Peripheral microcircuit serpentine cooling for turbine airfoils

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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Reexamination Certificate

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07744347

ABSTRACT:
A turbine component has an airfoil portion with at least one central core element, a pressure side wall, and a suction side wall. The airfoil portion also has a serpentine cooling passageway in at least one of the walls. In a preferred embodiment, the airfoil portion has a serpentine cooling passageway in both of the pressure and suction side walls. A refractory metal core for forming the serpentine cooling passageway(s) is also described.

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patent: 6705836 (2004-03-01), Bourriaud et al.
patent: 60-135606 (1985-07-01), None
patent: 62-282102 (1987-12-01), None

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