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. 12, 2021

Filed:

Jul. 16, 2019
Applicant:

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

Inventors:

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

Leon Hu, Bloomfield Hills, MI (US);

Dave R. Hanna, Troy, MI (US);

Jianwen James Yi, West Bloomfield, MI (US);

Eric Warren Curtis, Milan, MI (US);

Assignee:

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

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/66 (2006.01); F04D 25/02 (2006.01); F04D 29/051 (2006.01); F02C 6/12 (2006.01); F01D 3/00 (2006.01); F02B 37/12 (2006.01); F02B 37/04 (2006.01); F02B 37/14 (2006.01); F02B 37/10 (2006.01); F02D 23/00 (2006.01); F04D 17/10 (2006.01); F04D 25/04 (2006.01); F04D 29/16 (2006.01); F01D 5/04 (2006.01); F04D 29/28 (2006.01);
U.S. Cl.
CPC ...
F04D 29/662 (2013.01); F01D 3/00 (2013.01); F02B 37/04 (2013.01); F02B 37/10 (2013.01); F02B 37/12 (2013.01); F02B 37/14 (2013.01); F02C 6/12 (2013.01); F02D 23/00 (2013.01); F04D 17/10 (2013.01); F04D 25/024 (2013.01); F04D 25/045 (2013.01); F04D 29/051 (2013.01); F01D 5/048 (2013.01); F04D 29/162 (2013.01); F04D 29/284 (2013.01); F05D 2220/40 (2013.01); F05D 2260/15 (2013.01);
Abstract

Methods and systems are provided for a turbocharger system to reduce and balance axial thrust load on the turbine shaft and the associated bearing system and sealing. In one example, a partial back plate compressor may be used in combination with an axial turbine to reduce axial thrust load and to improve turbocharger transient response time. In another example, a regenerative turbocharger system with back-to-back turbo pump may be used to reduce and balance axial thrust load.


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