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:
Aug. 22, 2023

Filed:

Jun. 27, 2018
Applicants:

Mitsubishi Power Americas, Inc., Lake Mary, FL (US);

Mitsubishi Power, Ltd., Yokohama, JP;

Inventor:

Shimin Deng, Oakville, CA;

Assignees:

Mitsubishi Power Americas, Inc., Lake Mary, FL (US);

Mitsubishi Power, Ltd., Yokohama, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/04 (2006.01); F01K 23/10 (2006.01); F02C 7/18 (2006.01); F02C 7/22 (2006.01); F02C 7/224 (2006.01);
U.S. Cl.
CPC ...
F02C 6/04 (2013.01); F01K 23/10 (2013.01); F02C 7/18 (2013.01); F02C 7/22 (2013.01); F02C 7/224 (2013.01); F05D 2220/32 (2013.01); F05D 2220/722 (2013.01); F05D 2240/36 (2013.01); F05D 2260/232 (2013.01);
Abstract

A gas turbine combined-cycle power plant can comprise a gas turbine engine, a heat recovery steam generator, a steam turbine, a fuel regasification system and a Rankine Cycle system. The gas turbine engine can comprise a compressor for generating compressed air, a combustor that can receive a fuel and the compressed air to produce combustion gas, and a turbine for receiving the combustion gas and generating exhaust gas. The heat recovery steam generator is configured to generate steam from water utilizing the exhaust gas. The steam turbine is configured to produce power from steam from the heat recovery steam generator. The fuel regasification system is configured to convert the fuel from a liquid to a gas before entering the combustor. The Organic Rankine Cycle system is configured to cool compressed air extracted from the compressor to cool the gas turbine engine, and heat liquid fuel entering the fuel regasification system.


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