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:
Feb. 19, 2019

Filed:

Apr. 10, 2016
Applicant:

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

Inventors:
Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 27/04 (2006.01); F01D 25/18 (2006.01); F01D 25/16 (2006.01); F04D 29/053 (2006.01); F04D 29/056 (2006.01); F04D 29/059 (2006.01); F04D 29/063 (2006.01); F02C 6/12 (2006.01); F16C 35/077 (2006.01); F16C 25/08 (2006.01); F04D 29/42 (2006.01); F02B 37/00 (2006.01); F16C 19/16 (2006.01); F16C 19/54 (2006.01);
U.S. Cl.
CPC ...
F01D 25/18 (2013.01); F01D 25/16 (2013.01); F01D 25/162 (2013.01); F02C 6/12 (2013.01); F04D 29/053 (2013.01); F04D 29/059 (2013.01); F04D 29/0563 (2013.01); F04D 29/063 (2013.01); F16C 25/083 (2013.01); F16C 35/077 (2013.01); F02B 37/00 (2013.01); F04D 29/4206 (2013.01); F05D 2220/40 (2013.01); F05D 2260/38 (2013.01); F16C 19/163 (2013.01); F16C 19/548 (2013.01); F16C 2360/24 (2013.01);
Abstract

An assembly can include a turbocharger center housing that includes a through bore that extends between a compressor end and a turbine end of the turbocharger center housing where the through bore includes a sleeve mating surface; and a sleeve positioned at least in part in the through bore of the turbocharger center housing where the sleeve includes an outer mating surface, an inner compressor side bearing lubricant film formation surface disposed at a first radius, an inner turbine side bearing lubricant film formation surface disposed at a second radius, and a surface between the inner compressor side bearing lubricant film formation surface and the inner turbine side bearing lubricant film formation surface that includes a third radius that is less than the first radius and less than the second radius and where outer mating surface of the sleeve contacts the sleeve mating surface of the turbocharger center.


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