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:
Mar. 14, 2023

Filed:

Feb. 20, 2018
Applicant:

Mitsubishi Heavy Industries Engine & Turbocharger, Ltd., Sagamihara, JP;

Inventors:

Takuya Arakawa, Tokyo, JP;

Takaya Futae, Tokyo, JP;

Shuichi Miura, Tokyo, JP;

Yosuke Danmoto, Sagamihara, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/04 (2006.01); F01D 5/04 (2006.01); F01D 25/16 (2006.01); F02B 39/14 (2006.01); F16C 3/02 (2006.01); F16C 17/02 (2006.01); F16C 23/04 (2006.01); F16C 33/10 (2006.01);
U.S. Cl.
CPC ...
F01D 25/04 (2013.01); F01D 5/048 (2013.01); F01D 25/166 (2013.01); F02B 39/14 (2013.01); F16C 3/02 (2013.01); F16C 17/02 (2013.01); F16C 23/045 (2013.01); F16C 33/1045 (2013.01); F05D 2220/40 (2013.01); F05D 2240/53 (2013.01); F05D 2260/96 (2013.01); F16C 2202/06 (2013.01); F16C 2360/24 (2013.01);
Abstract

A forced induction device () includes: a rotor () which includes a turbine side shaft portion (), a compressor side shaft portion (), and a connection shaft portion () connecting these to each other; a turbine side bearing () which supports the turbine side shaft portion (); and a compressor side bearing () which supports the compressor side shaft portion (). A rigidity of the connection shaft portion () is lower than that of the turbine side shaft portion () and the compressor side shaft portion () so that a node in a mode shape at each critical speed involving with an operating rotational speed region of the rotor () is located between the turbine side bearing () and the compressor side bearing ().


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