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:
Mar. 22, 2016

Filed:

Feb. 08, 2013
Applicant:

GM Global Technology Operations Llc, Detroit, MI (US);

Inventors:

Yue-Yun Wang, Troy, MI (US);

Ibrahim Haskara, Macomb, MI (US);

Kevin Andrew Gady, Ypsilanti, MI (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02B 37/12 (2006.01); F02B 37/18 (2006.01); F02B 37/24 (2006.01); F02D 41/00 (2006.01); F02D 41/14 (2006.01); F02M 25/07 (2006.01);
U.S. Cl.
CPC ...
F02B 37/12 (2013.01); F02B 37/18 (2013.01); F02B 37/24 (2013.01); F02D 41/0007 (2013.01); F02B 2037/122 (2013.01); F02D 41/0072 (2013.01); F02D 2041/1433 (2013.01); F02D 2200/0402 (2013.01); F02M 25/0707 (2013.01); F02M 25/0713 (2013.01); Y02T 10/144 (2013.01);
Abstract

A method for controlling a turbocharger is provided. The turbocharger has a turbine operatively connected to an exhaust of an internal combustion engine, and a compressor operatively connected to an intake of the engine. The method includes determining a boost pressure command for the compressor. The boost pressure command is configured to provide sufficient combustion reactant for the engine. The method includes calculating a compressor power from the determined boost pressure command, and calculating a turbine flow from the calculated compressor power. The method commands the turbocharger to operate at the calculated turbine flow.


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