| 发明名称 |
GEARED TURBOFAN WITH HIGH FAN ROTOR POWER INTENSITY |
| 摘要 |
<p>A gas turbine engine includes a fan rotating structure including a plurality of fan blades supported on a hub that defines a frontal area. A turbine section drives the fan through a geared architecture about the axis. The fan rotating structure includes a weight of the fan rotating structure relative to the frontal area that enables improvements in engine operating and propulsive efficiencies.</p> |
| 申请公布号 |
WO2014055113(A9) |
申请公布日期 |
2015.04.09 |
| 申请号 |
WO2013US29321 |
申请日期 |
2013.03.06 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FREDERICK M.;BIFULCO, ANTHONY R. |
| 分类号 |
F02K3/06;F02C3/04;F02C7/04;F02C7/36 |
主分类号 |
F02K3/06 |
| 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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