| 发明名称 |
Maxmet Composites for Turbine Engine Component Tips |
| 摘要 |
A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix. |
| 申请公布号 |
US2016024955(A1) |
申请公布日期 |
2016.01.28 |
| 申请号 |
US201314775927 |
申请日期 |
2013.12.16 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Amini Shahram;Strock Christopher W;Burlatsky Sergei F;Novikov Dmitri;Fuller David Ulrich |
| 分类号 |
F01D11/12;F01D9/04;B23K1/00;B23K1/19;C23C24/04;B23K20/22;B23K26/34;B23K26/00;C23C4/12;F01D5/28;B23K20/02 |
主分类号 |
F01D11/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine system comprising:
a turbine engine component having an airfoil portion and a tip; said turbine engine component having a MAXMET composite bonded to said tip. |
| 地址 |
Hartford CT US |
