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:
Jul. 18, 2017

Filed:

Jul. 08, 2015
Applicant:

Cummins Turbo Technologies Limited, Huddersfield, GB;

Inventors:

James A. McEwan, Huddersfield, GB;

Lee J. Robinson, Huddersfield, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02B 37/013 (2006.01); F02B 37/22 (2006.01); F02B 37/18 (2006.01); F02D 9/06 (2006.01); F01D 5/02 (2006.01); F02B 33/40 (2006.01); F01D 25/24 (2006.01); F02M 26/08 (2016.01); F02M 26/10 (2016.01); F02M 26/23 (2016.01);
U.S. Cl.
CPC ...
F02B 37/013 (2013.01); F01D 5/02 (2013.01); F02B 33/40 (2013.01); F02B 37/183 (2013.01); F02B 37/22 (2013.01); F02B 37/225 (2013.01); F02D 9/06 (2013.01); F01D 25/24 (2013.01); F02M 26/08 (2016.02); F02M 26/10 (2016.02); F02M 26/23 (2016.02); F05D 2220/40 (2013.01); F05D 2240/24 (2013.01); Y02T 10/144 (2013.01);
Abstract

A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger () and a second relatively large low pressure (LP) turbocharger (). The turbine () of the LP turbocharger () is connected in series downstream of the turbine () of the HP turbocharger () in a first exhaust gas passage (). An exhaust bypass flow passage () provides a bypass flow path around the HP turbine (). A rotary valve () is located at a junction of the bypass flow passage () and a first exhaust gas flow passage (). The rotary valve () comprises a valve rotor () which is rotatable to selectively permit or block flow to the LP turbine () from either the first exhaust gas passage () or the bypass gas passage ().


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