发明名称 |
Cooled airfoil for gas turbine engine and method of making the same |
摘要 |
An airfoil (40) for use in a gas turbine engine includes a pressure side (42) and a suction side (44) joined at a trailing edge wall (60) that defines a trailing edge (48). The airfoil (40) includes at least one cooling hole (68) extending through the trailing edge wall (60) so as to pass cooling fluid from the pressure side (42) of the airfoil (40) to the suction side (44). <IMAGE> |
申请公布号 |
EP1106782(A2) |
申请公布日期 |
2001.06.13 |
申请号 |
EP20000310957 |
申请日期 |
2000.12.08 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
TSAI, GENE CHEN-FU;TUNG, SUNG;FLAHERTY, TERENCE CARROLL;MANNING, ROBERT FRANCIS |
分类号 |
F01D9/02;F01D5/18 |
主分类号 |
F01D9/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|