Methods and systems for a two-stage turbocharger
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United States of America Patent
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Oct 27, 2020
Grant Date -
Jan 11, 2018
app pub date -
Jun 30, 2017
filing date -
Jul 5, 2016
priority date (Note) -
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Abstract
The disclosure relates to a supercharged, direct-injection internal combustion engine having an intake system for the supply of charge air and having an exhaust-gas discharge system for the discharge of exhaust gas and having at least two series-connected exhaust-gas turbochargers which each comprise a turbine arranged in the exhaust-gas discharge system and a compressor arranged in the intake system and of which a first exhaust-gas turbocharger serves as a low-pressure stage and a second exhaust-gas turbocharger serves as a high-pressure stage, a first bypass line being provided which branches off from the exhaust-gas discharge system between the first turbine and the second turbine so as to form a first junction point.
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