Patents by Inventor Metodi Blagoev Zlatinov

Metodi Blagoev Zlatinov 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).

  • Component for a gas turbine engine with a film hole
    Patent number: 11773729
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling; hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Grant
    Filed: August 24, 2022
    Date of Patent: October 3, 2023
    Assignee: General Electric Company
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson
  • COMPONENT FOR A GAS TURBINE ENGINE WITH A FILM HOLE
    Publication number: 20220412219
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling; hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Application
    Filed: August 24, 2022
    Publication date: December 29, 2022
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson
  • Component for a gas turbine engine with a film hole
    Patent number: 11466575
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Grant
    Filed: September 5, 2018
    Date of Patent: October 11, 2022
    Assignee: General Electric Company
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson
  • COMPONENT FOR A GAS TURBINE ENGINE WITH A FILM HOLE
    Publication number: 20190003314
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Application
    Filed: September 5, 2018
    Publication date: January 3, 2019
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson
  • Component for a gas turbine engine with a film hole
    Patent number: 10094226
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Grant
    Filed: November 11, 2015
    Date of Patent: October 9, 2018
    Assignee: General Electric Company
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson
  • COMPONENT FOR A GAS TURBINE ENGINE WITH A FILM HOLE
    Publication number: 20170130592
    Abstract: A component is provided and comprises at least one wall comprising a first and a second surface. At least one film cooling hole extends through the wall between the first and second surfaces and has an outlet region at the second surface. The film cooling hole includes a first expansion section being a side diffusion portion and a second expansion section being a layback diffusion portion, wherein the side diffusion portion is upstream and spaced from the layback diffusion portion.
    Type: Application
    Filed: November 11, 2015
    Publication date: May 11, 2017
    Inventors: Aaron Ezekiel Smith, Metodi Blagoev Zlatinov, Thomas Earl Dyson