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:
Jul. 04, 2017

Filed:

Apr. 12, 2015
Applicant:

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

Inventors:

Raphaël Hettinger, La Baffe, FR;

Raphaël Boileau, Thaon les Vosges, FR;

Fréderic Daguin, Epinal, FR;

José Antonio Molina, Vitoria-Gasteiz, ES;

Tomás Moriñigo, Vitoria, ES;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 19/06 (2006.01); F16C 27/04 (2006.01); F16C 19/54 (2006.01); F16C 33/66 (2006.01); F01D 25/16 (2006.01); F02C 6/12 (2006.01); F02C 7/06 (2006.01); F16C 25/08 (2006.01); F16C 19/16 (2006.01);
U.S. Cl.
CPC ...
F01D 25/164 (2013.01); F02C 6/12 (2013.01); F02C 7/06 (2013.01); F16C 19/548 (2013.01); F16C 25/083 (2013.01); F16C 33/6659 (2013.01); F05D 2220/40 (2013.01); F05D 2240/54 (2013.01); F05D 2260/602 (2013.01); F05D 2300/43 (2013.01); F16C 19/163 (2013.01);
Abstract

A turbocharger bearing assembly can include a spacer that includes an axial through bore, a compressor side surface and a turbine side surface; a compressor side rolling element bearing that includes an outer race surface that faces the compressor side surface of the spacer; a turbine side rolling element bearing that includes an outer race surface that faces the turbine side surface of the spacer; and a spring seated between a first end cap disposed at least in part in the axial through bore of the spacer and a second end cap disposed at least in part in the axial through bore of the spacer where the spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing and where the spring biases an axially facing surface of the second end cap against the outer race surface of the turbine side rolling element bearing.


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