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. 27, 2016

Filed:

Apr. 02, 2013
Applicant:

Kawasaki Jukogyo Kabushiki Kaisha, Kobe-shi, Hyogo, JP;

Inventors:

Kazuhiko Tanimura, Akashi, JP;

Ryozo Tanaka, Kakogawa, JP;

Takao Sugimoto, Kobe, JP;

Hiroshi Morishita, Kobe, JP;

Karsten Kusterer, Moresnet, BE;

Dieter Bohn, Moers, DE;

Rene Braun, Aachen, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01K 23/10 (2006.01); F02C 6/18 (2006.01); F02C 1/05 (2006.01); F02C 7/143 (2006.01); F02C 7/08 (2006.01); F03G 6/00 (2006.01); F03G 6/06 (2006.01); F01K 25/08 (2006.01);
U.S. Cl.
CPC ...
F01K 23/10 (2013.01); F01K 25/08 (2013.01); F02C 1/05 (2013.01); F02C 6/18 (2013.01); F02C 7/08 (2013.01); F02C 7/143 (2013.01); F03G 6/005 (2013.01); F03G 6/064 (2013.01); F03G 6/067 (2013.01); Y02E 10/46 (2013.01); Y02E 20/14 (2013.01); Y02E 20/16 (2013.01);
Abstract

A combined-type gas turbine engine system is provided which achieves high efficiency by very effectively using exhaust heat from a gas turbine engine. In a gas turbine engine system including: a compressor for compressing a first working medium; a heater for heating the compressed first working medium by an external heat source; a turbine for outputting power from the first working medium; an intermediate cooler provided at the compressor for cooling the first working medium compressed by a low-pressure compression part of the compressor and supplying the first working medium to a high-pressure compression part of the compressor; and an exhaust heat boiler using as a heating medium an exhaust gas from the turbine, a Rankine cycle engine using the intermediate cooler and the exhaust heat boiler as heat sources and a cooling medium of the intermediate cooler as a second working medium.


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