Unmanned aerial vehicle structure and unmanned aerial vehicle with stealth function
A drone and fuselage technology, applied in the field of drones, can solve the problems of difficult disassembly and low stability of drones
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Embodiment 1
[0040] Such as Figure 1-5 As shown, the UAV structure provided by the present embodiment includes a fuselage 10, wings 20 and a central control unit 30; the inside of the fuselage 10 is provided with a cabin 40, and the central control unit 30 is arranged in the cabin 40. 30 is used to receive instructions and issue instructions; the wings 20 are arranged along the circumference of the fuselage 10, and the wings 20 are used to provide power to drive the fuselage 10 to hang in the air, and the central control unit 30 can drive the wings 20 to generate power; the fuselage 10 Comprising an upper fuselage 101 and a lower fuselage 102, the upper fuselage 101 and the lower fuselage 102 are fastened together, and the upper fuselage 101 and the lower fuselage 102 jointly form the cabin 40; the upper fuselage 101 and the lower fuselage 102 are both in the shape of Streamlined structure.
[0041] Specifically, the UAV structure includes a fuselage 10, wings 20 and a central control un...
Embodiment 2
[0081] This embodiment also provides a UAV with a stealth function, which includes the above-mentioned UAV structure, and the outer sides of the fuselage 10 and the wings 20 are provided with a stealth coating.
[0082] Specifically, in order to improve the stealth of the UAV structure, stealth coatings are provided on the outer walls of the fuselage 10 and the wings 20, thereby forming a UAV with a stealth function.
[0083] Among them, the stealth coating is applied with stealth materials, which can reduce the detection rate and improve the survival rate of the drone itself.
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