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. 05, 2019

Filed:

Mar. 01, 2017
Applicant:

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

Inventors:

Alain Lombard, Vosges, FR;

Stephane Pees, Ceintrey, FR;

Hani Mohtar, Chaumousey, FR;

Stephane Doise, Epinal, FR;

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/46 (2006.01); F04D 17/10 (2006.01); F04D 27/02 (2006.01); F04D 25/04 (2006.01); F02B 37/00 (2006.01); F02B 37/22 (2006.01); F04D 27/00 (2006.01); F02B 37/24 (2006.01); F04D 29/42 (2006.01); F04D 29/68 (2006.01); F16K 3/03 (2006.01); F02B 37/16 (2006.01);
U.S. Cl.
CPC ...
F04D 29/462 (2013.01); F02B 37/00 (2013.01); F02B 37/225 (2013.01); F02B 37/24 (2013.01); F04D 17/10 (2013.01); F04D 25/04 (2013.01); F04D 27/002 (2013.01); F04D 27/0246 (2013.01); F04D 27/0253 (2013.01); F04D 29/4213 (2013.01); F04D 29/464 (2013.01); F04D 29/681 (2013.01); F16K 3/03 (2013.01); F02B 37/16 (2013.01); F05D 2220/40 (2013.01); Y02T 10/144 (2013.01);
Abstract

A centrifugal compressor for a turbocharger includes an inlet-adjustment mechanism in an air inlet for the compressor, operable to move between an open position and a closed position in the air inlet. The inlet-adjustment mechanism includes a plurality of blades disposed about the air inlet and each pivotable about one end of the blade, the blades extending through a slot in the air inlet wall 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. Movement of the inlet-adjustment mechanism from the open position to the closed position is effective to shift the compressor's surge line to lower flow rates.


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