The invention provides an airborne folding wing unmanned aerial vehicle launching adjusting device. The airborne folding wing unmanned aerial vehicle launching adjusting device comprises a launching cylinder, a booster, a thrust line adjusting tool, an unmanned aerial vehicle assembly, a plurality of snapping rods and a plurality of cutting-off assemblies. The launch canister has a launch port; the booster, the thrust line adjusting tool and the unmanned aerial vehicle assembly are sequentially arranged in the direction close to the launching opening, and the thrust line adjusting tool comprises a first thrust line adjusting piece and a second thrust line adjusting piece. According to the airborne folding wing unmanned aerial vehicle launching adjusting device, position adjustment of the unmanned aerial vehicle assembly and the booster can be achieved in the adjusting direction perpendicular to the launching direction through the thrust line adjusting tool, the problem that the thrust line cannot be adjusted is solved, the unmanned aerial vehicle assembly is smoothly launched from the launching cylinder, the overall structure is stable, and the overall structure is simple. The unmanned aerial vehicle assembly can be stably limited in the launching cylinder, the unmanned aerial vehicle assembly is prevented from falling off from the launching cylinder in the flying process of the flying mother aircraft, the booster and the aircraft body can be smoothly separated by cutting off the explosive bolt of the assembly, and the tail pushing piece is smoothly started.
本发明提供一种机载折叠翼无人机发射调整装置,包括:发射筒、助推器、推力线调整工装、无人机组件、若干拉断杆和若干切断组件;发射筒具有发射口;助推器、推力线调整工装和无人机组件在靠近发射口的方向依次布置,推力线调整工装包括第一推力线调整件和第二推力线调整件。本发明的机载折叠翼无人机发射调整装置能够通过推力线调整工装在垂直于发射方向的调节方向上实现对无人机组件和助推器的位置调节,弥补了推力线无法调节的问题,使得无人机组件顺利从发射筒射出,整体结构稳定,无人机组件能够被稳定限制在发射筒内,避免飞行母机在飞行途中无人机组件从发射筒脱落,切断组件的爆炸螺栓可使得助推器和机体顺利分离,使得尾推件顺利启动。
Launching adjusting device of airborne folding wing unmanned aerial vehicle
一种机载折叠翼无人机发射调整装置
2025-02-28
Patent
Electronic Resource
Chinese
IPC: | B64U |
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