Gas turbine engine with an air cooled bearing

Power plants – Combustion products used as motive fluid – With lubricators

Reexamination Certificate

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Details

C384S476000, C384S900000

Reexamination Certificate

active

07997057

ABSTRACT:
A small gas turbine engine where the compressor and turbine are supported on a rotary shaft, and a main bearing is supported on the rotary shaft, the main bearing being located in a hot zone of the combustor. The main bearing includes cooling air passages within the races to provide cooling for the bearing. A cooling air is diverted from the compressor and passed through the bearing cooling passages for cooling the bearing, and then the cooling air is directed into the combustor. The cooling air is also passed through a guide nozzle before being passed through the bearing to cool both the guide nozzle and the bearing. A swirl cup injector is used to deliver the compressed air from the compressor and the cooling air from the bearing into the combustor, the swirl cup injector also acting to draw the cooling air through the bearing.

REFERENCES:
patent: 2479573 (1949-08-01), Howard
patent: 3200580 (1965-08-01), Millar
patent: 3898793 (1975-08-01), Nakamura et al.
patent: 4000608 (1977-01-01), Chute
patent: 4156342 (1979-05-01), Korta et al.
patent: 5526640 (1996-06-01), Brooks et al.
patent: 6966191 (2005-11-01), Fukutani et al.
patent: 2005/0235651 (2005-10-01), Morris et al.

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