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 |
US2014086737(A1) |
申请公布日期 |
2014.03.27 |
申请号 |
US201213712155 |
申请日期 |
2012.12.12 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HYATT THOMAS B.;KLINETOB CARL BRIAN;LEROUX JASON |
分类号 |
F01D9/02 |
主分类号 |
F01D9/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|