A tilt vertical take-off and landing fixed-wing aircraft

Abstract

A tilt vertical take-off and landing fixed-wing aircraft belongs to the technical field of aircraft, and comprises a fuselage, a wing, a tail wing, a left rotor thrust device, a right rotor thrust device, a driving motor, a rotating shaft, and a flight control device, wherein, the tilt vertical take-off and landing fixed-wing aircraft comprises a fuselage, a wing, a tail wing, a left rotor thrustdevice and a right rotor thrust device. The inner wing is fixed on the fuselage, and the inner wing and the outer wing are fixed by fixing rods. The outer wing is fixed on the fuselage by fixing rods.The outer wing is provided with an aileron; Left rotor thrust device and right rotor thrust device are provided with connecting rods; a left rotor thrust device and a right rotor thrust device are movably connected between an inner wing and an out wing of that wing through a bearing structure; Both the left rotor thrust device and the right rotor thrust device provide thrust force in the form that the motor drives the propeller to rotate. The driving device drives the rotating shaft. The rotating shaft tilts both the left rotor thrust device and the right rotor thrust device via a synchronousbelt. The invention can perform vertical take-off and landing, the flight process is stable, the safety factor is high, and the invention is suitable for the work of logistics transportation, air fire extinguishing, post-disaster rescue and the like.

Description

technical field [0001] A tilting vertical take-off and landing fixed-wing aircraft belongs to the technical field of aircraft, and in particular relates to a vertical take-off and landing fixed-wing aircraft. Background technique [0002] Although the flight speed of the aircraft is fast and the flight time is long, it cannot hover at a fixed point; although the multi-rotor aircraft can hover in the air, its flight time is short and the flight speed is slow. Although there are currently some aircrafts that combine multi-rotor aircraft and aircraft, they all have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part becomes a burden on the aircraft. Increased the burden on the aircraft. Contents of the invention [0003] In view of this, the present invention provides a tilting vertical take-off and landing fixed-wing aircraft, which can perform vertical lift, hover in the air, and cruise for a long time and a lon...

AI Technical Summary

Problems solved by technology

[0002] Although the flight speed of the aircraft is fast and the flight time is long, it cannot hover at a fixed point; although the multi-rotor aircraft can hover in the air, its flight time is short and the flight speed is slow.

Although there are currently some aircrafts that combine multi-rotor aircraft and aircraft, they all have certain defects. When flying in fixed-wing mode, the power of the multi-rotor part must be stopped, and this part becomes a burden on the aircraft. increase the burden on the aircraft

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