TWO-STAGE TURBOCHARGER ASSEMBLY WITH SINGLE LOW-PRESSURE TURBOCHARGER
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United States of America Patent
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app pub date -
Nov 26, 2013
filing date -
Nov 25, 2009
priority date (Note) -
Abandoned
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Abstract
A two-stage turbocharger assembly for an internal combustion engine is provided. The assembly has a single low pressure turbocharger, and more than two high pressure turbochargers arranged in parallel with each other. The compressor outlet of the single low pressure turbocharger is operatively connected to the compressor inlets of the high pressure turbochargers. The turbine outlets of the high pressure turbochargers are operatively connected to the turbine inlet of the single low pressure turbocharger.
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