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:
May. 24, 2016

Filed:

Jul. 10, 2013
Applicant:

Electro-motive Diesel, Inc., Lagrange, IL (US);

Inventors:

Shakeel Nasir, Willowbrook, IL (US);

Joshua David Schueler, New Lenox, IL (US);

Assignee:

Electro-Motive Diesel, Inc., LaGrange, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 37/02 (2006.01); F02B 37/00 (2006.01); F02B 37/007 (2006.01); F02B 37/013 (2006.01); F02M 25/07 (2006.01); F01D 9/02 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F02B 37/025 (2013.01); F01D 9/026 (2013.01); F01D 9/041 (2013.01); F02B 37/001 (2013.01); F02B 37/004 (2013.01); F02B 37/007 (2013.01); F02B 37/013 (2013.01); F05D 2220/40 (2013.01);
Abstract

A turbocharger is disclosed for use with an engine system. The turbocharger may have a housing at least partially defining a compressor shroud and a turbine shroud. The turbine shroud may form a first volute and a second volute, each having an inlet configured to receive exhaust from an exhaust manifold of the engine in a tangential direction, and an axial channel disposed downstream of the inlet. The turbocharger may also have a turbine wheel disposed within the turbine shroud and configured to receive exhaust from the axial channels of the first and second volutes, a compressor wheel disposed within the compressor shroud, and a shaft connecting the turbine wheel to the compressor wheel. The turbocharger may further have a nozzle ring in fluid communication with the axial channels of the first and second volutes at a location upstream of the turbine wheel.


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