The invention provides an aircraft cluster self-sliding ejection device suitable for complex terrains, which comprises an erecting frame which is in sliding connection with a sliding frame; a cylinder group is arranged on the sliding frames, at least one cylinder is arranged in the cylinder group, supporting lugs are uniformly and fixedly arranged on the periphery of the cylinder in the radial direction, the cylinder is arranged on the end faces of hoops through the supporting lugs, the front sliding frame and the rear sliding frame are each provided with a plurality of hoops, the hoops of the front sliding frame are fixedly connected to form a first layer of hoops, and the hoops of the rear sliding frame are fixedly connected to form a second layer of hoops; a plurality of hoops of the rear sliding frame are fixedly connected to form a second-layer hoop, a locking mechanism is arranged in the middle of the first-layer hoop and the middle of the second-layer hoop, a stepping motor is connected to the bottom of the locking mechanism, and the stepping motor drives the locking mechanism to rotate and locks the barrel on the sliding frame; the sliding rail is arranged on the outer side of the cylinder in the axial direction, the cylinder is arranged in the hoop through the sliding rail, the cylinder slides in the axial direction relative to the hoop and makes full contact with the ground, and the stability of the ejection device in the aircraft ejection process is guaranteed.

    本发明提供了一种适用于复杂地形的飞行器集束自滑移弹射装置,包括:起竖架,起竖架、滑移架滑动连接;滑移架,滑移架上设置有筒体组,筒体组内至少设置有一个筒体,筒体四周沿径向均匀固定设置有支耳,筒体通过支耳设置于抱箍端面上,前滑移架、后滑移架分别设置有若干个抱箍,前滑移架若干个抱箍固接为第一层抱箍,后滑移架若干个抱箍固接为第二层抱箍,第一层抱箍、第二层抱箍中间位置设置有锁止机构,锁止机构底部连接有步进电机,步进电机驱动锁止机构转动并将筒体锁止在滑移架上;筒体外侧沿轴向设置有滑轨,筒体通过滑轨设置于抱箍内,实现筒体相对抱箍沿轴向滑动,并实现筒体与地面充分接触,保证了飞行器弹射过程中弹射装置的稳定性。


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    Titel :

    Aircraft cluster self-sliding ejection device suitable for complex terrains


    Weitere Titelangaben:

    一种适用于复杂地形的飞行器集束自滑移弹射装置


    Beteiligte:
    YAO SHUJIAN (Autor:in) / SUN CHENGMING (Autor:in) / LU ZHAIJUN (Autor:in) / ZHONG MU (Autor:in) / FAN DENGKE (Autor:in) / HOU ERYONG (Autor:in) / LIU KAI (Autor:in)

    Erscheinungsdatum :

    25.06.2024


    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



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