The invention relates to the technical field of aircrafts, in particular to an aircraft body quick release mechanism and an aircraft. The quick release mechanism for the aircraft body comprises a first aircraft body part, a second aircraft body part and a third aircraft body part, wherein a first front-end hook is arranged on the first aircraft body part; a second front-end hook is arranged on the second machine body part, and the second front-end hook and the first front-end hook are overlapped and aligned to form a front-end hook; a front-end hook groove is formed in the third machine body part, the front-end hook is movably installed in the front-end hook groove, and a locking device used for locking and unlocking the front-end hook in the front-end hook groove is installed in the front-end hook groove. The device has the beneficial effects that the first machine body part, the second machine body part and the third machine body part can be quickly disassembled and assembled, operation is easy and convenient, and the disassembling and assembling efficiency is high.

    本发明涉及飞行器技术领域,特别是涉及一种飞行器机体快拆机构及飞行器。该飞行器机体快拆机构包括第一机体部件、第二机体部件和第三机体部件,所述第一机体部件上设有第一前端挂钩;所述第二机体部件上设有第二前端挂钩,所述第二前端挂钩与所述第一前端挂钩重叠对齐形成前端挂钩;所述第三机体部件上设有前端挂钩槽,所述前端挂钩可移动地安装在所述前端挂钩槽内,所述前端挂钩槽内安装有用于所述前端挂钩在所述前端挂钩槽内锁定和解锁的锁紧装置。本发明的有益效果是:能够快速实现第一机体部件、第二机体部件和第三机体部件的拆装,操作简单方便,拆装效率高。


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    Titel :

    Aircraft body quick release mechanism and aircraft


    Weitere Titelangaben:

    飞行器机体快拆机构及飞行器


    Beteiligte:
    QU HUMIN (Autor:in) / WANG CHAO (Autor:in) / WANG KUN (Autor:in) / YU XIN (Autor:in) / CHEN QIURUN (Autor:in)

    Erscheinungsdatum :

    02.12.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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