Rotatable component for turbomachines, including a non-axisymmetric overhanging portion
AssigneeGeneral Electric Company
InventorsGanesh Seshadri, Mahendran Manoharan
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AssigneeGeneral Electric Company
InventorsGanesh Seshadri, Mahendran Manoharan
Estimating the term…
A rotatable component for a turbomachine and a method for regulating a circumferential ingress of a fluid at a trailing edge of the rotatable component are disclosed. The rotatable component includes an airfoil and a mechanical component. The airfoil includes a pressure side and a suction side. The mechanical component is coupled to the airfoil and includes a forward overhanging portion, and an aft overhanging portion. The forward overhanging portion is disposed at a leading edge of the airfoil and extends longitudinally beyond the leading edge. The aft overhanging portion is disposed at a trailing edge of the airfoil and extends longitudinally beyond the trailing edge, where both the forward and aft overhanging portions further extend circumferentially along the pressure side and the suction side of the airfoil. The aft overhanging portion includes a non-axisymmetric profile for regulating the circumferential ingress of the fluid from the pressure to suction sides.
A rotatable component comprising:
A turbomachine comprising:
A method comprising:
Dependencies are inferred from the claim text.