| 发明名称 |
ROTOR BLADE MANUFACTURE |
| 摘要 |
A method is provided of processing one or more blades of a row of blades which forms part of a rotor for a gas turbine engine. The method includes: providing a rotor disc having a slot for mounting one or more blades; applying tape at one or both sides of the slot such that when the blades are loaded in the slot the tape reduces a range of tilt angles which can be adopted by the blades; loading the blades in the slot; and performing a processing operation on the loaded blades. |
| 申请公布号 |
US2015369050(A1) |
申请公布日期 |
2015.12.24 |
| 申请号 |
US201514725785 |
申请日期 |
2015.05.29 |
| 申请人 |
Rolls-Royce plc |
发明人 |
RAVEN Gemma Alexandra;TAYLOR Christopher Jonathan;MAY Alexander David;BAIRD Andrew Alan Robert |
| 分类号 |
F01D5/14;F01D5/30;F01D5/28;F01D5/02 |
主分类号 |
F01D5/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of processing one or more blades of a row of blades which forms part of a rotor for a gas turbine engine, the method including:
providing a rotor disc having a slot for mounting one or more blades; applying tape at one or both sides of the slot such that when the blades are loaded in the slot the tape reduces the range of tilt angles which can be adopted by the blades; loading the blades in the slot; performing a processing operation on the loaded blades; and removing the tape from the disc after the processing operation. |
| 地址 |
London GB |
