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:
May. 17, 2022

Filed:

Dec. 18, 2019
Applicant:

Mitsubishi Power, Ltd., Yokohama, JP;

Inventors:

Hironori Tsukidate, Yokohama, JP;

Kunihiro Oga, Yokohama, JP;

Yoshitaka Terada, Yokohama, JP;

Koichi Nishida, Yokohama, JP;

Assignee:

Mitsubishi Power, Ltd., Yokohama, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F02C 7/22 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F23R 3/286 (2013.01); F02C 7/22 (2013.01); F05D 2240/35 (2013.01); F23D 2900/00008 (2013.01); F23D 2900/14004 (2013.01); F23R 3/343 (2013.01); F23R 2900/00014 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/03042 (2013.01); F23R 2900/03343 (2013.01);
Abstract

The present invention reduces the concentration of thermal stress on a burner. A gas turbine combustor receiving compressed air from a compressor, mixing the compressed air with a fuel, burning the mixture to generate a combustion gas, and supplying the combustion gas to a turbine. The combustor includes: an inner cylinder internally forming a combustion chamber; an outer cylinder covering the inner cylinder and forming a cylindrical outer circumferential flow path between the inner and outer cylinders to allow the compressed air to flow; and a burner mounted on an end of the outer cylinder, which is positioned on an opposite side to a turbine side, and facing the combustion chamber. The burner includes a cylindrical base frame including a cavity distributing the fuel, and fuel nozzles circularly arranged as viewed from the combustion chamber and connected to the cavity. When viewed from the combustion chamber, slits extending radially are formed in the base frame such that each separate the circumferentially adjacent fuel nozzles from each other.


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