Wing connecting structure of sensor unmanned aerial vehicle, wing and unmanned aerial vehicle
A technology for connecting structure and unmanned aerial vehicle, applied in the field of unmanned aerial vehicle, can solve the problems of difficult mechanical connection method and thick foam interlayer, and achieve the effect of satisfying the structural integrity of the wing, the satisfactory connection strength, and the feasible connection process
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[0072] figure 1 An exploded view of the structure of the wing of the drone of the present embodiment is shown; figure 2 A sectional view of the wing of the drone of the present embodiment is shown; image 3 A top view of the drone wing of the present embodiment is shown; Figure 4 A schematic diagram of the wing connection structure of this embodiment is shown.
[0073] Such as figure 1 As shown, the UAV wing includes a wing skeleton 3 and an upper skin 1 and a lower skin 2, such as figure 2 As shown, the upper skin 1 and the lower skin 2 cover the wing frame 3; wherein, the upper skin 1 and the lower skin 2 have the same structure, as Figure 4 As shown, it includes a main bearing plate 12 of carbon fiber plate material, a foam plate 11 and a glass fiber plate 10 stacked in sequence from the inside to the outside, and the antenna unit 9 is built in the foam plate 11;
[0074] Such as image 3 As shown, the edge of the wing frame 3 includes a front beam 4 arranged alon...
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