The invention discloses a ship-borne fixed-wing unmanned aerial vehicle inflatable track rapid take-off and landing platform. The platform mainly comprises a fixed end structure, a flexible steel cable, an air bag and a supporting platform. The rapid take-off and landing platform is fixed to the tail of a ship through the fixed end structure. According to the rapid take-off and landing platform, the flexible steel cables connected with all the sub-airbags are used for bearing pull loads, the inflated airbags are used for providing normal supporting rigidity, the upper edge strip, the lower edge strip and the web of the engineering beam are simulated respectively, and the target of bearing the bending as the main load in the rapid take-off and landing platform is achieved. The supporting platform is fixed to the flexible steel cable through the pulleys and can slide along the flexible steel cable. When the unmanned aerial vehicle takes off, the rapid take-off and landing platform is rapidly unfolded, and then the supporting platform is driven by the driving damping device to drive the unmanned aerial vehicle to take off rapidly in a short distance; when the unmanned aerial vehicle lands, the arresting cable on the supporting platform captures the wheels of the unmanned aerial vehicle, and damping force is applied to the supporting platform to ensure that the speed of the unmanned aerial vehicle is reduced to zero within a short distance.

    本发明公开了一种舰载固定翼无人机充气轨道快速起降平台,主要包括固定端结构、柔性柔性钢索、气囊和支撑平台。固定端结构将快速起降平台固定在舰船尾部。快速起降平台利用与各子气囊相连的柔性钢索承受拉载荷,利用充气后的气囊提供法向支撑刚度,分别模拟工程梁的上、下缘条和腹板,实现承受快速起降平台中以弯曲为主要载荷的目标。支撑平台通过滑轮固定在柔性钢索上,可以沿柔性钢索滑动。当无人机起飞时,快速起降平台快速展开,随后支撑平台在驱动阻尼装置的驱动下带动无人机在短距离内快速起飞;当无人机着落时,支撑平台上的拦阻索捕获无人机机轮,通过对支撑平台施加阻尼力保证无人机速度在短距离内降为0。


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    Titel :

    Rapid taking-off and landing platform for inflatable track of ship-borne fixed-wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种舰载固定翼无人机充气轨道快速起降平台


    Beteiligte:
    DONG BO (Autor:in) / YU CHEN (Autor:in) / LYU SHENGLI (Autor:in)

    Erscheinungsdatum :

    2024-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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