Axial thrust loading mitigation in a turbocharger
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United States of America Patent
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Oct 12, 2021
Grant Date -
Nov 7, 2019
app pub date -
Jul 16, 2019
filing date -
Oct 30, 2015
priority date (Note) -
In Force
status (Latency Note)
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Abstract
Methods and systems are provided for a turbocharger system to reduce and balance axial thrust load on the turbine shaft and the associated bearing system and sealing. In one example, a partial back plate compressor may be used in combination with an axial turbine to reduce axial thrust load and to improve turbocharger transient response time. In another example, a regenerative turbocharger system with back-to-back turbo pump may be used to reduce and balance axial thrust load.
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