Patents by Inventor Carlos Gilberto Fernandez-Soto

Carlos Gilberto Fernandez-Soto 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: 11970979
    Abstract: A turbine engine and method of operating includes an engine core with a compressor, a combustor, and a turbine in axial flow arrangement. A flow path extends through the engine core from the compressor to the turbine to define a flow direction for a working airflow through the engine core.
    Type: Grant
    Filed: November 2, 2022
    Date of Patent: April 30, 2024
    Assignee: General Electric Company
    Inventors: Christopher Ryan Johnson, Paul Hadley Vitt, Eric Joseph Schroeder, Carlos Gilberto Fernandez-Soto
  • Publication number: 20230059927
    Abstract: A turbine engine and method of operating includes an engine core with a compressor, a combustor, and a turbine in axial flow arrangement. A flow path extends through the engine core from the compressor to the turbine to define a flow direction for a working airflow through the engine core.
    Type: Application
    Filed: November 2, 2022
    Publication date: February 23, 2023
    Inventors: Christopher Ryan Johnson, Paul Hadley Vitt, Eric Joseph Schroeder, Carlos Gilberto Fernandez-Soto
  • Patent number: 11519333
    Abstract: Aspects of the disclosure generally relate to a turbine engine and method of operating a turbine engine having an engine core including a compressor, combustor, and turbine in axial flow arrangement, whereby a working airflow passes through the engine core from the compressor to the turbine to define a flow direction through the engine core. The method includes generating a shockwave in the working airflow that propagates in the flow direction, and at least partially attenuating the shockwave.
    Type: Grant
    Filed: September 10, 2020
    Date of Patent: December 6, 2022
    Assignee: General Electric Company
    Inventors: Christopher Ryan Johnson, Paul Hadley Vitt, Eric Joseph Schroeder, Carlos Gilberto Fernandez-Soto
  • Publication number: 20220074348
    Abstract: Aspects of the disclosure generally relate to a turbine engine and method of operating a turbine engine having an engine core including a compressor, combustor, and turbine in axial flow arrangement, whereby a working airflow passes through the engine core from the compressor to the turbine to define a flow direction through the engine core. The method includes generating a shockwave in the working airflow that propagates in the flow direction, and at least partially attenuating the shockwave.
    Type: Application
    Filed: September 10, 2020
    Publication date: March 10, 2022
    Inventors: Christopher Ryan Johnson, Paul Hadley Vitt, Eric Joseph Schroeder, Carlos Gilberto Fernandez-Soto