Patents by Inventor Yasutsugu Takata

Yasutsugu Takata has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Publication number: 20240117772
    Abstract: A gas turbine system and control method for the gas turbine system that includes: a gas turbine including a compressor for producing compressed air, a combustor for burning fuel with the compressed air, and a turbine driven by combustion gas generated by burning fuel in the combustor; a motor generator drivable by the turbine and capable of providing rotational power to the gas turbine by electric power supplied from outside the gas turbine; a fuel flow determination device for determining a set value of a parameter used to control a flow rate of the fuel supplied to the combustor; and a fuel flow control device for controlling the flow rate of the fuel supplied to the combustor, based on the set value. The fuel flow determination device determines the set value such that the flow rate of the fuel is a lower limit value in a reverse power operation mode.
    Type: Application
    Filed: March 23, 2022
    Publication date: April 11, 2024
    Inventors: Hiroshi TANABE, Yasutsugu TAKATA, Kyosuke KAWANO
  • Patent number: 10815905
    Abstract: A control device includes a fuel equivalent value calculation unit for determining the flow rate of fuel supplied to a gas turbine in accordance with a target value deviation between an actual rotation speed and a target rotation speed, an upper limit deviation calculation unit for obtaining an upper limit deviation which is a deviation between a set upper limit output and an actual output, a lower limit deviation calculation unit for obtaining a lower limit deviation which is a deviation between a set lower limit output and the actual output, and a parameter-changing unit for changing any one parameter among the target rotation speed, the actual rotation speed, and the target value deviation so that the target value deviation decreases when the actual rotation speed decreases and the upper limit deviation is small, and so that the target value deviation increases when the actual rotation speed increases and the lower limit deviation is small.
    Type: Grant
    Filed: April 30, 2015
    Date of Patent: October 27, 2020
    Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
    Inventors: Hiroki Suzuki, Yasutsugu Takata, Yoshiaki Nakanishi, Masayuki Murakami
  • Publication number: 20170044994
    Abstract: A control device includes a fuel equivalent value calculation unit for determining the flow rate of fuel supplied to a gas turbine in accordance with a target value deviation between an actual rotation speed and a target rotation speed, an upper limit deviation calculation unit for obtaining an upper limit deviation which is a deviation between a set upper limit output and an actual output, a lower limit deviation calculation unit for obtaining a lower limit deviation which is a deviation between a set lower limit output and the actual output, and a parameter-changing unit for changing any one parameter among the target rotation speed, the actual rotation speed, and the target value deviation so that the target value deviation decreases when the actual rotation speed decreases and the upper limit deviation is small, and so that the target value deviation increases when the actual rotation speed increases and the lower limit deviation is small.
    Type: Application
    Filed: April 30, 2015
    Publication date: February 16, 2017
    Applicant: Mitsubishi Hitachi Power Systems, Ltd.
    Inventors: Hiroki SUZUKI, Yasutsugu TAKATA, Yoshiaki NAKANISHI, Masayuki MURAKAMI
  • Patent number: 8749085
    Abstract: Provided is a gas turbine control device that is used in a generating facility including a gas turbine and a generator for generating power when at least rotational power of the gas turbine is transmitted, the gas turbine control device including a first control section for obtaining a first fuel control command for causing generator output to follow a generator output set value decided based on a demand load, where the first control section has a feedback control section (60), and the feedback control section (60) includes a subtraction section (62) for calculating a deviation of the generator output with respect to the generator output set value, a PI control section (64) provided in a later stage of control than the subtraction section (62), and a peak suppression section (66) for suppressing a peak in amplitude characteristics of the generator or a utility grid including the generator.
    Type: Grant
    Filed: November 28, 2011
    Date of Patent: June 10, 2014
    Assignee: Mitsubishi Heavy Industries, Ltd.
    Inventors: Makoto Kishi, Yasuo Fujishima, Takashi Sonoda, Koichiro Hirato, Yasutsugu Takata, Fuminori Fujii
  • Publication number: 20130147208
    Abstract: Provided is a gas turbine control device that is used in a generating facility including a gas turbine and a generator for generating power when at least rotational power of the gas turbine is transmitted, the gas turbine control device including a first control section for obtaining a first fuel control command for causing generator output to follow a generator output set value decided based on a demand load, where the first control section has a feedback control section (60), and the feedback control section (60) includes a subtraction section (62) for calculating a deviation of the generator output with respect to the generator output set value, a PI control section (64) provided in a later stage of control than the subtraction section (62), and a peak suppression section (66) for suppressing a peak in amplitude characteristics of the generator or a utility grid including the generator.
    Type: Application
    Filed: November 28, 2011
    Publication date: June 13, 2013
    Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
    Inventors: Makoto Kishi, Yasuo Fujishima, Takashi Sonoda, Koichiro Hirato, Yasutsugu Takata, Fuminori Fujii