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