Turbine blade, and turbine and gas turbine including the same
AssigneeDoosan Heavy Industries Construction Co., Ltd
InventorHyuk Hee LEE
Life of this patent
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AssigneeDoosan Heavy Industries Construction Co., Ltd
InventorHyuk Hee LEE
Estimating the term…
A turbine blade, a turbine, and a gas turbine which have enhanced cooling performance are provided. The turbine blade may include: an airfoil having a blade shape and including a suction side formed in a convex shape and a pressure side formed in a concave shape; a platform coupled to a lower portion of the airfoil; and a root member protruding downward from the platform and coupled to a rotor disk, wherein the platform may include: a plurality of inlets through which air is drawn into the platform; a plurality of outlets through which the air is discharged from the platform; and a cooling passage connecting the inlets to the outlets and including a plurality of dispersion spaces, a width in each dispersion spaces increasing from the inlet to the outlet, and a narrow space formed between the dispersion spaces and having a width less than the width of each dispersion spaces.
A turbine blade comprising:
A turbine comprising:
A gas turbine comprising:
Dependencies are inferred from the claim text.