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. 13, 2022

Filed:

Dec. 22, 2017
Applicant:

Mitsubishi Hitachi Power Systems, Ltd., Kanagawa, JP;

Inventors:

Yamato Shiramasa, Kanagawa, JP;

Ryuta Ito, Tokyo, JP;

Takayuki Kurimura, Tokyo, JP;

Yoshifumi Tsuji, Kanagawa, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F02C 7/18 (2006.01); F01D 9/04 (2006.01); F01D 25/24 (2006.01); F01D 11/18 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F02C 7/18 (2013.01); F01D 9/041 (2013.01); F01D 11/18 (2013.01); F01D 25/24 (2013.01); F05D 2240/11 (2013.01); F05D 2240/12 (2013.01); F05D 2260/201 (2013.01); F05D 2260/30 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A ring-segment surface-side member is included in a ring segment disposed at a position opposite to a turbine blade on a stationary side of a gas turbine, serves as a part of a combustion gas flow path through which combustion gas flows, and is formed of a ceramic matrix composite. The ring-segment surface-side member includes: a surface portion forming the combustion gas flow path; a turned-back portion including a first part extending outward in a radial direction of the gas turbine from the surface portion and a second part extending toward a central line of the surface portion from an end part of the first part; and a protrusion portion extending outward from the turned-back portion in the radial direction of the gas turbine.


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