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:
Feb. 24, 2015

Filed:

Sep. 15, 2011
Applicants:

Jonathan Nagurney, Lawrence Park, PA (US);

Daniel Loringer, Lawrence Park, PA (US);

Kendall Swenson, Lawrence Park, PA (US);

Lukas Johnson, Lawrence Park, PA (US);

Rodrigo Rodriguez Erdmenger, Garching, DE;

Amit Sharma, Bangalore, IN;

Swaminathan Gopalakrishnan, Bangalore, IN;

Inventors:

Jonathan Nagurney, Lawrence Park, PA (US);

Daniel Loringer, Lawrence Park, PA (US);

Kendall Swenson, Lawrence Park, PA (US);

Lukas Johnson, Lawrence Park, PA (US);

Rodrigo Rodriguez Erdmenger, Garching, DE;

Amit Sharma, Bangalore, IN;

Swaminathan Gopalakrishnan, Bangalore, IN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02D 23/00 (2006.01); F02B 33/00 (2006.01); F02B 37/013 (2006.01); F01N 13/18 (2010.01); F02B 37/00 (2006.01); F02B 37/02 (2006.01); F02B 37/18 (2006.01); F17D 1/04 (2006.01);
U.S. Cl.
CPC ...
F02B 37/013 (2013.01); F01N 13/1816 (2013.01); F02B 37/004 (2013.01); F02B 37/02 (2013.01); F02B 37/18 (2013.01); F17D 1/04 (2013.01); Y02T 10/144 (2013.01);
Abstract

Various apparatuses and systems are provided for a turbocharger. In one example, the turbocharger system includes a first turbine having an exhaust flow outlet and a second turbine having an exhaust flow inlet. The turbocharger system further includes a transition conduit fluidically coupling the outlet of the first turbine to the inlet of the second turbine, the transition conduit including an expansion region upstream of a first bend, and a bypass which routes exhaust flow around the first turbine, the bypass having an exhaust flow outlet fluidically coupled to the transition conduit downstream of the expansion region.


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