Seal cooling apparatus

Power plants – Combustion products used as motive fluid – Combustion products generator

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Details

60 3983, 415112, 415176, F01D 2512, F01D 1104

Patent

active

045547890

ABSTRACT:
An improved seal cooling apparatus is provided for use in a gas turbine engine. In a particular embodiment, this apparatus includes means for deriving conditioning air from air discharged from the compressor diffuser and directing this air onto the seal stator to improve its thermal response. The apparatus also includes means to inject a portion of the conditioning air into a cavity forward of the seal to purge the region and prevent zero airflow conditions during engine operation for the purpose of discouraging overheating of a portion of the compressor rotor. A portion of the conditioning air from the cavity is subsequently directed to flow through and thereby cool the seal.

REFERENCES:
patent: 3291447 (1966-12-01), Brandon
patent: 3365172 (1968-01-01), McDonough et al.
patent: 3826084 (1974-07-01), Branstrom et al.
patent: 3989410 (1976-11-01), Ferrari
patent: 4190397 (1980-02-01), Schilling et al.
patent: 4358926 (1982-11-01), Smith

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