| 发明名称 |
Internally cooled airfoil for a gas turbine engine and method |
| 摘要 |
An internally-cooled airfoil for a gas turbine engine, wherein the airfoil comprises at least one substantially chordwise-extending and internally-projecting stiffener located on an internal surface of one of the sidewalls and adjacent to the insert.
|
| 申请公布号 |
US2006120870(A1) |
申请公布日期 |
2006.06.08 |
| 申请号 |
US20040000957 |
申请日期 |
2004.12.02 |
| 申请人 |
TRINDADE RICARDO;PAPPLE MICHAEL L C;DJERIDANE TOUFIK;SREEKANTH SRI |
发明人 |
TRINDADE RICARDO;PAPPLE MICHAEL L.C.;DJERIDANE TOUFIK;SREEKANTH SRI |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
