Turbine blade wall cooling apparatus and method of fabrication
AssigneeGeneral Electric Company
InventorsRonald Scott Bunker, Frederic Joseph Klug, Shyh-Chin Huang
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AssigneeGeneral Electric Company
InventorsRonald Scott Bunker, Frederic Joseph Klug, Shyh-Chin Huang
Estimating the term…
A turbine blade comprises an external pressure side plate comprising a plurality of external pressure ribs, an internal pressure side plate comprising a plurality of internal pressure ribs, and a plurality of pressure flow redirection areas. The external pressure side plate is disposed over the internal pressure side plate to form a pressure side double wall. The external pressure ribs are disposed at a first angle with respect to a blade span reference line and the internal pressure ribs are disposed at a second angle with respect to the blade span reference line to form the pressure flow redirection areas. The pressure side double wall is configured to pass a coolant through the pressure side double wall. A fabrication method aligns the external pressure side plate and the internal pressure side plate to form the pressure flow redirection areas between the external pressure side plate and the internal pressure side plate.
An pressure side double wall for a turbine blade comprising:
A turbine blade comprising:
A method of fabricating a pressure side double wall for a turbine blade comprising:
A method of fabricating a suction side double wall for a turbine blade comprising:
A method of fabricating a pressure side double wall and a suction side double wall for a turbine blade comprising:
Dependencies are inferred from the claim text.