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. 13, 2018

Filed:

Jul. 08, 2015
Applicant:

Dr. Ing. H.c. F. Porsche Aktiengesellschaft, Stuttgart, DE;

Inventor:

Werner Verdoorn, Ludwigsburg, DE;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02B 37/18 (2006.01); F02B 33/40 (2006.01); F02B 37/007 (2006.01); F02B 37/013 (2006.01); F02B 37/00 (2006.01); F02B 37/02 (2006.01); F02D 13/02 (2006.01); F01N 13/10 (2010.01);
U.S. Cl.
CPC ...
F02B 37/183 (2013.01); F02B 33/40 (2013.01); F02B 37/001 (2013.01); F02B 37/004 (2013.01); F02B 37/007 (2013.01); F02B 37/013 (2013.01); F02B 37/02 (2013.01); F02D 13/0242 (2013.01); F02D 13/0257 (2013.01); F01N 13/107 (2013.01); Y02T 10/144 (2013.01); Y02T 10/18 (2013.01);
Abstract

Exhaust gas from a first outlet port () of a cylinder () of a combustion engine () can flow through the first turbocharger (), and exhaust gas from a second outlet port () of the cylinder () can flow through the second turbocharger (). A first connecting duct () can supply the second turbine () with exhaust gas from the first turbine (). The first connecting duct () is connected to a first bypass duct () that issues into a tailpipe line () downstream of the second turbine () to bypass the second turbine (). The first bypass duct () has a second control valve () that can block the first bypass duct (). The first connecting duct () has a first control valve () that can block the first connecting duct () to prevent exhaust gas from flowing through the first turbine () to the second turbine ().


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