A locking mechanism of a pan-tilt, a pan-tilt, and an unmanned aerial vehicle, the pan-tilt comprising a first pan-tilt component (1), a second pan-tilt component (2), and a locking mechanism. The locking mechanism comprises: a connection member (3) used for movably connecting the first pan-tilt component (1) and the second pan-tilt component (2); a locking member (4) for locking or unlocking thefirst pan-tilt component (1) and the second pan-tilt component (2); and an operating member (5), the operating member (5) being able to pivot around the connection member (3) and being used for driving the locking member to lock or unlock the first pan-tilt component (1) and the second pan-tilt component (2). The connection member is provided to connect the two pan-tilt components, and the operating member pivotal around the connection member is provided to drive the locking member to lock or unlock the relative rotation of the two pan-tilt components, realizing quick assembly and disassemblyof the pan-tilt components and quick adjustment of the angle.
一种云台的锁定机构、云台及无人机,其中云台包括第一云台组件(1)、第二云台组件(2)和锁定机构,锁定机构包括:连接件(3),用于活动连接第一云台组件(1)和第二云台组件(2);锁定件(4),用于锁定或解锁第一云台组件(1)和第二云台组件(2);以及操作件(5),操作件(5)可围绕连接件(3)转动,用于驱动锁定件锁定或解锁第一云台组件(1)和第二云台组件(2)。通过设置连接件以连接两个云台组件,通过设置可围绕连接件转动的操作件从而驱动锁定件锁定或解锁两个云台组件的相对转动,实现了云台组件的快速装卸和角度的快速调节。
LOCKING MECHANISM OF PAN-TILT, PAN-TILT AND UNMANNED AERIAL VEHICLE
一种云台的锁定机构、云台及无人机
2021-01-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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