An aircraft ice protection system (10) comprises an ice protection device (21), an onboard power source (30), a supply line (31) from the power source (30) to the device (21), a controller (41) which controls the line (31), and an optimizer (50) which conveys operation-optimizing instructions (51) to the controller (41). An ice detector (60) provides an input (70) to the optimizer (50) and this ice-condition input (70) is used to generate the operation-optimizing instructions (51).


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    Title :

    Aircraft ice protection system with operation optimization based on ice-detection input


    Additional title:

    Eisschutzsystem für Flugzeug mit optimierter Funktion basierend auf Eiserfassungseingabe
    Système de protection contre la glace pour aéronef avec optimisation d'operation sur la base d'une entrée de détection de glace



    Publication date :

    2016-08-03


    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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