Device for cooling turbine disks

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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Details

C415S191000, C415S209200

Reexamination Certificate

active

07025562

ABSTRACT:
A turbine disk cooling device fed with cooling air from an orifice through an annular support platform for a fixed vane of a low-pressure turbine is disposed between an upstream flange and a downstream flange of the support platform. The device includes upstream and downstream annular plates longitudinally defining an annular cavity, a sealing device extending longitudinally between the upstream and downstream plates so as to close the cooling air cavity, an element to hold the upstream and downstream plates against upstream and downstream flanges of the support platform, and a plurality of holes for ejecting cooling air towards the turbine disks.

REFERENCES:
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patent: 3945758 (1976-03-01), Lee
patent: 4217755 (1980-08-01), Williams
patent: 4805398 (1989-02-01), Jourdain et al.
patent: 5358374 (1994-10-01), Correia et al.
patent: 5503528 (1996-04-01), Glezer et al.
patent: 6065928 (2000-05-01), Rieck et al.
patent: 6152685 (2000-11-01), Hagi
patent: 6179555 (2001-01-01), Tremaine
patent: 6464232 (2002-10-01), Marchi et al.
patent: 6551056 (2003-04-01), Rau
patent: 1.351.268 (1964-01-01), None

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