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:
Jan. 30, 2024

Filed:

Feb. 13, 2020
Applicant:

Mitsubishi Heavy Industries, Ltd., Tokyo, JP;

Inventors:

Yuichi Nakatani, Tokyo, JP;

Yuki Morisaki, Tokyo, JP;

Yasuhiro Saiki, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/30 (2006.01); B64D 27/24 (2006.01); F01D 15/10 (2006.01); F02C 6/00 (2006.01); F02K 1/34 (2006.01); F02K 1/38 (2006.01);
U.S. Cl.
CPC ...
F01D 25/30 (2013.01); B64D 27/24 (2013.01); B64D 33/06 (2013.01); F01D 15/10 (2013.01); F02C 6/00 (2013.01); F02K 1/34 (2013.01); F02K 1/386 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2240/35 (2013.01);
Abstract

A gas turbine system includes: a compressor configured to compress external air to generate compressed air; a combustor configured to burn the compressed air together with fuel to generate a combustion gas; a turbine configured to be driven by the combustion gas; an exhaust unit configured to guide the combustion gas, which has passed through the turbine, to outside; a shell having a cylindrical shape and extending along an axis line about which the turbine is configured to rotate and being arranged so as to cover the compressor, the combustor, the turbine, and the exhaust unit; and an exit unit configured to guide the combustion gas, which has passed through the turbine, to a discharge port in the surface of the shell.


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