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:
Sep. 21, 2021

Filed:

Mar. 01, 2016
Applicant:

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

Inventors:

Yuya Kojima, Tokyo, JP;

Takashi Nambu, Tokyo, JP;

Yosuke Dammoto, Tokyo, JP;

Takaya Futae, Tokyo, JP;

Shuichi Isayama, Tokyo, JP;

Yoji Akiyama, Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16N 7/28 (2006.01); F16C 33/10 (2006.01); F01M 11/02 (2006.01); F16C 17/04 (2006.01); F16N 31/00 (2006.01); F16H 57/04 (2010.01); F16N 29/02 (2006.01); F16C 33/66 (2006.01);
U.S. Cl.
CPC ...
F16N 7/28 (2013.01); F01M 11/02 (2013.01); F16C 17/04 (2013.01); F16C 33/101 (2013.01); F16C 33/103 (2013.01); F16C 33/1065 (2013.01); F16H 57/0423 (2013.01); F16H 57/0436 (2013.01); F16H 57/0457 (2013.01); F16N 29/02 (2013.01); F16N 31/00 (2013.01); F01M 2011/021 (2013.01); F16C 33/6666 (2013.01); F16C 2360/24 (2013.01); F16H 57/0447 (2013.01); F16H 57/0469 (2013.01); F16N 2210/14 (2013.01);
Abstract

The present invention improves the drainability of lubricating oil at a thrust bearing. The present invention comprises: a rotating shaft; a thrust bearing that is provided to the rotating shaft and restricts the axial-direction movement of the rotating shaft; and an oil reservoir part () that has formed therein an oil reservoir space () that is provided to be adjacent to the thrust bearing in the axial direction and to open downward, the oil reservoir space () having formed therein an inclined surface () that, in a region that is in and below a horizontal plane H that passes through the center of the rotating shaft, protrudes to the thrust bearing side and is inclined along the rotational direction of the rotating shaft.


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