Airfoil with three-pass serpentine cooling channel and...

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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C415S115000

Reexamination Certificate

active

07131818

ABSTRACT:
An airfoil, and in a disclosed embodiment a rotor blade, has a serpentine cooling path. To best account for the Coriolis effect, the paths of the serpentine cooling channel have trapezoidal cross-sections. An area of the rotor blade between a smaller side of the trapezoidal-shaped paths, and a facing wall of the rotor blade has high thermal and mechanical stresses, and is a challenge to adequately cool. A microcircuit, which is a very thin cooling circuit having crossing pedestals, is embedded into the blade in this area. The microcircuit provides additional cooling, and addresses the challenges with regard to cooling these areas.

REFERENCES:
patent: 5720431 (1998-02-01), Sellers et al.
patent: 6514042 (2003-02-01), Kvasnak et al.
patent: 6896487 (2005-05-01), Cunha et al.
U.S. Appl. No. 10/637,352 entitled: “Microcircuit Airfoil Main Body,” filed Aug. 8, 2003.

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