An unmanned aerial vehicle (100200), including the fuselage (10, 10 '), the arm (20), and the power components (30, 30'). The arm (20) is connected to the fuselage (10, 10 \) and supports the power components (30, 30\). The arm (20) includes at least the first arm (21, 21 '), and the first arm (21, 21') has the first state relative to the body (10, 10 ') and the second state relative to the body (10, 10'). When the first arm (21, 21) in the first state, the first arm (21, 21 ') the first arm connected to the body of the mounting portion (15, 15'), when the first arm (21, 21) in the second state, the the first arm (21, 21 ') of the power components should be close to the first arm mounting portion (15, 15').
【技术实现步骤摘要】
【国外来华专利技术】PCT国内申请,说明书已公开。
【技术保护点】
PCT国内申请,权利要求书已公开。
【技术特征摘要】
【国外来华专利技术】2016.02....
【专利技术属性】
技术研发人员:邓雨眠,熊荣明,赵涛,唐尹,
申请(专利权)人:深圳市大疆创新科技有限公司,
类型:发明
国别省市:广东,44
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