Patents by Inventor Ievdoshyn Andrii

Ievdoshyn Andrii 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: 11753954
    Abstract: Disclosed are a compressor, which is a cantilever type that is easy to manufacture and assemble, and is capable of minimizing the vane tip clearance as the elastic member absorbs the impact and is compressed when the vane collides with the shroud segment due to expansion of the vane, and a gas turbine including the same.
    Type: Grant
    Filed: January 31, 2023
    Date of Patent: September 12, 2023
    Assignee: DOOSAN ENERBILITY CO., LTD.
    Inventors: Oleksiy Korepin, Ievdoshyn Andrii, Dong Woo Ham
  • Publication number: 20230250729
    Abstract: Disclosed are a compressor, which is a cantilever type that is easy to manufacture and assemble, and is capable of minimizing the vane tip clearance as the elastic member absorbs the impact and is compressed when the vane collides with the shroud segment due to expansion of the vane, and a gas turbine including the same.
    Type: Application
    Filed: January 31, 2023
    Publication date: August 10, 2023
    Inventors: Oleksiy Korepin, Ievdoshyn Andrii, Dong Woo Ham
  • Patent number: 11371527
    Abstract: A compressor rotor disk for a gas turbine includes a circumferential surface; and a plurality of dovetail slots formed along the circumferential surface, each dovetail slot comprising a cutout portion formed by removing a portion of a radially outer convex surface of the dovetail slot. The compressor rotor disk can reduce stresses generated in the compressor rotor disk by centrifugal force, by reducing the centrifugal force of the compressor rotor disk through the formation of the cutout portion at the radially outer portion of the compressor rotor disk, thereby enhancing the durability and reliability of the compressor rotor disk.
    Type: Grant
    Filed: July 13, 2018
    Date of Patent: June 28, 2022
    Inventors: Goroshchak Iurii, Ievdoshyn Andrii
  • Patent number: 10787908
    Abstract: Disclosed herein is a disk assembly for a gas turbine compressor, which comprises a partition wall formed to partition a space between disks for a gas turbine compressor to optimize a cooling fluid path.
    Type: Grant
    Filed: February 1, 2018
    Date of Patent: September 29, 2020
    Assignee: Doosan Heavy Industries Construction Co., Ltd
    Inventors: Kyu Sic Hwang, Ievdoshyn Andrii
  • Publication number: 20190078584
    Abstract: A compressor rotor disk for a gas turbine includes a circumferential surface; and a plurality of dovetail slots formed along the circumferential surface, each dovetail slot comprising a cutout portion formed by removing a portion of a radially outer convex surface of the dovetail slot. The compressor rotor disk can reduce stresses generated in the compressor rotor disk by centrifugal force, by reducing the centrifugal force of the compressor rotor disk through the formation of the cutout portion at the radially outer portion of the compressor rotor disk, thereby enhancing the durability and reliability of the compressor rotor disk.
    Type: Application
    Filed: July 13, 2018
    Publication date: March 14, 2019
    Inventors: GOROSHCHAK IURII, IEVDOSHYN ANDRII
  • Publication number: 20180223669
    Abstract: Disclosed herein is a disk assembly for a gas turbine compressor, which comprises a partition wall formed to partition a space between disks for a gas turbine compressor to optimize a cooling fluid path.
    Type: Application
    Filed: February 1, 2018
    Publication date: August 9, 2018
    Inventors: Kyu Sic Hwang, Ievdoshyn Andrii