Low-wind-resistance high-speed multi-rotor unmanned aerial vehicle

According to the low-wind-resistance high-speed multi-rotor unmanned aerial vehicle, an upward elevation angle of a fuselage is formed by the fuselage and horizontal rotors, when the fuselage flies forwards, the axis of the fuselage can be consistent with the flight direction, before the fuselage does not completely reach the horizontal state, the fuselage can provide additional lift force, and when the fuselage flies horizontally, the windward area is small, and air resistance is reduced; the flying speed can be higher, a larger voyage can be achieved, the streamline lift fuselage further reduces wind resistance and provides additional lift, the flying speed can be higher, and the larger voyage can be achieved. The fuselage is provided with the ailerons, additional lift force and flight stability are provided while the strength of the fuselage is improved, the ailerons structurally comprise reinforcing ribs capable of serving as rotor arms, the overload resistance of the unmanned aerial vehicle can be improv