发明名称 |
СПОСОБ ИЗГОТОВЛЕНИЯ ЛОПАТКИ И ЭЛЕМЕНТА ГАЗОВОЙ ТУРБИНЫ |
摘要 |
Method for manufacturing a vane ( 1 ) to a gas turbine component intended for guiding a gas flow. The vane ( 1 ) is produced by casting, and an internal hole ( 3 ) for coolant is then cut out of the cast vane ( 1 ). The vane ( 1 ) is provided with a starter hole ( 5 ), either during casting or once casting is completed, following which the internal hole ( 3 ) for coolant is cut out of the vane, proceeding from the starter hole. A method is also disclosed for manufacturing a gas turbine component including a plurality of vanes ( 1 ) for guiding a gas flow. The gas turbine component is cast in such a way that it includes the vanes and an internal hole ( 3 ) for coolant is then cut out of each of the vanes. |
申请公布号 |
RU2003112976(A) |
申请公布日期 |
2005.02.27 |
申请号 |
RU20030112976 |
申请日期 |
2001.09.25 |
申请人 |
ВОЛЬВО АЭРО КОРПОРЕЙШН (SE) |
发明人 |
Бертиль ЙЁНССОН (SE);Ларс СУНДИН (SE) |
分类号 |
B23H7/02;B23H9/00;B23H9/10;B23P15/02;F01D5/18 |
主分类号 |
B23H7/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|