| 发明名称 |
Coated transition duct for a gas turbine |
| 摘要 |
A gas turbine hot gas inlet manifold consists of a heat and corrosion resistant metal substrate (9) with interior and exterior high temperature corrosion and oxidation protective layers (4). The metal substrate consists of a nickel base alloy and the high temperature corrosion and oxidation protective layers consist of MCrAlY containing 31% Cr, 11% Al and 0.6% Y. |
| 申请公布号 |
EP0949410(A3) |
申请公布日期 |
2000.11.02 |
| 申请号 |
EP19990103176 |
申请日期 |
1999.02.18 |
| 申请人 |
MAN TURBOMASCHINEN AG GHH BORSIG |
发明人 |
CHANDRA, SHARAD DR.-ING.;ELLERMANN, BERTOLD DIPL.-ING.;GATHMANN, HEINZ DIPL.-ING.;SCHNIEDERS, WERNER DIPL.-ING. |
| 分类号 |
F02C7/00;F01D5/28;F01D9/02 |
主分类号 |
F02C7/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
