发明名称 Airfoil machining method and cutting tools
摘要 A method of machining an airfoil includes the steps of providing first and second cutting tools respectively having first and second cutting contours that are different than one another. A blank is cut with the first cutting tool to provide a first airfoil surface on a first blade. The blank is cut with the second cutting tool to provide a second airfoil surface on a second blade. An airfoil is produced having the first and second blades. A cutting tool for machining the airfoil includes a shank. A cutting surface adjoins the shank and provides a cutting contour corresponding to an airfoil surface. The cutting surface extends along a cutting length axially from a nose to near a cutting boundary. The cutting length is configured to be greater than the blade length.
申请公布号 US8826784(B2) 申请公布日期 2014.09.09
申请号 US201113219872 申请日期 2011.08.29
申请人 United Technologies Corporation 发明人 Wu Chung Y.
分类号 B23C3/18;B23C5/10;B26D3/00 主分类号 B23C3/18
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A method of machining an airfoil comprising the steps of: providing first and second cutting tools respectively having first and second cutting contours that are different than one another; cutting a blank with the first cutting tool to provide a first airfoil surface on a first blade; cutting the blank with the second cutting tool to provide a second airfoil surface on a second blade; and producing an airfoil having the first and second blades.
地址 Hartford CT US