| 摘要 |
A turbine blade (10) includes an airfoil (16) having pressure and suction sidewalls (22, 24) spaced apart between opposite leading and trailing edges (26, 28) and interconnected by a plurality of partitions (42) to define first and second independent cooling circuits (44, 46) therein. The cooling circuits (44, 46) have corresponding inlets in a dovetail (20) of the |
