The invention relates to the technical field of missile release mechanisms, and concretely relates to a missile hoop release mechanism and an unmanned aerial vehicle. The missile hoop release mechanism comprises a base, a hoop assembly, a driving part, a limiting assembly and a driving assembly; the hoop assembly has a clasping state and a release state, and when the hoop assembly is in the clasping state and the two ends of the driving part abut against a left hoop and a right hoop correspondingly, the driving part is used for limiting rotation of the left hoop and the right hoop so as to clasp a missile; and when the hoop assembly is in the release state and the driving piece is separated from the left hoop and the right hoop, the guided missile is released. Firstly, the limiting assembly is in a failure state, then the driving assembly drives the driving piece to rotate, so that the driving piece relieves limitation on the hoop assembly, at the moment, the hoop assembly rotates under the action of the gravity of the guided missile, the hoop assembly is in a release state, and then the guided missile is released. The release mechanism completes missile release through a simple mechanical structure and has the advantages of being high in reliability, low in maintenance cost, convenient and easy to use and the like.
本发明涉及导弹释放机构技术领域,特别是涉及一种导弹抱箍释放机构及无人机,包括:底座、抱箍组件、驱动件、限位组件以及驱动组件;抱箍组件具有抱紧状态与释放状态:当抱箍组件处于抱紧状态时,驱动件的两端分别与左抱箍、右抱箍相抵靠时,用于限制左抱箍、右抱箍的转动以抱紧导弹;当抱箍组件处于释放状态时,驱动件与左抱箍、右抱箍相分离时,以用于释放导弹。首先使限位组件处于失效状态,然后通过驱动组件驱动驱动件转动,从而使驱动件解除对抱箍组件的限制,此时抱箍组件受到导弹重力的作用转动,使抱箍组件处于释放状态,进而释放导弹。该装置通过简单的机械结构完成导弹的释放,具有可靠性高,维护成本低,使用方便简单等优点。
Missile hoop release mechanism and unmanned aerial vehicle
一种导弹抱箍释放机构及无人机
2021-09-17
Patent
Elektronische Ressource
Chinesisch
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