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.

Patent No.:

US 10787955 B1

PDF
Full Text
Expired
Date of Patent:
Sep. 29, 2020

Filed:

Mar. 03, 2017
Applicant:

Mitsubishi Heavy Industries, Ltd., Tokyo, JP;

Inventors:

Toyotaka Yoshida, Tokyo, JP;

Kunihiro Tomikawa, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02B 37/02 (2006.01); F02B 37/013 (2006.01); F02B 37/18 (2006.01); F02B 37/00 (2006.01);
U.S. Cl.
CPC ...
F02B 37/025 (2013.01); F02B 37/00 (2013.01); F02B 37/004 (2013.01); F02B 37/013 (2013.01); F02B 37/18 (2013.01); F02B 37/183 (2013.01); F05D 2220/40 (2013.01); F05D 2240/128 (2013.01); Y02T 10/144 (2013.01);
Abstract

A two-stage turbo system includes: a high-pressure stage turbocharger having a high-pressure stage turbine disposed in an exhaust passage of an engine; and a low-pressure stage turbocharger which includes a low-pressure stage turbine disposed downstream of the high-pressure stage turbine in the exhaust passage, and which is larger in size than the high-pressure stage turbocharger. The low-pressure stage turbine includes at least two scroll passages including a first scroll passage and a second scroll passage, which together form a scroll part for introducing exhaust gas into a nozzle flow passage of the low-pressure stage turbine. The scroll part is configured such that a first range of the nozzle flow passage into which the exhaust gas passing through the first scroll passage is introduced does not overlap with a second range of the nozzle flow passage into which the exhaust gas passing through the second scroll passage is introduced, in a circumferential direction of the nozzle flow passage.


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