Integrated turbocharger ejector intercooler with partial isothermal compression
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United States of America Patent
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-
Mar 4, 2003
Grant Date -
N/A
app pub date -
Dec 17, 2001
filing date -
Dec 17, 2001
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
An integrated cooling system for a turbocharger, suitable for an internal combustion engine. A cooling air shroud includes a cooling air inlet and a cooling air outlet. A flow inducer is associated with the cooling air outlet to draw air into the cooling air shroud, and pass the cooling air in heat exchange relationship with compressed air flowing through the turbocharger.
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