The invention relates to the technical field of unmanned aerial vehicles, in particular to a lifting aileron for an unmanned aerial vehicle and a lifting aileron control device.The lifting aileron comprises a fuselage, a left front wing and a right front wing are connected to the fuselage, and a lifting aileron I is connected to the leeward side of the left front wing through a flexible connecting piece I; the lifting aileron I is connected to the leeward side of the front right wing through a flexible connecting piece I, the lifting aileron II is connected to the leeward side of the front right wing through a flexible connecting piece II, and the lifting aileron I and the lifting aileron II are used for being regulated and controlled by a lifting aileron control device to conduct pitching deflection, so that in the flight process of the unmanned aerial vehicle, the lifting aileron I and the lifting aileron II are regulated and controlled through the lifting aileron control device; and controlling the flight attitude of the unmanned aerial vehicle. According to the miniature unmanned aerial vehicle lifting aileron, the lifting aileron and the front wing are flexibly connected through the flexible connecting piece, the flexible connecting piece limits the moving position of the lifting aileron, meanwhile, the connecting rigidity of the lifting aileron and the front wing is weakened, and the operability of the miniature unmanned aerial vehicle lifting aileron is improved.
本发明涉及无人机技术领域,具体涉及一种无人机用升降副翼及升降副翼控制装置,包括机身,所述机身上连接有左前机翼和右前机翼,还包括:升降副翼Ⅰ通过柔性连接件Ⅰ连接在所述左前机翼的背风侧;升降副翼Ⅱ通过柔性连接件Ⅱ连接在所述右前机翼的背风侧,所述升降副翼Ⅰ、升降副翼Ⅱ用于受升降副翼控制装置调控进行仰俯偏转,使得,无人机在飞行过程中,通过升降副翼控制装置对升降副翼Ⅰ、升降副翼Ⅱ进行仰俯偏转的调控,对无人机的飞行姿态进行控制。本发明,通过柔性连接件将升降副翼与前机翼进行柔性连接,柔性连接件限制升降副翼的活动位置,同时减弱升降副翼与前机翼的连接刚性,提升了微型无人机升降副翼的可操作性。
Lifting aileron for unmanned aerial vehicle and lifting aileron control device
一种无人机用升降副翼及升降副翼控制装置
2024-08-16
Patent
Electronic Resource
Chinese
IPC: | B64U |
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