A fault-tolerant active matrix display device for avionics systems includes a panel glass, a set of source signal lines, and a set of gate signal lines. Each of the gate signal lines includes a first gate line end and a second gate line end on opposite sides of the panel glass. A source driver circuit is coupled to at least a portion of the source signal lines. A first gate driver circuit includes a first set of gate driver cells. Each of the gate driver cells of the first gate line driver circuit includes a gate line output connected to one of the set of gate signal lines at the first gate line end thereof. A second gate driver circuit includes a second set of gate driver cells.


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    Titel :

    FAULT TOLERANT DISPLAY


    Beteiligte:
    OOGHE JÜRGEN (Autor:in)

    Erscheinungsdatum :

    2023-02-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G09G Anordnungen oder Schaltungen zur Steuerung oder Regelung von Anzeigevorrichtungen mit statischen Mitteln zur Darstellung veränderlicher Informationen , ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    Fault tolerant avionics

    HILLS, ANDY / MIRZA, NISAR | AIAA | 1988