发明名称 LANDING GEAR FOR UNMANNED AERIAL VEHICLE
摘要 Landing gear for an unmanned aerial vehicle, comprising a first support column (1), a second support column (2), a third support column (3), a first damping apparatus (4), a first support apparatus (5), a second damping apparatus (6), a second support apparatus (7), and a third damping apparatus (8); a first rectangular groove (11), a roller (12), and a first support bracket (13) are disposed on the first support column (1); a first recessed groove (21), a second recessed groove (22), a first spring (24), a first moving block (23), and a rectangular block are disposed on the second support column (2); a first positioning rod (31) and a second spring (32) are disposed on the third support column (3); the first damping apparatus (4) comprises a first fixing rod (41), a first rotating rod (42), a second rotating rod (43), a first fixing block (41), a third spring (45), and a positioning part (46); the first support apparatus (5) comprises a second support bracket (51), a first support rod (52), a first crossbar (53), and a third support bracket (54); and the second damping apparatus (6) comprises a first horizontal plate (61), a second positioning rod (62), a second horizontal plate (63), a clamping part (64), and an elastic part (65). The present landing gear for an unmanned aerial vehicle provides better and more stable support for an unmanned vehicle, and also has a good damping function, thus preventing damage to the unmanned aerial vehicle.
申请公布号 WO2017008530(A1) 申请公布日期 2017.01.19
申请号 WO2016CN77165 申请日期 2016.03.23
申请人 ZHANG, Ping 发明人 ZHANG, Ping
分类号 B64C25/62;B64C25/02 主分类号 B64C25/62
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