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:
Oct. 30, 2007

Filed:

Nov. 15, 2005
Applicants:

Ulrich Gobert, Göteborg, SE;

Lars Sundin, Malmö, SE;

Magnus Ising, Lund, SE;

Daniel Grunditz, Öjersjö, SE;

Per Andersson, Malmö, SE;

Kent Giselmo, Vellinge, SE;

Sebastian Krausche, Höllviken, SE;

Inventors:

Ulrich Gobert, Göteborg, SE;

Lars Sundin, Malmö, SE;

Magnus Ising, Lund, SE;

Daniel Grunditz, Öjersjö, SE;

Per Andersson, Malmö, SE;

Kent Giselmo, Vellinge, SE;

Sebastian Krausche, Höllviken, SE;

Assignee:

Volvo Lastvagnar AB, Gothenburg, SE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 37/00 (2006.01); F02B 37/02 (2006.01); F02B 37/013 (2006.01); F02B 33/44 (2006.01); F01D 25/26 (2006.01); F01D 25/24 (2006.01); F04D 29/60 (2006.01); F04D 29/40 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbocharger system for an internal combustion engine having at least one exhaust line for evacuating exhaust gases from the combustion chamber of the engine and at least one inlet line for supplying air to the combustion chamber. A high-pressure turbine interacts with a high-pressure compressor forming a high-pressure turbo unit with a common rotation axis. A low-pressure turbine interacts with a low-pressure compressor forming a low-pressure turbo unit with a common rotation axis. The high-pressure turbo unit and the low-pressure turbo unit are serially placed with the rotation axes essentially concentric and with the high-pressure turbine and the low-pressure turbine placed adjacent to each other and coupled together by an intermediate piece configured as a flow duct. The low-pressure turbo unit () is attached to one part of the internal combustion engine, while the high-pressure turbo unit is attached to another part of the engine.


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