The invention provides a fixed wing aircraft electric heating ice prevention/control method comprising the following steps: dividing each slat in the leading edge into a plurality of heating zones along a spanwise direction; arranging a plurality of heating elements from the outer side to the inner side of the slat in each heating zone; controlling the plurality of heating zones to heat in cycle in sequence; controlling the heating elements in the heating zones to work in a work sequence so as to realize heating in a staggering manner, thus uniformly heating each heating zone. The control method can prevent and control ice formation, can effectively reduce system power consumption, thus improving aircraft fuel economic property.


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    Titel :

    Fixed wing aircraft electric heating ice prevention/control method


    Beteiligte:
    HUA RUIRUI (Autor:in) / LI ZHIMAO (Autor:in) / LI GEPING (Autor:in) / HUO XIHENG (Autor:in) / ZENG FEIXIONG (Autor:in) / WANG XIANGZHUAN (Autor:in) / YANG SHENGHUA (Autor:in) / XU JIAJIA (Autor:in)

    Erscheinungsdatum :

    2016-02-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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