Gas turbine stator

Rotary kinetic fluid motors or pumps – With diversely oriented inlet or additional inlet for...

Reexamination Certificate

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C415S180000, C415S174500

Reexamination Certificate

active

07048497

ABSTRACT:
A gas turbine stator including at least a first injector providing a passage for a main cooling air stream into a pressurized chamber. An evacuation mechanism discharges air coming from an internal labyrinth gland of a first cavity towards a lower-pressure second cavity. A second injector evacuates the air contained in the second cavity towards a main duct. The stator further includes a third injector designed to generate an overpressure close to the internal labyrinth gland in the pressurized chamber.

REFERENCES:
patent: 3989410 (1976-11-01), Ferrari
patent: 4466239 (1984-08-01), Harris et al.
patent: 4822244 (1989-04-01), Maier et al.
patent: 5245821 (1993-09-01), Rieck, Jr. et al.
patent: 5402636 (1995-04-01), Mize et al.
patent: 5575616 (1996-11-01), Hagle et al.
patent: 6017189 (2000-01-01), Marchi et al.
patent: 6773225 (2004-08-01), Yuri et al.
patent: 6776573 (2004-08-01), Arilla et al.

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