| 发明名称 |
METHOD FOR ASSEMBLING GAS TURBINE ENGINE COMPONENTS |
| 摘要 |
Method for assembling into turbine sets turbine components having internal cooling passages. The turbine components are classified according to flow capability through the internal cooling passages and turbine sets are assembled in which the turbine components have the same flow capability classification. |
| 申请公布号 |
SG112093(A1) |
申请公布日期 |
2005.06.29 |
| 申请号 |
SG20040007166 |
申请日期 |
2004.11.19 |
| 申请人 |
MASSACHUSETTS INSTITUTE OF TECHNOLOGY;UNITED TECHNOLOGIES CORPORATION |
发明人 |
CARROLL V. SIDWELL;DAVID L. DARMOFAL |
| 分类号 |
F01D25/00;F01D5/18;F02C7/00 |
主分类号 |
F01D25/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
