发明名称 |
STRUCTURAL GUIDE VANE INTERNAL TOPOLOGY |
摘要 |
A disclosed structural guide vane for a gas turbine engine includes a strut defining a plurality of channels and a cover attached over the plurality of channels. The strut includes a first side defining a first surface of an airfoil and a second side including a plurality of channels. At least one of the plurality of channels defines a wall thickness of a portion of the first side that varies in a chord wise direction. |
申请公布号 |
WO2014052597(A1) |
申请公布日期 |
2014.04.03 |
申请号 |
WO2013US61929 |
申请日期 |
2013.09.26 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HYATT, THOMAS B.;KLINETOB, CARL BRIAN;LEROUX, JASON |
分类号 |
F01D9/02;F02C7/00;F02K3/02 |
主分类号 |
F01D9/02 |
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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