Multi-peripheral serpentine microcircuits for high aspect...

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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07980822

ABSTRACT:
A cooling arrangement for a pressure side of an airfoil portion of a turbine engine component is provided. The cooling arrangement comprises a pair of cooling circuits embedded within a wall forming the pressure side. The pair of cooling circuits includes a first serpentine cooling circuit and a second circuit offset from the first serpentine cooling circuit.

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patent: 6264428 (2001-07-01), Dailey et al.
patent: 6705836 (2004-03-01), Bourriaud et al.
patent: 7722324 (2010-05-01), Cunha et al.
patent: 2009/0104042 (2009-04-01), Liang
patent: 4203203 (1992-07-01), None

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