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Title:
ガスタービンシステムおよび制御方法
Document Type and Number:
Japanese Patent JP6582331
Kind Code:
B2
Abstract:
A gas turbine control device for a gas turbine system includes a sensing unit for measuring the rotor speed and the output of the power generator; a speed regulation rate setting unit for calculating an actual speed regulation rate based on the measured rotor speed and the measured output of the power generator, and for setting a reference speed regulation rate based on the actual speed regulation rate and the target speed regulation rate; and a fuel amount control unit for controlling an amount of fuel supplied to the combustor based on the set reference speed regulation rate. Stable system operation is secured by a method of controlling the gas turbine system to satisfy a target speed regulation rate if additional power should be supplied due to sudden load fluctuations or a failure at another power plant.

Inventors:
Choi, Byun Hee
Application Number:
JP2018044931A
Publication Date:
October 02, 2019
Filing Date:
March 13, 2018
Export Citation:
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Assignee:
Dothan Heavy Industries and Construction Company Limited
International Classes:
F02C9/28; F01D15/10; F02C7/22
Domestic Patent References:
JP2016153645A
JP2003239763A
JP2000170548A
JP60030404A
JP54158507A
Foreign References:
US20140260293
US20140060065
Attorney, Agent or Firm:
Longhua International Patent Service Corporation