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, 2019

Filed:

May. 18, 2017
Applicant:

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

Inventors:

Leon Hu, Dearborn, MI (US);

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

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01B 25/02 (2006.01); F01D 17/16 (2006.01); F01D 5/04 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 17/16 (2013.01); F01D 5/04 (2013.01); F01D 9/041 (2013.01); F05D 2220/40 (2013.01); F05D 2240/128 (2013.01); F05D 2240/80 (2013.01);
Abstract

Systems are provided for a nozzle blade for a variable nozzle turbine of a turbocharged engine. In one example, a nozzle blade for a turbine nozzle of a variable geometry turbine may include: a cambered outer surface that curves from an inlet end to an outlet end of the nozzle blade, relative to a chord of the nozzle blade, the chord having a chord length defined from the inlet end to the outlet end, the nozzle blade having an aspect ratio in a range of 1.54 to 2.95, a thickness that is greatest in a range of 47 to 61% of the chord length, and a camber line angle change ratio in a range of 0.94 to 1.16 from the inlet end to the outlet end of the nozzle blade.


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