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Arm linkage foldable device for UAV and UAV having the same

机译:无人机的臂连杆折叠装置及具有该装置的无人机

摘要

An arm linkage foldable device for a UAV (unmanned aerial vehicle) includes a linkage module and two connection modules. The linkage module includes a guided structure and a slider. The slider slides along the guided structure. Two aircraft arms located at two sides of the fuselage are respectively connected with two sides of a slider through the two connection modules, a joint of every connection module and the slider is rotatable. A protruding portion is located on every connection module, a slide groove is provided on the fuselage corresponding to the protruding portion, the protruding portion is inserted into the slide groove and slides along the slide groove. The slider moves along the guided structure to drive one connection module to move, the connection module drives one aircraft arm to move with the slider and rotate relatively to the slider, so that the aircraft is unfolded or folded.
机译:一种用于无人机(UAV)的臂连杆可折叠装置,包括连杆模块和两个连接模块。连杆模块包括被引导的结构和滑块。滑块沿引导结构滑动。位于机身两侧的两个飞行器臂通过两个连接模块分别与滑块的两侧连接,每个连接模块的接头与滑块可旋转。每个连接模块上均设有凸出部,在该凸出部对应的机身上设有滑槽,该凸部插入滑槽中并沿滑槽滑动。滑动件沿着被引导的结构运动以驱动一个连接模块运动,该连接模块驱动一个飞行器臂与滑动件一起运动并相对于滑动件旋转,从而使飞机展开或折叠。

著录项

  • 公开/公告号US2018134369A1

    专利类型

  • 公开/公告日2018-05-17

    原文格式PDF

  • 申请/专利权人 HAOXIANG ELECTRIC ENERGY (KUNSHAN)CO. LTD.;

    申请/专利号US201715854773

  • 发明设计人 YU TIAN;WENYAN JIANG;

    申请日2017-12-27

  • 分类号B64C1/30;B64C39/02;

  • 国家 US

  • 入库时间 2022-08-21 13:05:24

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