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. 13, 2022

Filed:

Aug. 07, 2018
Applicant:

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

Inventors:

Yutaka Fujita, Tokyo, JP;

Yosuke Danmoto, Sagamihara, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/12 (2006.01); F02B 39/00 (2006.01); F04D 29/26 (2006.01); F04D 29/28 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F02C 6/12 (2013.01); F02B 39/00 (2013.01); F01D 9/026 (2013.01); F04D 29/266 (2013.01); F04D 29/284 (2013.01); F05D 2220/40 (2013.01); F05D 2240/60 (2013.01); F05D 2250/292 (2013.01); F05D 2260/31 (2013.01);
Abstract

A turbine shaft used for a turbocharger including a turbine and a compressor includes a turbine impeller, and a rotor shaft joined on one end side to the turbine impeller. The rotor shaft includes a fitting region configured to fit with a compressor impeller of the compressor by inserting the other end side of the rotor shaft into a through hole formed in the compressor impeller, a fastening region formed between the fitting region and the other end side of the rotor shaft, and configured to allow fastening by a fastening part, and a tapered part having a maximum outer diameter at a position closest to the turbine impeller in the fitting region and formed such that an outer diameter of the rotor shaft decreases from the position closest to the turbine impeller toward a tip side of the compressor impeller.


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