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:
Oct. 02, 2018

Filed:

Jul. 21, 2015
Applicant:

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

Inventors:

Matthew Oakes, Petaluma, CA (US);

Filip Eckl, Dolni Kounice, CZ;

Christopher Arthur Carvalho, Claremont, CA (US);

Charles Robert Cadle, Redondo Beach, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 25/16 (2006.01); F02B 37/00 (2006.01); F02C 6/12 (2006.01); F04D 17/12 (2006.01); F04D 19/02 (2006.01); F04D 25/04 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F02B 37/004 (2013.01); F01D 25/243 (2013.01); F02C 6/12 (2013.01); F04D 17/12 (2013.01); F04D 19/02 (2013.01); F04D 25/045 (2013.01); F05D 2220/40 (2013.01); F05D 2230/642 (2013.01); F05D 2240/40 (2013.01); F05D 2240/55 (2013.01); F05D 2250/311 (2013.01); F05D 2250/36 (2013.01); F05D 2250/51 (2013.01); F05D 2250/52 (2013.01); F05D 2250/611 (2013.01); F05D 2260/39 (2013.01); Y02T 10/144 (2013.01);
Abstract

Turbine assemblies and related turbocharger systems having direct turbine interfaces are provided. One exemplary turbine assembly includes a first turbine housing having an outlet portion defining a fluid outlet of a first turbine and a second turbine housing having an inlet portion defining a fluid inlet of a second turbine, wherein at least a portion of the inlet portion radially surrounds at least a portion of the outlet portion to provide a direct interface from the fluid outlet of the first turbine to the fluid inlet of the second turbine in an axial direction.


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