主权项 |
1. A turbine rotor blade, comprising:
a. a mounting portion that partially defines a cooling circuit within the turbine rotor blade; b. an airfoil portion that extends radially outward from the mounting portion, the airfoil portion further defining the cooling circuit; c. a platform portion disposed radially between the mounting portion and the airfoil, the platform portion having a bottom wall, a top wall, a forward wall, an aft wall and a pair of opposing side walls; and d. a cooling plenum defined within the platform portion, the cooling plenum further defining the cooling circuit, wherein the cooling plenum is to least partially defined between the forward wall, the aft wall and between the pair of opposing side walls. |