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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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