Patents by Inventor Victor Odinokov

Victor Odinokov 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).

  • Stator vane for a gas turbine engine
    Patent number: 8152454
    Abstract: A guide vane for a gas turbine includes a vane body having a leading edge and a trailing edge and a shroud extending at least between the leading edge and the trailing edge. The shroud has a first side wall and a second side wall extending essentially radially and in a longitudinal direction of the gas turbine. The first side wall has a groove disposed in a region of the trailing edge extending in a longitudinal direction of the shroud and is configured to receive a sealing plate. The first side wall also has a clearance extending from the groove in a region of the trailing edge, wherein a depth of the clearance in a circumferential direction of the gas turbine is equal to a depth of the groove, and wherein a width of the clearance in the longitudinal direction of the shroud is between one to three times the depth of the clearance.
    Type: Grant
    Filed: December 23, 2009
    Date of Patent: April 10, 2012
    Assignee: Alstom Technology Ltd
    Inventors: Alexander Khanin, Igor Kurganov, Sergey Vorontsov, Victor Odinokov
  • STATOR VANE FOR A GAS TURBINE ENGINE
    Publication number: 20100150710
    Abstract: A guide vane for a gas turbine includes a vane body having a leading edge and a trailing edge and a shroud extending at least between the leading edge and the trailing edge. The shroud has a first side wall and a second side wall extending essentially radially and in a longitudinal direction of the gas turbine. The first side wall has a groove disposed in a region of the trailing edge extending in a longitudinal direction of the shroud and is configured to receive a sealing plate. The first side wall also has a clearance extending from the groove in a region of the trailing edge, wherein a depth of the clearance in a circumferential direction of the gas turbine is equal to a depth of the groove, and wherein a width of the clearance in the longitudinal direction of the shroud is between one to three times the depth of the clearance.
    Type: Application
    Filed: December 23, 2009
    Publication date: June 17, 2010
    Applicant: ALSTOM Technology Ltd
    Inventors: Alexander Khanin, Igor Kurganov, Sergey Vorontsov, Victor Odinokov