发明名称 Gas turbine engine cooling air flow
摘要 A turbofan engine uses fan air to cool bounding surfaces of the exhaust duct at all times. A portion of the fan air flow is used for augmentor combustion in the augmentation mode. In the non-augmented mode the flow for combustion is stopped and the cooling air is used to cool the tail cone and exit guide vanes. Infrared radiation is thereby reduced when non-augmented.
申请公布号 US5157917(A) 申请公布日期 1992.10.27
申请号 US19910702477 申请日期 1991.05.20
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LIANG, GEORGE P.;BEAL, GEORGE W.;DILLARD, GARY J.
分类号 F02K1/82;F02K3/075;F02K3/11 主分类号 F02K1/82
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