Patents by Inventor Gwang Nyeon RYU

Gwang Nyeon RYU 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).

  • Patent number: 11149592
    Abstract: A composite power generating device of the present invention includes an engine (110), a first flow line (121), a turbocharger (130), a second flow line (122), a third flow line (123), a compressor (211), a first medium line (221), a medium turbine (212), a second medium line (222), a working medium cooler (213), a recuperator (215), a power generating unit (214), a cross-line (233), a first heat exchanger (251), a second heat exchanger (252), and a third heat exchanger (253).
    Type: Grant
    Filed: January 22, 2018
    Date of Patent: October 19, 2021
    Assignee: HYUNDAI HEAVY INDUSTRIES CO., LTD.
    Inventors: Gwang Nyeon Ryu, Jin Ki Ham, Beom Joo Kim, Cheol Hee Lee
  • Publication number: 20200200049
    Abstract: A composite power generating device of the present invention includes an engine (110), a first flow line (121), a turbocharger (130), a second flow line (122), a third flow line (123), a compressor (211), a first medium line (221), a medium turbine (212), a second medium line (222), a working medium cooler (213), a recuperator (215), a power generating unit (214), a cross-line (233), a first heat exchanger (251), a second heat exchanger (252), and a third heat exchanger (253).
    Type: Application
    Filed: January 22, 2018
    Publication date: June 25, 2020
    Inventors: Gwang Nyeon RYU, Jin Ki HAM, Beom Joo KIM, Cheol Hee LEE
  • Patent number: 9989253
    Abstract: A gas turbine combustion instability control device has a combustion unit provided with a hollow combustion chamber, a gas turbine connected to the inside of the combustion chamber and a dynamic pressure sensor which is provided to the inside of the combustion chamber and measures the combustion dynamics of the inside of the combustion chamber; a diagnosis module which processes combustion dynamic pressure signals (p) according to the combustion dynamics measured by the dynamic pressure sensor to calculate the kurtosis value (k) of the dynamic pressure signals, and compares the same with a kurtosis reference value (kth) to evaluate the combustion instability; and a combustion control unit for controlling the operation of the combustion part according to the determination of the diagnosis module.
    Type: Grant
    Filed: November 20, 2013
    Date of Patent: June 5, 2018
    Assignees: Hanbat National University Industry-Academic Cooperation Foundation, Hyundai Heavy Industries Co., Ltd.
    Inventors: Dong Jin Cha, Won Joon Song, Kwang Ho Ahn, Gwang Nyeon Ryu
  • Publication number: 20150377485
    Abstract: A gas turbine combustion instability control device has a combustion unit provided with a hollow combustion chamber, a gas turbine connected to the inside of the combustion chamber and a dynamic pressure sensor which is provided to the inside of the combustion chamber and measures the combustion dynamics of the inside of the combustion chamber; a diagnosis module which processes combustion dynamic pressure signals (p) according to the combustion dynamics measured by the dynamic pressure sensor to calculate the kurtosis value (k) of the dynamic pressure signals, and compares the same with a kurtosis reference value (kth) to evaluate the combustion instability; and a combustion control unit for controlling the operation of the combustion part according to the determination of the diagnosis module.
    Type: Application
    Filed: November 20, 2013
    Publication date: December 31, 2015
    Applicants: Hanbat National University Industry-Academic Cooperation Foundation, Hyundai Heavy Industries Co., Ltd.
    Inventors: Dong Jin Cha, Won Joon Song, Kwang Ho Ahn, Gwang Nyeon RYU