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:
Sep. 19, 2017

Filed:

Apr. 11, 2014
Applicant:

Cummins Inc., Columbis, IN (US);

Inventors:

Emrah Arslanturk, Greenwood, IN (US);

Orcun Kurugol, Greenwood, IN (US);

Ohiorenuan J. Amu, Greenwood, IN (US);

Assignee:

CUMMINS INC., Columbus, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02D 41/00 (2006.01); F02D 21/08 (2006.01); F02M 26/02 (2016.01); F02M 26/04 (2016.01); F02M 26/45 (2016.01); F02M 26/47 (2016.01); F02M 26/48 (2016.01); F02M 26/49 (2016.01); F02B 37/22 (2006.01); F02B 37/24 (2006.01); F02M 26/05 (2016.01);
U.S. Cl.
CPC ...
F02D 41/0007 (2013.01); F02D 21/08 (2013.01); F02D 41/0052 (2013.01); F02M 26/48 (2016.02); F02B 37/22 (2013.01); F02B 37/24 (2013.01); F02D 2200/0402 (2013.01); F02D 2200/0406 (2013.01); F02M 26/05 (2016.02); F02M 26/47 (2016.02); Y02T 10/144 (2013.01); Y02T 10/47 (2013.01);
Abstract

An internal combustion engine having intake and exhaust manifolds, a turbocharger with a compressor, and at least one of: an exhaust gas recirculation (EGR) valve and a variable geometry turbine (VGT). The system further includes a control computer configured to determine at least one of torque demand, pressure across the compressor, and pressure gradient ratio between the exhaust manifold and the intake manifold relative to one of exhaust manifold pressure, intake manifold pressure, and 1. The control computer performs at least one of: closing the EGR valve in response to the determined at least one of torque demand, pressure across the compressor, and pressure gradient ratio, and lessening restriction provided by the variable geometry turbine responsive to the determined at least one of torque demand, pressure across the compressor, and pressure gradient between the exhaust manifold and the intake manifold.


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