Patents by Inventor Brady Powell Dearing

Brady Powell Dearing 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).

  • HYDRAULIC POWER PACK WITH ADJUSTABLE MOUNTING ARRANGEMENT
    Publication number: 20240141892
    Abstract: The present disclosure relates to a hydraulic power pack arrangement that can be configured in multiple different mounting configurations. The hydraulic power pack arrangement can include a bracket assembly for mounting a hydraulic power pack core assembly and a hydraulic reservoir assembly at a mounting location such as a floor, wall, or ceiling of an aircraft.
    Type: Application
    Filed: October 17, 2023
    Publication date: May 2, 2024
    Inventors: Joshua Boone Pepper, David E. Korba, Brady Powell Dearing, Eugene Mikhailovich Grigoriev, Kelly Dale Valtr, Stephen Marshall Devan
  • Hydraulic power pack with adjustable mounting arrangement
    Patent number: 11821419
    Abstract: The present disclosure relates to a hydraulic power pack arrangement that can be configured in multiple different mounting configurations. The hydraulic power pack arrangement can include a bracket assembly for mounting a hydraulic power pack core assembly and a hydraulic reservoir assembly at a mounting location such as a floor, wall, or ceiling of an aircraft.
    Type: Grant
    Filed: May 5, 2022
    Date of Patent: November 21, 2023
    Assignee: Eaton Intelligent Power Limited
    Inventors: Joshua Boone Pepper, David E. Korba, Brady Powell Dearing, Eugene Mikhailovich Grigoriev, Kelly Dale Valtr, Stephen Marshall Devan
  • HYDRAULIC POWER PACK WITH ADJUSTABLE MOUNTING ARRANGEMENT
    Publication number: 20220356875
    Abstract: The present disclosure relates to a hydraulic power pack arrangement that can be configured in multiple different mounting configurations. The hydraulic power pack arrangement can include a bracket assembly for mounting a hydraulic power pack core assembly and a hydraulic reservoir assembly at a mounting location such as a floor, wall, or ceiling of an aircraft.
    Type: Application
    Filed: May 5, 2022
    Publication date: November 10, 2022
    Inventors: Joshua Boone Pepper, David E. Korba, Brady Powell Dearing, Eugene Mikhailovich Grigoriev, Kelly Dale Valtr, Stephen Marshall Devan
  • REDUNDANT HYDRAULIC POWER PACK ARCHITECTURE FOR AIRCRAFT MAIN LANDING GEAR SYSTEM
    Publication number: 20220169367
    Abstract: The left and right main landing gears on an aircraft are normally controlled by separate hydraulic power packs (HPP). Each HPP is sized for the load of the respective main landing gear. During failure of one of the HPP, a backup valve actuates to allow the other HPP to operate both main landing gears. With the backup valve actuated, the pump of the functioning HPP is coupled to the reservoirs of both HPPs and to the load paths to both main landing gears.
    Type: Application
    Filed: November 30, 2021
    Publication date: June 2, 2022
    Inventors: Joshua Boone Pepper, Brady Powell Dearing