Central cooling circuit for a moving blade of a turbomachine

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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07661930

ABSTRACT:
A moving blade for a turbomachine with a central portion that is geometrically subdivided into four adjacent pressure-side zones disposed on the pressure side of the blade, and into four adjacent suction-side zones disposed on the suction side of the blade, the pressure-side and suction-side zones being distributed on either side of the skeleton of the blade, and the blade including in its central portion a pressure-side cooling circuit and a suction-side cooling circuit, the pressure-side cooling circuit including three radial cavities occupying three adjacent pressure-side zones, and the suction-side cooling circuit including three radial cavities occupying the four suction-side zones and the remaining pressure-side zone.

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patent: 5356265 (1994-10-01), Kercher
patent: 7513739 (2009-04-01), Boury et al.
patent: 2007/0059172 (2007-03-01), Lee et al.
patent: 2007/0116570 (2007-05-01), Boury et al.
patent: 2007/0253815 (2007-11-01), Kopmels et al.
patent: 1 526 250 (2005-04-01), None
patent: 1 584 790 (2005-10-01), None
patent: 60-135606 (1985-07-01), None
patent: 60198305 (1985-10-01), None

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