A method includes receiving pump cycle location data (144) associated with a fluid power system (102) of an aircraft. The fluid power system (102) includes a plurality of pumps (104), including at least a first pump (106), a second pump (108), and a third pump (110). Based on the pump cycle location data (144) having a first value, the method includes activating the first pump (106) as a primary pump. Based on the pump cycle location data (144) having a second value, the method includes activating the second pump (108) as the primary pump. The method also includes activating the third pump (110) as a secondary pump when the fluid power system (102) is in a multiple-pump operating mode.


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    Title :

    DYNAMIC ACTIVATION OF PUMPS OF A FLUID POWER SYSTEM


    Additional title:

    DYNAMISCHE AKTIVIERUNG VON PUMPEN EINER FLUIDTECHNISCHEN ANLAGE
    ACTIVATION DYNAMIQUE DE POMPES D'UN SYSTÈME D'ALIMENTATION DE FLUIDE


    Contributors:

    Publication date :

    2021-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F04B Verdrängerkraft- und Verdrängerarbeitsmaschinen für Flüssigkeiten , POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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