Turbo-compound compressor system

Pumps – Motor driven – Internal-combustion engine

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Details

417380, F04B 1700

Patent

active

046799923

ABSTRACT:
A turbo-compound compressor system includes a booster compressor connected to the output shaft of a power recovery turbine which is disposed downstream of the outlet of an expansion turbine in a turbocharger for an internal combustion engine and drivable by the exhaust gas of the engine, and a rotary positive-displacement air compressor drivable by the engine also into which the air delivered by the booster compressor is supplied through an air supply conduit having a throttle valve. The turbo-compound compressor system further includes a bypass line provided therein with a closing valve and adapted to prevent surging caused in the booster compressor.

REFERENCES:
patent: 3122308 (1964-02-01), Anderson et al.
patent: 3204859 (1965-09-01), Crooks
patent: 3495766 (1970-02-01), Hinkle

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