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:
Dec. 26, 2017

Filed:

Aug. 17, 2015
Applicant:

Electro-motive Diesel, Inc., LaGrange, IL (US);

Inventors:

Raji Rexavier, Plainfield, IL (US);

Gary Svihla, Burr Ridge, IL (US);

Alan Wiedmeyer, Aurora, IL (US);

Assignee:

Electro-Motive Diesel, Inc., LaGrange, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02D 23/00 (2006.01); F04D 29/30 (2006.01); F04B 17/00 (2006.01); F02M 26/04 (2016.01); F02B 37/00 (2006.01); F01D 5/02 (2006.01); F01D 11/00 (2006.01); F01D 25/16 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F02M 26/04 (2016.02); F01D 5/025 (2013.01); F01D 11/005 (2013.01); F01D 25/16 (2013.01); F01D 25/24 (2013.01); F02B 37/00 (2013.01); F05D 2220/40 (2013.01); F05D 2230/232 (2013.01); F05D 2230/60 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01); Y02T 10/144 (2013.01);
Abstract

This document discloses an exhaust gas turbocharger, which includes a turbine disk connected to a turbine disk hub. The turbine disk hub extends distally away from the turbine disk and towards a shaft that connects the turbine disk to a compressor. The shaft includes a proximal end that includes a shaft hub that extends proximally away from the shaft and towards the turbine disk hub. The turbine disk hub is coaxially connected to the shaft hub at a joint. The turbine disk hub and the shaft hub form a cavity between the turbine disk and the proximal end of the shaft. The turbocharger also includes a sleeve having an inner surface that surrounds and engages at least part of the turbine disk hub, at least part of the shaft hub and that further surrounds the joint and partially surrounds the cavity. The sleeve provides structural reinforcement for the joint and additional cooling functions beyond the cooling function provided by the cavity.


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