Turbine airfoil platform cooling circuit

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

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C416S19300A

Reexamination Certificate

active

11134927

ABSTRACT:
An airfoil assembly includes an airfoil extending away from a platform. One or more cooling circuits are formed through the platform in order to provide cooling of the platform. The cooling circuit may include a downwardly directed inlet receiving cooling air from below the platform. The cooling air is then directed in a direction generally parallel to the outer surface of the platform and through exits formed through the outer surface of the platform. The cooling circuit may optionally include a plurality of pedestals extending from an outer wall to an inner wall of the cooling circuit to increase the rigidity and the cooling function of the cooling circuit.

REFERENCES:
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patent: 6390774 (2002-05-01), Lewis et al.
patent: 7097424 (2006-08-01), Cunha et al.
U.S. Appl. No. 10/637,352, entitled “Microcircuit Airfoil Main Body,” filed Aug. 8, 2003.
U.S. Appl. No. 10/979,597, entitled Airfoil with Serpentine Cooling Channel and Microcircuit, filed Nov. 2, 2004.

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