| 摘要 |
PROBLEM TO BE SOLVED: To properly supply coolant. SOLUTION: This turbine blade particularly for gas turbine comprises at least one of chambers 22, 23, 24, and 25 and at least one of inlets 30 and 31 for supplying coolant to the chambers 22, 23, 24, and 25. In this turbine blade, the inlet 30 is arranged to have angle with respect to a longitudinal axial line 37 of the turbine blades 13 and 14, and extends approximately in parallel with a flow direction 15 of a medium flowing through a turbine 10. |
