The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 01, 2021

Filed:

May. 07, 2019
Applicant:

Caterpillar Inc., Deerfield, IL (US);

Inventor:

Christopher Lusardi, Peoria, IL (US);

Assignee:

Caterpillar Inc., Peoria, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 37/00 (2006.01); F02M 26/08 (2016.01); F02B 37/24 (2006.01); F02B 37/013 (2006.01); F04D 29/22 (2006.01); F01D 5/14 (2006.01); H01M 8/04111 (2016.01); H01M 8/124 (2016.01);
U.S. Cl.
CPC ...
F02B 37/001 (2013.01); F01D 5/14 (2013.01); F02B 37/013 (2013.01); F02B 37/24 (2013.01); F02M 26/08 (2016.02); F04D 29/2216 (2013.01); H01M 8/04111 (2013.01); H01M 2008/1293 (2013.01);
Abstract

An engine system includes an internal combustion engine having an intake passage, a first set of combustion chambers, a second set of combustion chambers, a first exhaust passage fluidly connected to the first set of combustion chambers, and a second exhaust passage fluidly connected to the second set of combustion chambers. The engine system includes a first turbocharger including a first compressor and a first turbine. The engine system also includes a second turbocharger including a second compressor and a second turbine, the second compressor connected in series with the first compressor, and the second turbine being in fluid communication with the second exhaust passage. The first and second turbines are connected in parallel such that the first turbine only receives exhaust flow from the first set of combustion chambers, and the second turbine only receives exhaust flow from the second set of combustion chambers.


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