JP2002139220A5 - - Google Patents

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Publication number
JP2002139220A5
JP2002139220A5 JP2001305905A JP2001305905A JP2002139220A5 JP 2002139220 A5 JP2002139220 A5 JP 2002139220A5 JP 2001305905 A JP2001305905 A JP 2001305905A JP 2001305905 A JP2001305905 A JP 2001305905A JP 2002139220 A5 JP2002139220 A5 JP 2002139220A5
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JP
Japan
Prior art keywords
cooling
group
hole
holes
combustor
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.)
Granted
Application number
JP2001305905A
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English (en)
Japanese (ja)
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JP4124585B2 (ja
JP2002139220A (ja
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Publication date
Priority claimed from US09/678,069 external-priority patent/US6408629B1/en
Application filed filed Critical
Publication of JP2002139220A publication Critical patent/JP2002139220A/ja
Publication of JP2002139220A5 publication Critical patent/JP2002139220A5/ja
Application granted granted Critical
Publication of JP4124585B2 publication Critical patent/JP4124585B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001305905A 2000-10-03 2001-10-02 選択的に傾斜させた冷却孔を有する燃焼器ライナ Expired - Fee Related JP4124585B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/678,069 US6408629B1 (en) 2000-10-03 2000-10-03 Combustor liner having preferentially angled cooling holes
US09/678069 2000-10-03

Publications (3)

Publication Number Publication Date
JP2002139220A JP2002139220A (ja) 2002-05-17
JP2002139220A5 true JP2002139220A5 (enExample) 2005-04-21
JP4124585B2 JP4124585B2 (ja) 2008-07-23

Family

ID=24721244

Family Applications (1)

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JP2001305905A Expired - Fee Related JP4124585B2 (ja) 2000-10-03 2001-10-02 選択的に傾斜させた冷却孔を有する燃焼器ライナ

Country Status (3)

Country Link
US (1) US6408629B1 (enExample)
EP (1) EP1195559B1 (enExample)
JP (1) JP4124585B2 (enExample)

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US9897320B2 (en) * 2009-07-30 2018-02-20 Honeywell International Inc. Effusion cooled dual wall gas turbine combustors
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US9625151B2 (en) * 2012-09-25 2017-04-18 United Technologies Corporation Cooled combustor liner grommet
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US9482432B2 (en) 2012-09-26 2016-11-01 United Technologies Corporation Gas turbine engine combustor with integrated combustor vane having swirler
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JP7458370B2 (ja) 2018-07-23 2024-03-29 ８ リバーズ キャピタル，エルエルシー 無炎燃焼による発電のためのシステムおよび方法
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