Patents by Inventor Mikel Villaro Amurrio

Mikel Villaro Amurrio 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).

  • Turbine guide vane
    Patent number: 11719110
    Abstract: A guide vane for a vane assembly of a turbo machine, the guide vane can include: an aerofoil body including: a forward portion, a rear portion, and opposite outer surfaces, extending between the forward portion and the rear portion, a liner shaped with a sheet like geometry, the liner being configured for being fixed to the aerofoil body, the liner including: a first portion configured for being connected to the forward portion of the aerofoil body, a trailing edge portion shaped with a convex geometry, a first coupling portion extending between the first portion and the trailing edge portion, and configured for being fixed to an outer surface of the aerofoil body, a second portion extending from the trailing edge portion and configured for being connected to the rear portion of the aerofoil body, wherein when the first coupling portion of the liner is fixed to an outer surface of the aerofoil body: the trailing edge portion of the liner extends from the rear portion of the aerofoil body, and the second porti
    Type: Grant
    Filed: September 29, 2021
    Date of Patent: August 8, 2023
    Assignee: ITP NEXT GENERATION TURBINES, S.L.
    Inventor: Mikel Villaro Amurrio
  • TURBINE GUIDE VANE
    Publication number: 20220186625
    Abstract: A guide vane for a vane assembly of a turbo machine, the guide vane can include: an aerofoil body including: a forward portion, a rear portion, and opposite outer surfaces, extending between the forward portion and the rear portion, a liner shaped with a sheet like geometry, the liner being configured for being fixed to the aerofoil body, the liner including: a first portion configured for being connected to the forward portion of the aerofoil body, a trailing edge portion shaped with a convex geometry, a first coupling portion extending between the first portion and the trailing edge portion, and configured for being fixed to an outer surface of the aerofoil body, a second portion extending from the trailing edge portion and configured for being connected to the rear portion of the aerofoil body, wherein when the first coupling portion of the liner is fixed to an outer surface of the aerofoil body: the trailing edge portion of the liner extends from the rear portion of the aerofoil body, and the second porti
    Type: Application
    Filed: September 29, 2021
    Publication date: June 16, 2022
    Inventor: Mikel Villaro Amurrio