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. 07, 2020

Filed:

May. 19, 2015
Applicant:

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

Inventors:

Keita Fujii, Kanagawa, JP;

Shin Akazawa, Kanagawa, JP;

Nobukazu Ishii, Kanagawa, JP;

Masahiro Matsubara, Kanagawa, JP;

Masayuki Murakami, Kanagawa, JP;

Fuminori Fujii, Kanagawa, JP;

Hiroshi Tanabe, Kanagawa, JP;

Masaru Takamatsu, Kanagawa, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/34 (2006.01); F23R 3/28 (2006.01); F02C 7/228 (2006.01); F23R 3/60 (2006.01); F02C 7/20 (2006.01); F02C 9/32 (2006.01); F02C 7/22 (2006.01); F02C 7/232 (2006.01);
U.S. Cl.
CPC ...
F23R 3/346 (2013.01); F02C 7/20 (2013.01); F02C 7/222 (2013.01); F02C 7/228 (2013.01); F02C 7/232 (2013.01); F02C 9/32 (2013.01); F23R 3/28 (2013.01); F23R 3/60 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/80 (2013.01); F05D 2240/35 (2013.01); F23R 2900/00016 (2013.01); F23R 2900/00017 (2013.01);
Abstract

A combustor replacement method and a gas turbine plant capable of efficiently replacing a combustor using an existing facility. The combustor replacement method includes a step of separating, from a plurality of fuel supply systems, a first combustor that includes a plurality of nozzle systems connected to any of the plurality of fuel supply systems and supplied with fuel from the connected fuel supply systems, and removing the first combustor from a gas turbine plant. The method includes a step of attaching a second combustor that includes fewer nozzle systems than the first combustor to the gas turbine plant, and a step of providing communication between the fuel supply systems connected to the same nozzle system of the second combustor by a coupling pipe, and coupling the fuel supply systems and the second combustor.


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