Cooling air evacuation slots of turbine blades

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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11032012

ABSTRACT:
A turbine blade of a turbomachine, having at least a bottom platform connected to the base of the blade by a bottom connection zone, and a cooling circuit consisting of at least one cooling cavity, of a plurality of evacuation slots arranged along the trailing edge of the blade, said blade having a bottom evacuation slot that is disposed near the blade base, the bottom evacuation slot including an end wall provided with an opening that opens into the cavity, a setback wall, a bottom wall disposed beside the blade base, a bottom edge formed between the setback wall and the bottom wall, and a bottom shoulder formed between the bottom wall and the bottom connection zone, both the bottom edge of the bottom evacuation slot and the bottom shoulder of the bottom evacuation slot having respective right sections of substantially rounded shape, thereby avoiding any protruding angles between the opening of said slot and the bottom connection zone.

REFERENCES:
patent: 6062817 (2000-05-01), Danowski et al.
patent: 6328531 (2001-12-01), Bariaud et al.
patent: 6612811 (2003-09-01), Morgan et al.
patent: 2003/0108423 (2003-06-01), Morgan et al.
patent: 0 945 594 (1999-09-01), None
patent: 0 978 634 (2000-02-01), None
patent: 1 016 773 (2000-07-01), None
patent: 2 835 015 (2003-07-01), None

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