GAS TURBINE COMBUSTOR AND STEAM INJECTED GAS TURBINE

A gas turbine combustor includes: a tubular combustion liner (11) that has a plurality of dilution holes (22) disposed circumferentially at a section downstream in a direction of flow of combustion gas (105); a combustor casing (12) that encloses the combustion liner (11); a liner flow sleeve (16) d...

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Bibliographische Detailangaben
1. Verfasser: KOGANEZAWA, TOMOMI
Format: Patent
Sprache:eng ; fre ; ger
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