Microcircuit airfoil mainbody

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

06896487

ABSTRACT:
A cooling circuit disposed within a first wall portion and a second wall portion of a wall for use in a gas turbine engine is provided. The cooling circuit includes a plurality of inlet apertures disposed in the first wall portion to provide a flow path of cooling air into the cooling circuit, a first exit slot disposed in the second wall portion to provide a cooling air flow path out of the cooling circuit, a plurality of pedestals arranged in rows extending between the first wall portion and the second wall portion and a first elongated pedestal disposed radially and extending between the first and second wall portions. The first elongated pedestal is positioned between the pedestals and the first exit slot.

REFERENCES:
patent: 4542867 (1985-09-01), Memmen
patent: 6247896 (2001-06-01), Auxier et al.
patent: 6254334 (2001-07-01), LaFleur
patent: 6280140 (2001-08-01), Soechting et al.
patent: 6402470 (2002-06-01), Kvasnak et al.
patent: 6514042 (2003-02-01), Kvasnak et al.

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