Micro-circuit platform

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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07097424

ABSTRACT:
A gas turbine engine component, such as a high pressure turbine blade, has an airfoil portion, a platform, and micro-circuits within the platform for cooling at least one of a platform edge adjacent the pressure side of the airfoil portion and the trailing edge of the platform. The micro-circuits include a first micro-circuit on a suction side of the airfoil and a second micro-circuit on a pressure side of the airfoil. The micro-circuits within the platform achieve high thermal convective efficiency, high film coverage, and high cooling effectiveness.

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patent: 5340278 (1994-08-01), Magowan
patent: 5413458 (1995-05-01), Calderbank
patent: 6120249 (2000-09-01), Hultgren et al.
patent: 6179565 (2001-01-01), Palumbo et al.
patent: 6390774 (2002-05-01), Lewis et al.

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