Invention Grant
US08727724B2 Turbine bucket having a radial cooling hole 有权
涡轮斗具有径向冷却孔

Turbine bucket having a radial cooling hole
Abstract:
A turbine bucket is provided and includes a shank interconnectable with a rotor and formed to accommodate coolant therein and an airfoil blade coupled to a radially outward portion of the shank and including a body formed to define a substantially radially extending cooling hole therein, which is disposed to be solely receptive of the coolant accommodated within the shank for removing heat from the body, the cooling hole being further defined as having a substantially non-circular cross-sectional shape at a predefined radial position of the body.
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