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:
Jan. 26, 2021

Filed:

Apr. 06, 2018
Applicant:

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

Inventors:

Filip Eckl, Dolni Kounice, CZ;

Petr Pribyl, Zdar nad Sazavou, CZ;

Petr Skara, Prague, CZ;

Pavel Foucek, Brno, CZ;

Ashraf Mohamed, Torrance, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F02C 6/12 (2006.01); F02B 37/18 (2006.01); F02B 37/02 (2006.01); F02B 37/013 (2006.01);
U.S. Cl.
CPC ...
F02C 6/12 (2013.01); F01D 17/165 (2013.01); F02B 37/025 (2013.01); F02B 37/183 (2013.01); F02B 37/013 (2013.01); F05D 2220/40 (2013.01); F05D 2240/10 (2013.01);
Abstract

A turbocharger has a meridionally divided turbine housing defining a first scroll and a first nozzle, and a second scroll and a second nozzle. The first and second nozzles are divided from each other by a shroud plate mounted within the nozzle, for isolating the exhaust gas streams flowing through the two nozzles from each other. A plurality of circumferentially spaced vanes are rotatably mounted at a radially inner side of the nozzles. Leading-edge portions of the vanes are slotted to receive the shroud plate when the vanes are pivoted open. Trailing-edge portions of the vanes are unslotted. A radially inner periphery of the shroud plate includes cutouts for abutting the trailing-edge portions of the vanes in the closed position, and includes contour portions for influencing a flow separation ratio of the turbine.


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