Invention Grant
US08684691B2 Turbine blade with chamfered squealer tip and convective cooling holes 有权
涡轮叶片带倒角尖尖和对流冷却孔

Turbine blade with chamfered squealer tip and convective cooling holes
Abstract:
A squealer tip formed from a pressure side rib and a suction side rib extending radially outward from a tip of the turbine blade is disclosed. The pressure and suction side ribs may be positioned along the pressure side and the suction side of the turbine blade, respectively. The pressure and suction side ribs may include chamfered leading edges with film cooling holes having exhaust outlets positioned therein. The film cooling holes may be configured to be diffusion cooling holes with one or more tapered sections for reducing the velocity of cooling fluids and increasing the size of the convective surfaces.
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