| 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 |
EP2971560(A2) |
申请公布日期 |
2016.01.20 |
| 申请号 |
EP20130878721 |
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;FURRER, DAVID ULRICH |
| 分类号 |
F01D5/28;B23K1/00;B23K1/19;B23K20/02;B23K20/22;B23K26/00;B23K26/34;B23K103/16;C04B35/56;C04B35/58;C04B41/51;C23C24/04;F01D5/14;F01D9/04;F01D11/12;F01D11/20;F02C7/30 |
主分类号 |
F01D5/28 |
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