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 |