The invention discloses a buffer device for stable landing of a fixed wing model airplane, comprising a runway on which a guide slide rail is arranged; the sliding plate is located above the runway and arranged on the guide sliding rail in a sliding mode, and the upper portion of the sliding plate is elastically connected with a buffer plate; the energy dissipation assemblies are fixed to the buffer plate, the two energy dissipation assemblies are arranged in the mode of being parallel to the landing moving direction of the model airplane at intervals, the energy dissipation assemblies are connected through blocking nets, and the blocking nets are elastic nets; the anti-bounce assembly is fixed to the side, facing the model airplane, of the energy dissipation assembly.

    本发明公开了一种固定翼航模平稳降落缓冲装置,包括跑道,其上设置有导向滑轨;滑板,其位于所述跑道的上方,且滑动设置在所述导向滑轨上,所述滑板的上方弹性连接有缓冲板;消能组件,其固定在所述缓冲板上,且平行航模降落移动方向间隔设置有两组,各所述消能组件之间通过拦网进行连接,所述拦网位弹性网;以及防弹跳组件,其固定在所述消能组件朝向航模的一侧。


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    Titel :

    Buffering device for stable landing of fixed-wing model airplane


    Weitere Titelangaben:

    一种固定翼航模平稳降落缓冲装置


    Beteiligte:
    LI ZHONGTAO (Autor:in) / LIAO YICHEN (Autor:in) / MAO XUMING (Autor:in) / HAN YUKE (Autor:in) / SONG TING (Autor:in) / HU ZHIWEI (Autor:in) / SU DEBAO (Autor:in) / NONG JIAJIE (Autor:in)

    Erscheinungsdatum :

    2023-01-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64U



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