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. 21, 2018

Filed:

Dec. 14, 2015
Applicant:

GM Global Technology Operations Llc, Detroit, MI (US);

Inventors:

Armando Mogavero, Turin, IT;

Fiorello Losano, Turin, IT;

Cesare Maria Meano, Turin, IT;

Eugenio Manta, Valdellatorre, IT;

Vincenzo Petronzi, Turin, IT;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02B 23/00 (2006.01); F02B 33/00 (2006.01); F02D 41/00 (2006.01); F02B 37/12 (2006.01); F02B 37/24 (2006.01); F02B 37/00 (2006.01); F02B 37/013 (2006.01); F02B 37/18 (2006.01); F02D 35/02 (2006.01);
U.S. Cl.
CPC ...
F02D 41/0007 (2013.01); F02B 37/004 (2013.01); F02B 37/013 (2013.01); F02B 37/127 (2013.01); F02B 37/183 (2013.01); F02B 37/24 (2013.01); F02D 35/023 (2013.01); F02D 2200/101 (2013.01); Y02T 10/144 (2013.01);
Abstract

A two stage turbocharger for an internal combustion engine, the two stage turbocharger comprising a high pressure turbine fluidly connected to an exhaust manifold of the engine through a high pressure turbine inlet duct and a low pressure turbine fluidly connected to the high pressure turbine through a low pressure turbine inlet duct, wherein the low pressure turbine is a variable geometry turbine, wherein the two stage turbocharger comprise a bypass duct system to bypass the variable geometry low pressure turbine, wherein the bypass duct system comprises a bypass valve.


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