application granted granted Critical
Publication of JP4315245B2 publication Critical patent/JP4315245B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2003076724A 2002-03-22 2003-03-20 バンド冷却式タービンノズル Expired - Fee Related JP4315245B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/104,211 2002-03-22
US10/104,211 US6769865B2 (en) 2002-03-22 2002-03-22 Band cooled turbine nozzle

Publications (3)

Publication Number Publication Date
JP2003301702A JP2003301702A (ja) 2003-10-24
JP2003301702A5 true JP2003301702A5 (ja) 2006-05-11
JP4315245B2 JP4315245B2 (ja) 2009-08-19

Family

ID=27788386

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003076724A Expired - Fee Related JP4315245B2 (ja) 2002-03-22 2003-03-20 バンド冷却式タービンノズル

Country Status (4)

Country Link
US (1) US6769865B2 (ja)
EP (1) EP1347152B1 (ja)
JP (1) JP4315245B2 (ja)
CN (1) CN100339560C (ja)

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US10132195B2 (en) * 2015-10-20 2018-11-20 General Electric Company Wheel space purge flow mixing chamber
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US20170198602A1 (en) * 2016-01-11 2017-07-13 General Electric Company Gas turbine engine with a cooled nozzle segment
US10689994B2 (en) * 2016-03-31 2020-06-23 General Electric Company Seal assembly to seal corner leaks in gas turbine
US10626797B2 (en) * 2017-02-15 2020-04-21 General Electric Company Turbine engine compressor with a cooling circuit
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