The invention discloses a carbon fiber folding wing for an unmanned aerial vehicle, which belongs to the field of unmanned aerial vehicle processing. The carbon fiber folding wing comprises a vehiclebody, a push-pull groove is formed in the bottom of the side face of the vehicle body, a sleeve rod groove is formed in the side face of the vehicle body, the top of the vehicle body is sleeved with athreaded rod in a threaded mode, a push-pull rod is movably sleeved with the sleeve rod groove, a containing groove is formed in the top of the push-pull rod, a supporting rod is movably sleeved withthe containing groove, and the bottom end of the outer portion of the supporting rod is sleeved with a first threaded sleeve in a threaded mode. By arranging the supporting rod and a second threadedsleeve, when the unmanned aerial vehicle is not used, the wing is folded and the second threaded sleeve is rotated, so that one end of the wing is movably connected into the second threaded sleeve ina sleeved mode, and at the moment, the outer part of the supporting rod is pressed to enable the supporting rod to drive the wing to be movably connected into the containing groove in a sleeved mode;the problem that the wing needs to be disassembled and stored when the unmanned aerial vehicle is not used is avoided, and therefore convenience is brought to use of the unmanned aerial vehicle.
本发明公开了一种无人机用碳纤维折叠机翼,属于无人机加工领域,包括机体,所述机体侧面的底部开设有推拉槽,且机体的侧面开设有套杆槽,所述机体的顶部螺纹套接有螺纹杆,所述套杆槽的内部活动套接有推拉杆,所述推拉杆的顶部开设有放置槽,所述放置槽的内部活动套接有支撑杆,所述支撑杆外部的底端螺纹套接有一号螺纹套;通过设置支撑杆和二号螺纹套,当无人机不使用时,通过折叠机翼并转动二号螺纹套,使得机翼的一端活动套接在二号螺纹套的内部,此时按压支撑杆的外部,促使支撑杆带动机翼活动套接在放置槽的内部,避免了无人机在不使用时需要对机翼进行拆卸保存的问题,从而为无人机的使用带来了便利。
Carbon fiber folding wing for unmanned aerial vehicle
一种无人机用碳纤维折叠机翼
09.02.2021
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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