The invention discloses a solar energy and air energy composite aircraft. When the solar energy and air energy composite aircraft turns and slows down, a joint bearing drives an action shaft to swingcircumferentially; a horizontal thrust is applied to a second piston; a damping spring is driven to absorb pressure brought by the second piston; meanwhile, the second piston transmits pressure to a first air cylinder; the first air cylinder is driven to extrude internal air towards a direction of a first piston to slow down an impact; the first air cylinder located on the opposite side of an aircraft body sucks the air through a damping control valve; and a separation speed of the first air cylinder and the first piston is reduced, and then rebound vibration of the damping spring after absorbing pressure is inhibited so that when the aircraft steers and decelerates, the impact of the inertia of a load on the aircraft body can be reduced, and the aircraft can stably fly.

    本发明公开了一种太阳能与空气能复合飞行器,当所述太阳能与空气能复合飞行器转弯减速时,由所述关节轴承带动作轴向圆周摆动,对所述第二活塞施加水平推力,驱使所述减震弹簧吸收所述第二活塞带来的压力,同时所述第二活塞对所述第一气缸传递压力,驱使所述第一气缸朝向所述第一活塞的方向挤压内部的气体对冲击进行减缓,位于所述机体相对一侧的所述第一气缸通过所述阻尼控制阀吸入气体,减缓所述第一气缸与所述第一活塞的分离速度,进而抑制所述减震弹簧吸收压力后反弹的振动,如此能在飞行器进行转向减速时,减小载重物的惯性对所述机体带来的冲击,进而使飞行器保持平稳飞行。


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    Titel :

    Solar energy and air energy composite aircraft


    Weitere Titelangaben:

    一种太阳能与空气能复合飞行器


    Beteiligte:
    ZHOU QIFENG (Autor:in)

    Erscheinungsdatum :

    2020-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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