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:
Jul. 16, 2019

Filed:

Oct. 13, 2017
Applicant:

Doosan Heavy Industries & Construction Co., Ltd., Changwon-si, Gyeongsangnam-do, KR;

Inventors:

Yeong Chun Kim, Changwon-si, KR;

Jeong Min Kim, Changwon-si, KR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F01D 25/24 (2006.01); F01D 25/28 (2006.01); F02C 7/06 (2006.01); F02C 7/20 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/16 (2013.01); F01D 25/162 (2013.01); F01D 25/24 (2013.01); F01D 25/28 (2013.01); F01D 25/285 (2013.01); F02C 7/04 (2013.01); F02C 7/06 (2013.01); F02C 7/20 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/72 (2013.01); F05D 2240/52 (2013.01); F05D 2240/90 (2013.01);
Abstract

A gas turbine comprises a strut assembly including an inner ring; an inclined member including a first end connected to the inner ring, a second end positioned opposite the first end, and a flange extending radially inward from the second end; an oil sump mounted to the second end or the flange; a thrust bearing fixed to the oil sump; and a thrust collar extending radially from a rotor, wherein the inclined member has an aperture portion formed therein, the aperture portion is positioned in an upper portion of a region between the thrust bearing and a journal bearing, and the aperture portion has a width and a circumferential length greater than at least the journal bearing. The gas turbine has the feature that the journal bearing is easily withdrawn and the total weight of the gas turbine is reduced.


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