Patents by Inventor George W. Wilson

George W. Wilson 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: 11971056
    Abstract: A head unit device for controlling motion of an object includes a chamber filled with a shear thickening fluid (STF) and a piston. The piston is housed within the chamber and exerts pressure against the STF from a force applied to the piston from the object. The STF is configured to have a decreasing viscosity in response to a first range of shear rates and an increasing viscosity in response to a second range of shear rates. The piston includes at least one piston bypass between opposite sides of the piston that controls flow of the STF between the opposite sides of the piston to selectively react with a shear threshold effect of the first range of shear rates or the second range of shear rates.
    Type: Grant
    Filed: October 29, 2021
    Date of Patent: April 30, 2024
    Assignee: Moshun, LLC
    Inventors: Timothy John Boundy, Steven Michael Barger, Terence Michael Lydon, Richard Michael Lang, Wilfredo Gonzalez, Jr., Darren Michael Boundy, Eric McHugh, David Schuda, George L Wilson, IV, Gary W. Grube, Jason K. Resch, Mario F. DeRango, John Edward Buchalo, Richard A. Herbst, Kurt Estes, Evan Anderson
  • Patent number: 4422468
    Abstract: A lawn umbrella expansion device in which an enlarged canopy is provided with a centrally disposed pole cap to engage the tip of an umbrella pole and thereafter be unfurled and stabilized with canopy poles to provide a greatly increased containment area.
    Type: Grant
    Filed: February 24, 1982
    Date of Patent: December 27, 1983
    Inventor: George W. Wilson
  • Patent number: 4242917
    Abstract: An illustrative embodiment of the invention provides an isolation flexure assembly for the control moment gyroscope of a spacecraft attitude control system for attenuation of vibratory disturbances therein, due to rotor static and dynamic unbalance and spin bearing radial forces. The isolation flexure assembly isolates the rotor, the main generator of the vibratory disturbances, from the spacecraft permitting ultraprecise pointing or precision torquing of the spacecraft.
    Type: Grant
    Filed: July 3, 1978
    Date of Patent: January 6, 1981
    Assignee: Sperry Corporation
    Inventors: Virgil O. Bennett, George W. Wilson