| 发明名称 |
TRANSIENT LIQUID PHASE BONDED TIP SHROUD |
| 摘要 |
A composite ceramic turbine blade includes a ceramic airfoil portion and a ceramic outer tip shroud portion. The ceramic outer tip shroud portion is joined to the ceramic airfoil portion by a bonding means. In an embodiment, the bonding means comprises partial transient liquid phase bonding. In another embodiment, the airfoil portion is a fiber reinforced ceramic. |
| 申请公布号 |
US2016032735(A1) |
申请公布日期 |
2016.02.04 |
| 申请号 |
US201414775535 |
申请日期 |
2014.03.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
McCaffrey Michael G.;Abbott Michael G.;Cook, III Grant O. |
| 分类号 |
F01D5/28;F01D5/14 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A composite ceramic turbine blade comprising:
a ceramic airfoil portion; and a ceramic outer tip shroud portion joined to the airfoil portion. |
| 地址 |
Hartford CT US |
