The invention discloses an unmanned aerial vehicle and a driving device of a cracking-type auxiliary wing thereof. The unmanned aerial vehicle comprises a wing, a cracking type auxiliary wing and a transmission device, wherein the transmission device comprises a driving steering engine, adjustable clamping holes, a transmission connecting rod and a torsion machine arm; the driving steering enginetransmits power to the adjustable clamping holes; one end of the transmission connecting rod is connected with the adjustable clamping holes while the other end of the transmission connecting rod is propped to the torsion machine arm; and the cracking type auxiliary wing is arranged on the lower rear part of the wing. According to the unmanned aerial vehicle and the driving device of the cracking-type auxiliary wing thereof disclosed by the invention, by adopting the cracking-type auxiliary wing structure, gaps are not reserved on the surface of the wing, so that the excellent pneumatic performance of the wing is met, and benefit guarantee is provided for pavement of solar battery panels on the wing; and meanwhile, through cooperation between the cracking-type auxiliary wing and the driving device, operation ways are simplified, the operation efficiency is improved, and the weight of the driving device is also reduced at the same time.
本发明提出了一种无人机及其开裂式副翼的驱动装置,包括:机翼、开裂式副翼和传动装置;所述传动装置包括驱动舵机、调整卡孔、传动连杆和扭转机臂,所述驱动舵机将动力传输到调整卡孔,所述传动连杆一端与调整卡孔连接,另一端与扭转机臂抵接;所述开裂式副翼位于机翼下后方。本发明采用开裂式副翼结构,机翼表面没有缝隙,既满足机翼优良的气动性能,也给机翼铺设太阳能电池板提供有利保证;同时,开裂式副翼与驱动装置的配合,简化了操作方式,提高了操作效率,同时也减轻了驱动装置的重量。
Unmanned aerial vehicle and driving device of cracking-type auxiliary wing thereof
一种无人机及其开裂式副翼的驱动装置
2020-12-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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