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. 21, 2017

Filed:

Feb. 06, 2015
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Hani Mohtar, Chaumousey, FR;

Stephane Pees, Meurthe-et-Moselle, FR;

Pascal Delapierre, Vaxoncourt, FR;

William Joseph Smith, Gardena, CA (US);

Pascal Villemin, Girancourt, FR;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/00 (2006.01); F02B 37/24 (2006.01); F01D 17/14 (2006.01); F04D 27/02 (2006.01); F02C 6/12 (2006.01); F04D 29/46 (2006.01); F01D 5/02 (2006.01); F01D 25/24 (2006.01); F02B 33/40 (2006.01); F04D 17/10 (2006.01); F04D 29/42 (2006.01);
U.S. Cl.
CPC ...
F02B 37/24 (2013.01); F01D 5/02 (2013.01); F01D 17/141 (2013.01); F01D 25/24 (2013.01); F02B 33/40 (2013.01); F02C 6/12 (2013.01); F04D 17/10 (2013.01); F04D 27/0253 (2013.01); F04D 29/4206 (2013.01); F04D 29/4213 (2013.01); F04D 29/464 (2013.01); F05D 2220/40 (2013.01); F05D 2240/24 (2013.01); F05D 2250/51 (2013.01); F05D 2270/101 (2013.01);
Abstract

A centrifugal compressor for a turbocharger includes a passive or semi-passive inlet-adjustment mechanism in an air inlet for the compressor, operable to move between an open position and a closed position solely by aerodynamic forces on the mechanism. The inlet-adjustment mechanism includes a plurality of flexible vanes collectively forming a duct, and an effective diameter of the air inlet at the inducer portion of the compressor wheel is determined by a trailing edge inside diameter of the duct. The vanes are movable solely or in part by aerodynamic forces exerted on the vanes by the air flowing to the compressor wheel. The duct has a tapering configuration when the vanes are in a relaxed state, but under aerodynamic force the vanes flex outwardly and increase the trailing edge inside diameter of the duct, thereby increasing an effective diameter of the air inlet.


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