| 发明名称 |
VARIABLE FAN INLET GUIDE VANE FOR TURBINE ENGINE |
| 摘要 |
<p>A turbine engine includes a compressor section, a combustor arranged in fluid-receiving communication with the compressor section, a turbine section arranged in fluid-receiving communication with the combustor and a gearbox assembly coupled to be driven by the turbine section. The gearbox assembly is located at an axial position that is aft of the compressor section.</p> |
| 申请公布号 |
SG11201402892V(A) |
申请公布日期 |
2014.10.30 |
| 申请号 |
SG11201402892V |
申请日期 |
2012.12.26 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MERRY, BRIAN;SUCIU, GABRIEL L.;NORRIS, JAMES W.;SIRICA, STEVEN J.;SCHWARZ, FREDERICK M. |
| 分类号 |
F02K3/02;F02C3/04;F02C3/073 |
主分类号 |
F02K3/02 |
| 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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