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:
Aug. 08, 2017

Filed:

Jun. 26, 2015
Applicant:

Ford Global Technologies, Llc, Dearborn, MI (US);

Inventors:

Franz J. Brinkmann, Huerth-Efferen, DE;

Kai Sebastian Kuhlbach, Bergisch Gladbach, DE;

Assignee:

Ford Global Technologies, LLC, Dearborn, MI (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02B 37/013 (2006.01); F02B 37/12 (2006.01); F02B 37/18 (2006.01); F02D 23/00 (2006.01); F02D 41/00 (2006.01); F02D 41/14 (2006.01); F02B 37/00 (2006.01); F02B 37/007 (2006.01);
U.S. Cl.
CPC ...
F02B 37/013 (2013.01); F02B 37/002 (2013.01); F02B 37/007 (2013.01); F02B 37/12 (2013.01); F02B 37/183 (2013.01); F02D 23/00 (2013.01); F02D 41/0007 (2013.01); F02D 41/1448 (2013.01); Y02T 10/144 (2013.01);
Abstract

An engine system for a motor vehicle is provided. The engine system includes a first exhaust-gas turbine in a first turbocharger driven by exhaust gas from the engine, a second exhaust-gas turbine in a second turbocharger driven by exhaust gas from the engine, a bypass coupled upstream and downstream of the first exhaust-gas turbine, and a pneumatic charge pressure control device including a bypass valve positioned in the bypass and a charge pressure control valve pneumatically coupled to the bypass valve and an intake line downstream of a first compressor included in the first turbocharger, the pneumatic charge pressure control device further including an adaptation unit pneumatically coupled to the bypass valve and an exhaust line upstream of the second exhaust-gas turbine.


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