发明名称 Gas turbine exhaust assembly
摘要 An exhaust device is disclosed that includes a duct that turns an exhaust flow from a gas turbine engine from a first direction to a second direction. A diverter cup is disposed within the duct and serves to split the exhaust flow into two streams as well as introduce cooling air through an ejector pump at the downstream end of the diverter cup. A splitter is disposed downstream of the diverter cup and serves to split the cooling air into two streams which are thereafter mixed with the split exhaust flow. A diffuser is created in the exhaust device between the duct and the splitter. Various cooling slots are also provided in the duct.
申请公布号 US8322126(B2) 申请公布日期 2012.12.04
申请号 US20080154510 申请日期 2008.05.23
申请人 BIES CHRISTOPHER J.;BERGERON STEPHEN A.;LERG BRYAN H.;DEJULIO EMIL R.;ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. 发明人 BIES CHRISTOPHER J.;BERGERON STEPHEN A.;LERG BRYAN H.;DEJULIO EMIL R.
分类号 F02C7/08;F02G1/00 主分类号 F02C7/08
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