| 摘要 |
<p>A turbine bucket (10) has an airfoil portion (12) and a root portion, with a substantially planar platform (14) at an interface between the airfoil portion (12) and root portion. A platform cooling arrangement includes at least one bore (36) in the root portion and at least one impingement cooling tube (40) seated in the bore, the tube (40) extending beyond the bore (36) with an outlet in close proximity to a targeted area on an underside of the platform (14). <IMAGE></p> |
