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:
Nov. 11, 2014

Filed:

Apr. 18, 2011
Applicants:

Carnell E. Williams, Southfield, MI (US);

Timothy J. Johnson, Auburn Hills, MI (US);

Tracy M. Farell, Grand Blanc, MI (US);

Kulwinder Singh, Rochester Hills, MI (US);

Gary J. Hazelton, White Lake, MI (US);

Inventors:

Carnell E. Williams, Southfield, MI (US);

Timothy J. Johnson, Auburn Hills, MI (US);

Tracy M. Farell, Grand Blanc, MI (US);

Kulwinder Singh, Rochester Hills, MI (US);

Gary J. Hazelton, White Lake, MI (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 27/02 (2006.01); F04D 29/44 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 29/441 (2013.01); F04D 29/681 (2013.01);
Abstract

A turbocharger compressor includes a compressor housing having a housing wall that includes a shroud that defines a central air channel and a compressor inlet in fluid communication with the central channel and an inlet duct. It also includes a compressor wheel configured to draw air into the compressor inlet from the inlet duct and create a main airflow in the central air channel axially toward a compressor outlet. The compressor also includes a bypass channel that extends between an opening in the main channel located between the compressor inlet and compressor outlet proximate the compressor blades and the compressor inlet. The compressor also includes a deflector that includes a deflector surface that is configured to direct a bypass airflow in the bypass channel, and flowing in a direction from the main channel toward the compressor inlet, into the compressor inlet axially and radially inwardly toward the compressor wheel.


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