发明名称 |
Gas turbine engine with auxiliary fan |
摘要 |
A method of operating a propulsion system (14) includes powering an auxiliary fan (18) with a gas turbine engine (20), where the auxiliary fan (18) is along an auxiliary axis (F) and the gas turbine engine (20) is along an engine axis (F), the auxiliary axis (F) being parallel to the engine axis (A). |
申请公布号 |
EP2587039(A3) |
申请公布日期 |
2016.11.09 |
申请号 |
EP20120189326 |
申请日期 |
2012.10.19 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KUPRATIS, DANIEL B. |
分类号 |
F02K3/12;F02C3/107;F02C7/36;F02K3/077 |
主分类号 |
F02K3/12 |
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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