The invention discloses a self-unlocking releasing mechanism for an aircraft. The self-unlocking releasing mechanism for the aircraft comprises a tension sensor installed on a base body, a fixing block is installed on the side, away from the base body, of the tension sensor, a connecting plate is arranged on the side, away from the tension sensor, of the fixing block, a hinge plate is arranged on one side of the connecting plate, and the hinge plate is connected with the tension sensor. The fixing plate and the hinged plate are each provided with a guide rail assembly, the two guide rail assemblies are perpendicularly arranged, the hinged plate can be adjusted on the X axis and the Z axis under the action of the two guide rail assemblies, the fixing plate is connected with the connecting plate through one guide rail assembly, and the connecting plate is connected with the hinged plate through the other guide rail assembly. The self-unlocking releasing mechanism for the aircraft can still take off without depending on a runway, all the components are mostly made of common materials, and the cost is lower.

    本发明公开了一种用于飞行器的自解锁放飞机构。用于飞行器的自解锁放飞机构,包括:安装在基体上的拉力传感器,所述拉力传感器远离基体的一侧安装有固定块,所述固定块远离所述拉力传感器的一侧设置连接板,所述连接板的一侧设置有铰接板,所述固定板和所述铰接板上均设置有导轨组件,两个所述导轨组件呈垂直设置,两个导轨组件的作用下,铰接板能够在X轴和Z轴上实现调节,所述固定板通过其中一个导轨组件与连接板连接,所述连接板通过另一个导轨组件与铰接板连接。本发明提供的用于飞行器的自解锁放飞机构能够不依赖跑道仍然能够起飞,且各个部件多为普通材料,成本更低。


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    Titel :

    Self-unlocking releasing mechanism for aircraft


    Weitere Titelangaben:

    一种用于飞行器的自解锁放飞机构


    Beteiligte:
    HAN WEIQI (Autor:in) / LYU GUIDONG (Autor:in) / WANG RUOYI (Autor:in) / LIU ZEZHONG (Autor:in)

    Erscheinungsdatum :

    2023-03-31


    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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