Patents by Inventor Guy Mitaux-Maurouard

Guy Mitaux-Maurouard 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: 6112141
    Abstract: An aircraft display and control system includes a computer, a trackball and selection device, an aeronautical information database, a geographic database, and a plurality of flat panel display devices. The aircraft crew can perform flightplan entry and modification by manipulating graphical information on the display devices using cursor control.
    Type: Grant
    Filed: October 15, 1997
    Date of Patent: August 29, 2000
    Assignee: Dassault Aviation
    Inventors: Michel Briffe, Guy Mitaux-Maurouard
  • Patent number: 6057786
    Abstract: An aircraft display and control system includes a primary flight director and a head-up display. A flight management system computer generates a current aircraft velocity vector reticle, a desired aircraft velocity reticle, a speed reticle, an acceleration reticle, and a pitch reticle. The flight management system computer conformably generates a waypoint icon in the pilot's view through the windshield superimposed upon the position in the view of the geographic location and altitude of the actual waypoint.
    Type: Grant
    Filed: October 15, 1997
    Date of Patent: May 2, 2000
    Assignee: Dassault Aviation
    Inventors: Michel Briffe, Guy Mitaux-Maurouard
  • Patent number: 6038498
    Abstract: An aircraft includes a system for managing check lists solely by operation of a four-position rocker switch having a center return position. The system includes check list data organized into three levels and automatically displayed upon occurrence of an abnormal condition.
    Type: Grant
    Filed: October 15, 1997
    Date of Patent: March 14, 2000
    Assignee: Dassault Aviation
    Inventors: Michel Briffe, Guy Mitaux-Maurouard
  • Patent number: 5978715
    Abstract: An aircraft flight deck includes a primary flight display device and a combined autopilot/autothrottle controller. The controller is mounted on the flight panel below the windshield in a vertical line with the primary flight display. A thumb-activated multiaxis control switch is mounted on the control yoke and operates exclusively to adjust a preselected trajectory commanded to the autopilot when moved leftfright or fore/aft. Depressing the switch in a vertical axis in a position generates an ENABLE signal to activate the commanded preselected trajectory.
    Type: Grant
    Filed: October 15, 1997
    Date of Patent: November 2, 1999
    Assignee: Dassault Aviation
    Inventors: Michel Briffe, Guy Mitaux-Maurouard