The invention relates to a cable hooking preventing structure for a low-altitude flying aircraft, and belongs to the structural design of aircrafts. The cable hooking preventing structure is that a steel cable is arranged between a cockpit and a fixed fin of an empennage and is fixed on a bracket through a steel sleeve ring I, wherein the bracket is fixed on the fixed fin; a lead cutter structure is additionally arranged on an aircraft body; the upper part of the lead cutter structure is fixed on the cockpit through an upper bracket of a lead cutter, and while the lower part of the lead cutter structure is fixed on the aircraft body through a lower bracket of the lead cutter; the steel cable is integrally connected with a steel sleeve ring II and then is fixed to the upper part of the lead cutter through an elastic screw barrel. The cable hooking preventing structure is suitable for the low-altitude flying aircraft and has the advantages of being simple in structure, high in safety and low in cost; meanwhile, the empennage can be effectively prevented from being influenced by the cable, so that the safety and reliability of the aircraft flying at a low altitude are improved.


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    Titel :

    Cable hooking preventing structure for low-altitude flying aircraft


    Beteiligte:
    DENG CHENGYANG (Autor:in) / JI XIANWU (Autor:in) / LIANG HAO (Autor:in) / XU HUANYU (Autor:in) / LI XIAOBAO (Autor:in) / ZHANG GAIHUA (Autor:in) / LU WEIFU (Autor:in) / WU GENLIN (Autor:in) / FU JIEBIN (Autor:in) / CHEN LIGEN (Autor:in)

    Erscheinungsdatum :

    01.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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