Unmanned aerial vehicle with underwater submerging function
A technology for unmanned aerial vehicles and aerial vehicles, applied in the field of unmanned aerial vehicles, can solve the problems that it is difficult for aircraft to perform tasks in water, increase the difficulty of operations, and it is difficult to meet multi-task and multi-environment execution tasks, so as to achieve good application prospects and improve multi-function The effect of work ability
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Embodiment 1
[0096] The unmanned aerial vehicle with underwater diving function disclosed in Embodiment 1, such as figure 1 As shown, it includes an aircraft frame 2 and an aircraft fuselage 1 that is fitted and installed with it, and the aircraft fuselage 1 is streamlined as a whole; figure 2 As shown, the submersible functional assembly 3 includes a water flow duct 30 and a water pump 31 arranged therein; the aircraft fuselage 1 is provided with four symmetrically distributed water flow ducts 30, which are opened at the front end of the aircraft fuselage 1, and the outlet is located in the aircraft fuselage 1. The tail end of fuselage 1, such as image 3 As shown, the tail end of the aircraft fuselage 1 is provided with a tail fin 11, and four identical tail fins 11 are symmetrically distributed on the outer wall of the aircraft fuselage between the four water flow ducts 30 at intervals;
[0097] The flight function assembly 4 is arranged and installed on the aircraft frame 2, wherein ...
Embodiment 2
[0101] In Embodiment 2, the unmanned aerial vehicle includes an aircraft frame 2 and an aircraft fuselage 1 fitted with it; the aircraft frame 2 is arranged in the middle of the aircraft fuselage 1, and the aircraft fuselage 1 is divided into the front part of the aircraft fuselage, the Two parts at the rear of the aircraft fuselage; such as Figure 8 As shown, the aircraft fuselage 1 is in a vertical attitude, and two independent aircraft attitude adjustment assemblies 5 are provided inside the aircraft fuselage 1; The second motor 32 is arranged inside the aircraft fuselage and connected with the propeller 33; the propeller 33 is arranged inside the water flow cover, and the water flow cover has suitable water inlet, water outlet and cover structure to ensure that the propeller provides sufficient power ;
[0102] The aircraft attitude adjustment assembly 5 provided on the front of the aircraft fuselage 1 includes a third pressurized water tank 55 and a fourth pressurized w...
Embodiment 3
[0108] The unmanned aerial vehicle with underwater diving function disclosed in embodiment 3, such as Figure 10 As shown, it includes an aircraft frame 2 and an aircraft fuselage 1 that is fitted and installed with it, and the aircraft fuselage 1 is streamlined as a whole; The second motor 32 connected to it; the tail end of the aircraft fuselage 1 is provided with a tail fin 11, and a total of four tail fins 11 are arranged, which are symmetrically distributed on the outer wall of the aircraft fuselage around the submersible functional assembly 3, such as Figure 11 shown;
[0109] The aircraft frame 2 is provided with flight function components 4, wherein the four flight function components 4 are symmetrically arranged along the outer circumference of the aircraft fuselage 1, such as: Figure 12 The flight function assembly 4 includes a retractable rotor arm 40, and one end of the retractable rotor arm 40 is rotatably connected to the aircraft frame 2, so as to realize the...
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