Patents by Inventor Kevin Ron Fimbers

Kevin Ron Fimbers 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).

  • Composite airspeed indicator display for compound aircrafts
    Patent number: 10690554
    Abstract: An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.
    Type: Grant
    Filed: February 8, 2018
    Date of Patent: June 23, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: David L. Adams, Kevin Ron Fimbers
  • Composite airspeed indicator display for compound aircrafts
    Patent number: 10690555
    Abstract: A torque indicator for an aircraft having a main rotor system and a translational thrust system driven by at least one engine includes a first indicator operable to display an actual torque of an engine of the aircraft relative to an engine torque limit, a second indicator operable to display an actual torque of the translational thrust system of the aircraft relative to a translational thrust system torque limit, and a third indicator operable to display an actual torque of the main rotor system of the aircraft relative to a main rotor system torque limit.
    Type: Grant
    Filed: February 8, 2018
    Date of Patent: June 23, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: David L. Adams, Kevin Ron Fimbers
  • COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS
    Publication number: 20190113403
    Abstract: A torque indicator for an aircraft having a main rotor system and a translational thrust system driven by at least one engine includes a first indicator operable to display an actual torque of an engine of the aircraft relative to an engine torque limit, a second indicator operable to display an actual torque of the translational thrust system of the aircraft relative to a translational thrust system torque limit, and a third indicator operable to display an actual torque of the main rotor system of the aircraft relative to a main rotor system torque limit.
    Type: Application
    Filed: February 8, 2018
    Publication date: April 18, 2019
    Inventors: David L. Adams, Kevin Ron Fimbers
  • COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS
    Publication number: 20190112071
    Abstract: An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.
    Type: Application
    Filed: February 8, 2018
    Publication date: April 18, 2019
    Inventors: David L. Adams, Kevin Ron Fimbers
  • Flight display screen or portion thereof with graphical user interface including a composite indicator
    Patent number: D881206
    Type: Grant
    Filed: February 8, 2018
    Date of Patent: April 14, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: David L. Adams, Kevin Ron Fimbers
  • Flight display screen or portion thereof with graphical user interface including a composite indicator
    Patent number: D888069
    Type: Grant
    Filed: February 8, 2018
    Date of Patent: June 23, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: David L. Adams, Kevin Ron Fimbers