Patents by Inventor Daniel Osgood

Daniel Osgood 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 ENGINE WITH A NOZZLE HAVING COOLING FEATURES
    Publication number: 20260098478
    Abstract: A turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. A turbine nozzle is arranged in the turbine section. Vanes of the turbine nozzle include a vane airfoil having cooling features formed in a trailing edge of the vane airfoil. Vanes of the turbine nozzle further include a baffle insert in a cavity of the vane airfoil. The baffle insert includes cooling holes.
    Type: Application
    Filed: November 27, 2024
    Publication date: April 9, 2026
    Inventors: Nancy Haviland Morton, Harjit S. Hura, Alison E. Schulte, Michael David Gervasio, Daniel Osgood, Marie Myers, Brett A. Rich
  • Turbine engine with a nozzle having cooling features
    Patent number: 12467366
    Abstract: A turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. A turbine nozzle is arranged in the turbine section. Vanes of the turbine nozzle include a vane airfoil having cooling features formed in a trailing edge of the vane airfoil. Vanes of the turbine nozzle further include a baffle insert in a cavity of the vane airfoil. The baffle insert includes cooling holes.
    Type: Grant
    Filed: November 27, 2024
    Date of Patent: November 11, 2025
    Assignee: General Electric Company
    Inventors: Nancy Haviland Morton, Harjit S. Hura, Alison E. Schulte, Michael David Gervasio, Daniel Osgood, Marie Myers, Brett A. Rich
  • TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES
    Publication number: 20250179922
    Abstract: A turbine engine includes an engine core extending along an engine centerline and includes a compressor section, a combustor, and a turbine section in serial flow arrangement. A turbine nozzle is arranged in the turbine section. Vanes of the turbine nozzle include a vane airfoil having cooling features formed in a trailing edge of the vane airfoil. Vanes of the turbine nozzle further include a baffle insert in a cavity of the vane airfoil. The baffle insert includes cooling holes.
    Type: Application
    Filed: November 27, 2024
    Publication date: June 5, 2025
    Inventors: Nancy Haviland Morton, Harjit S. Hura, Alison E. Schulte, Michael David Gervasio, Daniel Osgood, Marie Myers, Brett A. Rich
  • SYSTEMS AND METHODS FOR SELECTING COMPONENTS FOR AN ENGINE
    Publication number: 20210158287
    Abstract: A system for selecting components for an engine includes an electronic control unit comprising a processor and a memory component and a machine-readable instruction set. The machine-readable instruction set is stored in the memory component of the electronic control unit and causes the system to perform at least the following when executed by the processor: receive a catalog of a plurality of components, where the plurality of components include a measured manufacturing characteristic, receive at least one operating environment characteristic of a plurality of operating environment characteristics, and select one or more components from the catalog of the plurality of components for a bill of materials based on the measured manufacturing characteristic and the at least one operating environment characteristic.
    Type: Application
    Filed: November 22, 2019
    Publication date: May 27, 2021
    Applicant: General Electric Company
    Inventors: Brendan Michael Freely, Daniel Osgood, Paul Maletta, Kevin Samuel Klasing, Eric John Ruggiero