The invention discloses a multi-rotor unmanned aerial vehicle capable of being folded and catapulted, and relates to the technical field of unmanned aerial vehicles, the multi-rotor unmanned aerial vehicle comprises a rack, a plurality of rotor assemblies, an unfolding assembly, a locking assembly, a catapulting assembly and a central control assembly; each rotor assembly can move relative to the rack so as to be stored in the rack or unfolded out of the rack; the unfolding assemblies can drive the corresponding rotor assemblies to unfold; when the rotor wing assembly is stored in the rack, the locking assembly can lock the position of the rotor wing assembly, and the locking assembly can release the position of the rotor wing assembly, so that the rotor wing assembly can be unfolded under the action of the unfolding assembly; the ejection assembly can eject the rack; the center control assembly is in communication connection with the rotor wing assembly, the locking assembly and the ejection assembly and can control actions of the rotor wing assembly, the locking assembly and the ejection assembly. According to the multi-rotor unmanned aerial vehicle capable of being catapulted in the folding mode, the catapult-assisted take-off efficiency of the unmanned aerial vehicle is The invention further provides a take-off method.
本发明公开了一种可折叠弹射的多旋翼无人机,涉及无人机技术领域,包括机架、多个旋翼组件、展开组件、锁定组件、弹射组件及中控组件;各旋翼组件均能够相对于机架活动以收纳于机架内或展开至机架外;展开组件能够驱动对应旋翼组件展开;旋翼组件收纳于机架内时,锁定组件能够对旋翼组件的位置进行锁定,且锁定组件能够解除对旋翼组件的位置,以使旋翼组件能够在展开组件的作用下展开;弹射组件能够对机架进行弹射;中控组件与旋翼组件、锁定组件和弹射组件均通信连接,并能够控制旋翼组件、锁定组件和弹射组件的动作。本发明提供的可折叠弹射的多旋翼无人机,提升无人机弹射起飞效率。本发明还提供一种起飞方法。
Multi-rotor unmanned aerial vehicle capable of being folded and catapulted and take-off method thereof
可折叠弹射的多旋翼无人机及其起飞方法
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64U |
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