An emergency braking method for an aircraft, comprising using a progressing parking brake controlled by a lever (10) that can be actuated by the pilot between a "0%" position in which the brakes are connected to the return pressure of the aircraft, and a "100%" position in which the brakes are connected to the feed pressure of the aircraft, the lever being blockable in the 100% position in order to provide parking braking when the aircraft is stationary. According to the invention, the emergency braking method is characterized in that it comprises: using a valve having an outlet port connectedto the brakes, a return port, and a feed port, the valve presenting a state connecting the outlet port to the return port and a state connecting the outlet port to the feed port; and controlling thevalve to occupy one or other of those states by pulse width modulation (PWM) having a duty ratio (R) that is a function of the position of the lever in order to deliver the brakes with pressure lyingin the range return pressure to feed pressure, depending on the position of the lever.


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    Titel :

    PROCEDE DE FREINAGE SECOURS D'UN AERONEF


    Weitere Titelangaben:

    AN EMERGENCY BRAKING METHOD FOR AN AIRCRAFT
    VERFAHREN ZUR NOTBREMSUNG FÜR EIN FLUGZEUG


    Beteiligte:
    FRANK DAVID (Autor:in) / FRAVAL JÉRÔME (Autor:in) / WARINT DONNY (Autor:in)

    Erscheinungsdatum :

    2021-01-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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