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:
Jan. 28, 2020

Filed:

Feb. 28, 2018
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Hani Mohtar, Chaumousey, FR;

Stephane Pees, Ceintrey, FR;

Stephane Doise, Epinal, FR;

Alain Lombard, Vosges, FR;

Assignee:

Garrett Transportation I Inc., Torrance, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/66 (2006.01); F02B 37/24 (2006.01); F04D 29/46 (2006.01); F16K 3/03 (2006.01); F04D 15/00 (2006.01);
U.S. Cl.
CPC ...
F04D 29/667 (2013.01); F02B 37/24 (2013.01); F04D 15/0022 (2013.01); F04D 29/462 (2013.01); F16K 3/03 (2013.01);
Abstract

A centrifugal compressor for a turbocharger includes an inlet-adjustment mechanism operable to move between an open position and a closed position. The inlet-adjustment mechanism includes a plurality of blades disposed about the compressor air inlet and located within an annular space within the air inlet wall. The blades are pivotable about respective pivot points such that the blades extend radially inward from the annular space into the air inlet when the blades are in the closed position so as to form an orifice of reduced diameter relative to a nominal diameter of the inlet. Downstream surfaces of the blades include vortex reducers that are structured and arranged to reduce a strength of an unsteady vortex generated from the radially inner edges of the blades.


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