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. 23, 2020

Filed:

Apr. 12, 2018
Applicant:

Caterpillar Inc., Deerfield, IL (US);

Inventor:

Matthew T. Wolk, Peoria, IL (US);

Assignee:

Caterpillar Inc., Peoria, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02M 26/08 (2016.01); F02M 26/23 (2016.01); F02M 26/17 (2016.01); F02M 26/39 (2016.01); F02M 26/35 (2016.01); F02B 37/013 (2006.01); F01N 13/10 (2010.01); F02M 26/00 (2016.01);
U.S. Cl.
CPC ...
F02M 26/08 (2016.02); F01N 13/107 (2013.01); F02B 37/013 (2013.01); F02M 26/17 (2016.02); F02M 26/23 (2016.02); F02M 26/39 (2016.02); F02M 26/35 (2016.02); F02M 2026/005 (2016.02);
Abstract

An engine system includes an engine including a plurality of engine cylinders, an intake manifold, and an exhaust manifold; and a compound turbocharger system having a first turbine driving a first compressor, and a second turbine driving a second compressor. The engine system further includes an intake line including the first compressor, the second compressor, and the at least one intake manifold; and an exhaust line including the exhaust manifold, the second turbine, and the first turbine. The engine system also includes an exhaust restriction valve located in the exhaust manifold of the engine downstream of a subset of the plurality of the engine cylinders; and an exhaust gas recirculation line having an upstream end located to receive exhaust from the subset of the plurality of engine cylinders, and a downstream end coupled to the intake line downstream the first compressor and upstream of the second compressor.


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