发明名称 SYSTEM FOR COOLING A HOT GAS COMPONENT FOR A COMBUSTOR OF A GAS TURBINE
摘要 A system for cooling a hot gas path component for a combustor generally includes an impingement sleeve that circumferentially surrounds an outer surface of the hot gas path component. A first cooling chamber is defined between the impingement sleeve and a first portion of the outer surface of the hot gas path component. A second cooling chamber is disposed downstream from the first cooling chamber. The second cooling chamber is defined between the impingement sleeve and a second portion of the outer surface of hot gas path component. An inlet extends through the impingement sleeve so as to define a first flow path into the first cooling chamber. An outlet defines a second flow path between the first cooling chamber and the second cooling chamber.
申请公布号 US2014130504(A1) 申请公布日期 2014.05.15
申请号 US201213674255 申请日期 2012.11.12
申请人 GENERAL ELECTRIC COMPANY 发明人 CHEN WEI;WASHAM ROY MARSHALL
分类号 F23R3/00 主分类号 F23R3/00
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