Patents by Inventor Dave G. Parsons

Dave G. Parsons 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: 8359542
    Abstract: An interactive aircraft performance substantiation is provided by determining maneuvers for a user-selected aircraft, determining operation and performance variables for a user-selected maneuver, displaying a scale graphic representation of the user-selected aircraft according to aircraft dimensions, displaying load selection fields according to aircraft dimensions and load-sites dimensions, interactively updating the scale graphic representation of the user-selected aircraft to include an oriented graphic representation of a user-selected load according to the aircraft dimensions, load dimensions, and load-site dimensions, interactively determining mass properties of the user-selected aircraft according to the aircraft dimensions, the load dimensions, and the load-site dimensions; receiving operation properties for the user-selected maneuver corresponding to the operation variables; and displaying an aircraft performance substantiation responsive to determining performance properties of the user-selected air
    Type: Grant
    Filed: August 13, 2010
    Date of Patent: January 22, 2013
    Assignee: Lockheed Martin Corporation
    Inventors: David M. Dingeman, Dave G. Parsons
  • Publication number: 20120042273
    Abstract: An interactive aircraft performance substantiation is provided by determining maneuvers for a user-selected aircraft, determining operation and performance variables for a user-selected maneuver, displaying a scale graphic representation of the user-selected aircraft according to aircraft dimensions, displaying load selection fields according to aircraft dimensions and load-sites dimensions, interactively updating the scale graphic representation of the user-selected aircraft to include an oriented graphic representation of a user-selected load according to the aircraft dimensions, load dimensions, and load-site dimensions, interactively determining mass properties of the user-selected aircraft according to the aircraft dimensions, the load dimensions, and the load-site dimensions; receiving operation properties for the user-selected maneuver corresponding to the operation variables; and displaying an aircraft performance substantiation responsive to determining performance properties of the user-selected air
    Type: Application
    Filed: August 13, 2010
    Publication date: February 16, 2012
    Inventors: David M. Dingeman, Dave G. Parsons