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:

Jun. 20, 2016
Applicant:

Volvo Truck Corporation, Gothenburg, SE;

Inventors:

Ulf Aronsson, Lund, SE;

Martin Bauer, Anderslov, SE;

Mohammed Adlouni, Eslöv, SE;

Assignee:

VOLVO TRUCK CORPORATION, Gothenburg, SE;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02M 26/05 (2016.01); F02M 26/08 (2016.01); F02M 26/09 (2016.01); F02B 37/18 (2006.01); F02B 37/013 (2006.01); F02B 37/02 (2006.01); F02B 37/00 (2006.01); F02M 26/42 (2016.01); F02M 26/38 (2016.01); F02D 41/00 (2006.01); F02B 41/10 (2006.01); F02M 26/16 (2016.01); F01N 3/021 (2006.01); F01N 3/20 (2006.01);
U.S. Cl.
CPC ...
F02D 41/0065 (2013.01); F01N 3/021 (2013.01); F01N 3/2066 (2013.01); F02B 37/004 (2013.01); F02B 37/013 (2013.01); F02B 37/025 (2013.01); F02B 37/18 (2013.01); F02B 37/183 (2013.01); F02B 41/10 (2013.01); F02M 26/05 (2016.02); F02M 26/08 (2016.02); F02M 26/09 (2016.02); F02M 26/16 (2016.02); F02M 26/38 (2016.02); F02M 26/42 (2016.02); F02D 41/0007 (2013.01); Y02T 10/12 (2013.01); Y02T 10/40 (2013.01);
Abstract

An internal combustion engine system includes an internal combustion engine, a first turbine unit receiving exhaust gases from the internal combustion engine, the turbine unit having a compressor for compressing intake air and feeding the intake air by an air intake line to the internal combustion engine, and an exhaust gas recirculation line connecting the air intake line with an exhaust as line of the internal combustion engine at a position upstream the first turbine unit. A bypass line connects the exhaust gas recirculation line to the exhaust gas line at a position downstream of the turbine unit, the bypass line having an arrangement for controlling the exhaust gas flow from the exhaust gas recirculation line to the exhaust gas line.


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