发明名称 |
BIFURCATED AIR INLET HOUSING FOR A GAS TURBINE ENGINE |
摘要 |
A gas turbine engine has a nose cone with a nose cone upstream end and an inlet housing including a plurality of separate flow paths at a housing upstream end which is downstream of the nose cone upstream end. The inlet housing includes a mixing portion downstream of the housing upstream end which mixes airflow from the separate flow paths, such that the airflow is generally around 360 degrees of a rotational axis of the gas turbine engine. A rotor and a turbine drive a shaft to drive the rotor with the shaft including a bearing mounted at a location downstream of the nose cone upstream end. |
申请公布号 |
WO2014165364(A1) |
申请公布日期 |
2014.10.09 |
申请号 |
WO2014US31828 |
申请日期 |
2014.03.26 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
JONES, ANTHONY C.;LYDON, PATRICK M.;THAYALAKHANDAN, NAGAMANY;ALEXANDER, ERIC J. |
分类号 |
F02C7/04;F02C7/057;F02C7/06;F02C9/16 |
主分类号 |
F02C7/04 |
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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