The invention provides a multi-control-surface empennage locking and releasing mechanism, a control method and a cylindrical folding wing unmanned aerial vehicle. The mechanism comprises a base, a fuel gas generator, a locking and releasing assembly and a limiting assembly. The gas generator is mounted to the base. In the locking and releasing assembly, one end of a driving shaft is contained in a base and provided with a cavity, gas can lead to the cavity to push the driving shaft to move in the direction away from the control surfaces, a bracket moves along with the driving shaft, a pin penetrates through the base to be installed on the bracket and can be inserted into the control surfaces, and the length of the pin depends on the length of the control surfaces and the releasing time sequence. In the limiting assembly, the supporting piece is fixed to the base through a supporting rod, and the stopping piece limits movement of the driving shaft when moving along with the driving shaft to make contact with the supporting piece. According to the invention, the control surface expansion of the empennage is irrelevant to the cylinder wall smoothness, and the empennage can be expanded in a delayed manner; locking and releasing of a plurality of control surfaces are controlled by the same mechanism, and the releasing reliability is high; the pins with different lengths can be selected for synchronous or asynchronous release of multiple control surfaces according to different lengths of empennage control surfaces and release time sequence requirements.

    本发明提供了多舵面尾翼锁紧释放机构、控制方法及筒射折叠翼无人机。该机构包括基座、燃气发生器、锁紧释放组件和限位组件。燃气发生器安装至基座。锁紧释放组件中,驱动轴一端容置在基座中且设有空腔,燃气能通向腔推动驱动轴沿远离舵面方向移动,托架随驱动轴运动,销穿过基座安装在托架上且能插入舵面,销长度取决于各舵面的长度和释放时序。限位组件中,支撑件通过支杆固定至基座,止挡件随驱动轴移动至与支撑件接触时限制驱动轴运动。根据本发明,尾翼舵面展开与筒壁光洁度无关且尾翼可延时展开;多个舵面的锁紧及释放由同一机构控制,释放可靠性高;可针对不同长度的尾翼舵面和释放时序需求,选择不同长度的销进行多舵面的同步或异步释放。


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    Title :

    Multi-control-plane empennage locking and releasing mechanism, control method and cylindrical folding wing unmanned aerial vehicle


    Additional title:

    多舵面尾翼锁紧释放机构、控制方法及筒射折叠翼无人机


    Contributors:
    MASATOSHI (author) / LIU YUTING (author) / FAN XINGYU (author) / ZHOU MING (author) / WANG FANGLONG (author) / ZHAO JIANG (author) / LI YU (author) / BAI JUNQIANG (author) / WANG HUI (author) / ZHANG YANG (author)

    Publication date :

    2024-05-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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