The invention provides an inertia release device, and relates to the technical field of ejection, the inertia release device comprises a track and a sliding unit, the sliding unit comprises a supporting main body, a turnover frame and an elastic supporting mechanism, and the supporting main body is slidably arranged on the track and has an acceleration mode and a deceleration mode. One side of the overturning frame is connected with the supporting body, the other side of the overturning frame is provided with a connecting part, and the overturning frame rotates relative to the supporting body. The elastic supporting mechanism is arranged on the supporting body, in the acceleration mode, the overturning frame deflects backwards to enable the connecting part to be located at the upper position and connected with the ejection part, and the overturning frame is connected with the elastic supporting mechanism so as to drive the ejection part to slide forwards through the connecting part. And in the speed reduction mode, the connecting part is separated from the ejection piece, and the overturning frame deflects forwards, so that the connecting part is located in the front position. According to the inertia release device, it can be guaranteed that the inertia release device is continuously connected with the catapult part in the acceleration process of the catapult part so that stable boosting can be achieved, and the reliability of catapult-assisted take-off is improved.

    本申请提供一种惯性释放装置,涉及弹射技术领域,包括轨道和滑动单元,滑动单元包括支撑主体、翻转架和弹性支撑机构,支撑主体滑动设置在轨道上,其具有加速模式和减速模式。翻转架的一侧连接支撑主体,另一侧设有连接部,翻转架相对于支撑主体转动。弹性支撑机构设置在支撑主体上,在加速模式下,翻转架朝后偏转使连接部处于上方位且与弹射件连接,翻转架与弹性支撑机构连接,以通过连接部驱动弹射件朝前滑行。在减速模式下,连接部与弹射件脱离,翻转架朝前方偏转,使连接部处于前方位。本申请提供的惯性释放装置,能够保证在对弹射件加速的过程中与之持续连接以实现稳定助推,提高弹射起飞的可靠性。


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    Titel :

    Inertia release device


    Weitere Titelangaben:

    一种惯性释放装置


    Beteiligte:
    LIAO JINJUN (Autor:in) / YU ZHONGBO (Autor:in) / SUI XIANGYING (Autor:in) / JIANG HAIHUA (Autor:in) / ZHAO GUISHENG (Autor:in) / CAO QINGQUAN (Autor:in)

    Erscheinungsdatum :

    2024-03-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / 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



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