发明名称 |
Composite airfoil and turbine engine |
摘要 |
A composite airfoil includes a core that has a three-dimensional network of fibers. The core defines an airfoil section and a root section. A composite skin covers a portion of the core excluding the root section. |
申请公布号 |
US9556742(B2) |
申请公布日期 |
2017.01.31 |
申请号 |
US201012955323 |
申请日期 |
2010.11.29 |
申请人 |
United Technologies Corporation |
发明人 |
Parkin Michael;Alexander Phillip;Klinetob Carl Brian |
分类号 |
F01D5/28;F01D5/14;B29C70/24;B32B5/26;B29D99/00 |
主分类号 |
F01D5/28 |
代理机构 |
Carlson, Gaskey & Olds, P.C. |
代理人 |
Carlson, Gaskey & Olds, P.C. |
主权项 |
1. A composite airfoil comprising:
a core including a three-dimensional network of fibers, the core defining an airfoil section and a root section; and a composite skin covering a portion of the core excluding the root section. |
地址 |
Hartford CT US |