Novel multifunctional box type joined wing water unmanned aerial vehicle
A multi-functional, unmanned aerial vehicle technology, applied in the direction of seaplanes, unmanned aircraft, motor vehicles, etc., can solve the problems of dynamic unbalanced flight course, dynamic instability, and restrictions on the wide application of water unmanned aerial vehicles. Achieve the effects of improving endurance and mission continuity, improving stability and heading controllability, and improving range and cruising time
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Embodiment 1
[0032] A novel multi-functional box-type winged water unmanned aerial vehicle of the present invention, the novel multi-functional box-type joint-wing water unmanned aerial vehicle comprises a hull type fuselage 1, a box-type joint wing 2, a vertical tail 3, a propeller propulsion Device 4, fuselage load 5, wing solar power generation device 6;
[0033] The hull-type fuselage 1 includes an upper arc-shaped fuselage 11, a bottom multi-stage stepped rectification hull 12, and a splash suppression bilge bend 13; the bottom multi-stage stepped rectification hull 12 is provided with an upper arc-shaped Fuselage 11, the two sides of the bottom suppress the splashing. The upper arc-shaped fuselage 11 can be modified and improved according to actual needs to adapt to loads of different shapes and sizes. The bottom multi-step rectification hull 12 adopts at least 2 steps to rectify the water flow to simulate Control the generation of water waves, reduce the resistance of the water sur...
Embodiment 2
[0043] The difference between embodiment 2 and embodiment 1 is that: the anhedral angle is 5.6 degrees, and the anhedral angle is 0.3 degrees.
[0044] The load 5 is installed inside or at the front of the hull-type fuselage 1, a cavity is provided in the front 51, and a laser sensor for detection or monitoring is provided in the cavity; the interior 52 is provided with A combination of the three in the water quality sampling device, the storage battery of the solar power generation device 6 or the engine of the propeller propulsion device 4, the payload of the interior 52 is 0.3 kg.
[0045] The solar power generation device 61 on the upper surface of the front wing and the solar power generation device 62 on the upper surface of the rear wing are polysilicon solar power generation devices.
Embodiment 3
[0047] The difference between embodiment 3 and embodiment 1 is that: the anhedral angle is 0.2 degrees, and the anhedral angle is 6.8 degrees.
[0048] The load 5 is installed inside or at the front of the hull-type fuselage 1, a cavity is arranged in the front 51, and an infrared sensor for detection or monitoring is arranged in the cavity; the inside 52 is provided with Combination of the two types of water quality sampling device and fish food throwing device, the payload of the interior 52 weighs 11kg.
[0049] The solar power generation device 61 on the upper surface of the front wing and the solar power generation device 62 on the upper surface of the rear wing are thin-film solar power generation devices.
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