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. 27, 2013

Filed:

Jan. 19, 2010
Applicants:

Harold Huimin Sun, West Bloomfield, MI (US);

Dave Hanna, Troy, MI (US);

Jizhong Zhang, West Bloomfield, MI (US);

Liangjun HU, West Bloomfield, MI (US);

Eric M. Krivitzky, Brownsville, VT (US);

Louis M. Larosiliere, Quechee, VT (US);

Nicholas C. Baines, Kidlington, GB;

Inventors:

Harold Huimin Sun, West Bloomfield, MI (US);

Dave Hanna, Troy, MI (US);

Jizhong Zhang, West Bloomfield, MI (US);

Liangjun Hu, West Bloomfield, MI (US);

Eric M. Krivitzky, Brownsville, VT (US);

Louis M. Larosiliere, Quechee, VT (US);

Nicholas C. Baines, Kidlington, GB;

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F04D 27/02 (2006.01);
U.S. Cl.
CPC ...
Abstract

In one example, a turbocharger for an internal combustion engine is described. The turbocharger comprises a casing containing an impeller having a full blade coupled to a hub that rotates about an axis of rotation. The casing includes a bleed port and an injection port. The full blade includes a hub edge, a casing edge, and a first distribution of angles, each angle measured between the axis of rotation and a mean line at the hub edge at a meridional distance along the hub edge. The full blade includes a second distribution of angles, each angle measured between the axis of rotation and a mean line at the casing edge at a meridional distance along the casing edge. Further, various systems are described for affecting the aerodynamic properties of the compressor and turbine components in a way that may extend the operating range of the turbocharger.


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