The invention provides a self-adaptive adapter and an aircraft launching structure. The self-adaptive adapter comprises an adaptive seat, an adapter sliding column structure, an elastic piece, an adaptive base and a limiting screw, the adapter base is fixedly connected with the top end of the adapter sliding column structure, and the bottom end of the adapter sliding column structure is slidably installed on the adapter base. The elastic piece is sleeved on a sliding column of the adapter sliding column structure, and the elastic piece is in a compressed state; the adaptive seat is mounted on an external transmitting device; the limiting screw comprises a head portion and a stud portion, the stud portion is connected with the adapter sliding column structure through a thread structure, and the head portion abuts against the adapter base. The sliding column, the elastic piece and the limiting screw are combined, the aircraft can be supported after the aircraft is installed in a launching device, and the adapter and the aircraft are in attached contact by controlling the screwing depth of the limiting screw to adjust the compression amount of the spring.
本发明提供了自适应适配器及飞行器发射结构。所述自适应适配器,包括适配座、适配器滑柱结构、弹性件、适配底座以及限位螺钉;所述适配座与适配器滑柱结构的顶端紧固连接,适配器滑柱结构的底端可滑动安装在所述适配底座上;所述弹性件套装在所述适配器滑柱结构所具有的滑柱上,弹性件处于压缩状态;所述适配座安装在外界发射装置上;所述限位螺钉包括头部与螺柱部,所述螺柱部通过螺纹结构与所述适配器滑柱结构连接,所述头部与所述适配座相抵。本发明将滑柱、弹性件以及限位螺钉相结合,可以在飞行器装入发射装置后为飞行器提供支撑,并通过控制限位螺钉的拧入深度调整弹簧的压缩量实现适配器与飞行器之间贴合接触。
Adaptive adapter and aircraft launching structure
自适应适配器及飞行器发射结构
2023-08-29
Patent
Elektronische Ressource
Chinesisch
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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