A system and method for selectively suspending the operation of aircraft systems based on prioritized system criticality in response to a high power demand from an aircraft engine. The method includes determining that a power demand on the aircraft engine will exceed a predetermined power limit, transmitting a suspend command to one or more of the aircraft systems in response to determining that the power demand on the aircraft engine will exceed the predetermined power limit, and causing the aircraft systems that receive the suspend command to enter a reduced power mode and not operate. The method also includes determining that the power demand on the one or more aircraft engines has been reduced below the predetermined power limit, and removing the suspend command and allow the aircraft systems that received the suspend command to operate as they were before receiving the suspend command.


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    Title :

    ADAPTIVE AIRCRAFT POWER MANAGEMENT SYSTEM


    Contributors:

    Publication date :

    2024-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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