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:
Dec. 27, 2016

Filed:

Sep. 25, 2011
Applicants:

John N. Chi, Dubuque, IA (US);

John M. Mulloy, Columbus, IN (US);

Sriram S. Popuri, Greenwood, IN (US);

Timothy R. Frazier, Columbus, IN (US);

Martin T. Books, Columbus, IN (US);

Divakar Rajamohan, Columbus, IN (US);

Indranil Brahma, Bloomington, IN (US);

Inventors:

John N. Chi, Dubuque, IA (US);

John M. Mulloy, Columbus, IN (US);

Sriram S. Popuri, Greenwood, IN (US);

Timothy R. Frazier, Columbus, IN (US);

Martin T. Books, Columbus, IN (US);

Divakar Rajamohan, Columbus, IN (US);

Indranil Brahma, Bloomington, IN (US);

Assignee:

Cummins, Inc., Columbus, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02M 25/07 (2006.01); F02B 39/10 (2006.01); F02B 37/10 (2006.01); F02B 37/14 (2006.01); F02D 41/00 (2006.01); F02D 41/14 (2006.01); F02B 37/24 (2006.01);
U.S. Cl.
CPC ...
F02B 39/10 (2013.01); F02B 37/10 (2013.01); F02B 37/14 (2013.01); F02D 41/0007 (2013.01); F02D 41/0052 (2013.01); F02D 41/0065 (2013.01); F02D 41/1448 (2013.01); F02D 41/1462 (2013.01); F02D 41/1467 (2013.01); F02B 37/24 (2013.01); F02D 2041/141 (2013.01); F02D 2041/1433 (2013.01); F02M 26/05 (2016.02); F02M 26/10 (2016.02); F02M 26/23 (2016.02); Y02T 10/144 (2013.01); Y02T 10/47 (2013.01);
Abstract

A system and method are provided for controlling an air handling system for an internal combustion engine including a turbocharger having a variable geometry turbine fluidly coupled to an exhaust manifold of the engine and a compressor fluidly coupled to an intake manifold of the engine, and an electric motor coupled to a rotatable shaft connected between the compressor and the variable geometry turbine. A target torque required to drive the compressor to achieve target compressor operating parameters is determined, a maximum available torque that can be supplied by the variable geometry turbine in response to a target exhaust gas flow through the variable geometry turbine is determined, and the electric motor is enabled to supply supplemental torque to the rotatable shaft if the target torque is greater than the maximum available torque.


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