| 发明名称 |
GAS TURBINE ENGINE |
| 摘要 |
A blade or a vane for a gas turbine engine. The blade or vane comprising an aerofoil and a leading edge member attached to the aerofoil. The leading edge comprises an electrically conductive support member and a nano-coating formed on the support member. |
| 申请公布号 |
US2017022826(A1) |
申请公布日期 |
2017.01.26 |
| 申请号 |
US201615204694 |
申请日期 |
2016.07.07 |
| 申请人 |
ROLLS-ROYCE plc |
发明人 |
READ Simon;RADOMSKI Steven A. |
| 分类号 |
F01D5/28;F01D9/02 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A blade or a vane for a gas turbine engine, the blade or vane comprising:
an aerofoil; and a leading edge member attached to the aerofoil; wherein the leading edge comprises an electrically conductive support member and a nano-crystalline metallic layer formed on the support member. |
| 地址 |
London GB |
