The invention belongs to the technical field of aircraft launching, and particularly relates to an aircraft rotary launching device and system which comprises a supporting body, at least one rotating body rotating around the axis of the supporting body and a driving device providing power for rotation of the rotating body. At least one attitude adjusting device is arranged on the rotating body, and the attitude adjusting device is used for adjusting the attitude of the aircraft in the rotating acceleration process and the launching process in real time; the attitude adjusting device is provided with a launcher used for holding and releasing an aircraft. And a base for stably supporting the whole launching device is arranged at the bottom of the supporting body. The attitude of the aircraft is controlled and adjusted in a targeted mode through the attitude adjusting device, the aircraft, especially a fixed-wing aircraft, can have the same linear speed of left and right wings relative to air at the launching moment, and therefore potential take-off safety caused by the lift force difference of the left and right wings is avoided.

    本发明属于飞行器发射技术领域,具体涉及一种飞行器旋转发射装置及系统,其包括支撑体,以及至少一个绕支撑体的轴心旋转的旋转体,以及为旋转体旋转提供动力的驱动装置;旋转体上设有至少一个姿态调节装置,所述的姿态调节装置用于实时调节飞行器在旋转加速中及发射时的姿态;姿态调节装置上设有用于保持和释放飞行器的发射架;支撑体的底部设有用于对发射装置整体提供稳定支撑的基座。本发明通过姿态调节装置针对性地控制调节飞行器的姿态,可以使飞行器,尤其是固定翼飞机在发射时刻左右机翼的相对于空气线速度相同,从而避免了左右机翼升力差带来的潜在起飞安全。


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    Titel :

    Aircraft rotary launching device and system


    Weitere Titelangaben:

    一种飞行器旋转发射装置及系统


    Beteiligte:
    JIANG JUN (Autor:in) / WANG XUEZHU (Autor:in)

    Erscheinungsdatum :

    2024-03-12


    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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