Unmanned aerial vehicle for pesticide spraying
A technology for drones and pesticides, applied in the field of aircraft, can solve problems such as affecting spraying efficiency, large body vibration, damage to pesticide medicine boxes, etc., and achieve the effects of improving spraying efficiency, increasing bearing capacity, and improving stability.
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Embodiment 1
[0025] This embodiment provides a drone for spraying pesticides, such as figure 1 As shown, the drone for spraying pesticides includes a fuselage 1, a main rotor 2 arranged on the top of the fuselage 1, and a landing gear 3 arranged at the bottom of the fuselage 1. The landing gear 3 includes two frame bodies 31, each frame body 31 is provided with a pesticide box 4 and a spraying device 5. The spraying device 5 includes a frame 51 and three pesticide spray heads 52 arranged on the frame 51 . One end of the bracket 51 is fixed on the frame body 31 , and the other end extends outwards. Three pesticide nozzles 52 are evenly distributed on the bracket 51 along the extending direction of the bracket 51 . The bottom of the fuselage 1 is also provided with a pesticide nozzle 52 communicating with the pesticide box 4 , and the pesticide spraying of the drone can be carried out through the pesticide nozzle 52 .
[0026] The length of the bracket 51 is 2 to 4 times of the width of th...
Embodiment 2
[0031] This embodiment provides a drone for spraying pesticides, such as figure 2 As shown, its basic structure is the same as that of Embodiment 1, including a fuselage 1, a main rotor 2 arranged at the top of the fuselage 1, and a landing gear 3 arranged at the bottom of the fuselage 1. The landing gear 3 includes two frame bodies 31, each frame body 31 is provided with a pesticide box 4 and a spraying device 5. A first lift wing 6 is arranged between the two frames 31 , and the first lift wing 6 is in the shape of a dish protruding toward the fuselage 1 .
[0032] The difference is that the UAV in this embodiment is provided with a second lift 8 above the main rotor 2, the structure of the second lift 8 is basically the same as that of the first lift 6, and it protrudes toward the fuselage 1. dish shape. Through the combination of the first lift wing 6 and the second lift wing 8, the carrying capacity of the UAV can be further improved.
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