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:
Apr. 06, 2021

Filed:

Sep. 21, 2018
Applicant:

Kawasaki Jukogyo Kabushiki Kaisha, Kobe, JP;

Inventors:

Koji Terauchi, Kobe, JP;

Ryoji Tamai, Akashi, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F02C 7/00 (2006.01); F01D 9/04 (2006.01); F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 25/246 (2013.01); F01D 9/04 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F01D 25/243 (2013.01); F02C 7/00 (2013.01); F05D 2240/11 (2013.01); F05D 2240/128 (2013.01); F05D 2240/14 (2013.01); F05D 2260/30 (2013.01);
Abstract

Provided is a structure in which nozzles of a turbine of a gas turbine and a shroud of the turbine are supported by a turbine casing. Each nozzle includes an outer circumferential flange having a front end portion and a rear end portion respectively engaged with an inner circumferential portion of the turbine casing, a front end portion of the shroud is engaged with the rear end portion of the outer circumferential flange located frontward thereof, a rear end portion of the shroud is engaged with the front end portion of the outer circumferential flange located rearward thereof, and the nozzle and the shroud are supported by the turbine casing through a support pin penetrating a superposition engagement portion at which engagement portions of the turbine casing, the outer circumferential flange, and the shroud are radially superposed on each other.


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