The invention discloses an icing detection device for a helicopter. Comprising a supporting rod (6) capable of rotating, and a hovering probe body (5) extending outwards in the radial direction is arranged on the supporting rod (6); the supporting rod (6) is provided with a flying state icing detection assembly on the windward side, and a hovering state icing detection assembly is arranged on the outer wall face of the hovering probe body (5). The problem of icing detection of the large unmanned rotorcraft in the high-altitude area is effectively solved.

    本发明公开了一种用于直升机的结冰探测装置。包括能自转的支杆(6),支杆(6)上设有沿径向外伸的悬停探头主体(5);所述的支杆(6)在迎风面上设有飞行状态结冰探测组件,悬停探头主体(5)外壁面上设有悬停状态结冰探测组件。本发明有效解决高海拔区域大型旋翼无人机的结冰探测问题。


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    Titel :

    Icing detection device for helicopter


    Weitere Titelangaben:

    一种用于直升机的结冰探测装置


    Beteiligte:
    LIU CHANG (Autor:in) / GUO YUDONG (Autor:in) / ZHANG JIAN (Autor:in) / YANG QIKE (Autor:in) / RAO BO (Autor:in) / ZHU XIYUAN (Autor:in)

    Erscheinungsdatum :

    2024-02-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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