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:
Jun. 02, 2020

Filed:

Jun. 16, 2015
Applicant:

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

Inventors:

Takashi Sonoda, Tokyo, JP;

Akihiko Saito, Tokyo, JP;

Yoshifumi Iwasaki, Kanagawa, JP;

Ryuji Takenaka, Kanagawa, JP;

Kozo Toyama, Kanagawa, JP;

Koji Takaoka, Kanagawa, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/54 (2006.01); F02C 9/20 (2006.01); F02C 9/28 (2006.01); F02C 3/04 (2006.01); F02D 41/02 (2006.01); F02C 9/22 (2006.01); F02D 41/00 (2006.01); F02D 41/30 (2006.01); F02D 43/04 (2006.01); F02D 13/02 (2006.01);
U.S. Cl.
CPC ...
F02D 41/024 (2013.01); F02C 9/20 (2013.01); F02C 9/22 (2013.01); F02C 9/28 (2013.01); F02C 9/54 (2013.01); F02D 41/0002 (2013.01); F02D 41/30 (2013.01); F02D 43/04 (2013.01); F02C 3/04 (2013.01); F02D 13/0223 (2013.01); F02D 2041/0265 (2013.01); F02D 2200/02 (2013.01); F02D 2200/04 (2013.01); F02D 2200/0406 (2013.01); F02D 2200/0414 (2013.01); F02D 2200/0802 (2013.01); F05D 2270/112 (2013.01);
Abstract

Provided is a control device of a gas turbine including a compressor, a combustor, and a turbine. The control device executes load control of allowing an operation control point for operation control of a gas turbine to vary in response to a load of the gas turbine. The operation of the gas turbine is controlled on the basis of a rated temperature adjustment line for temperature adjustment control of a flue gas temperature at a predetermined load to a rated flue gas temperature at which performance of the gas turbine becomes rated performance, a preceding setting line for setting of the flue gas temperature at the predetermined load to a preceding flue gas temperature that becomes lower in precedence to the rated flue gas temperature, and a limit temperature adjustment line for temperature adjustment control.


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