Gyro battery aircraft

Abstract

The invention discloses a gyro battery aircraft, and the aircraft comprises an aircraft shell, a hollow motor, a fixed-angle upper rotor wing, an adjusting-angle lower rotor wing, a gyro battery and a control adjusting system; the hollow motor serves as aircraft power, and the fixed-angle upper rotor wing drives the gyro battery to rotate and generates fixed lift force; the counter-rotating gears drive the angle-adjusting lower rotors to reversely rotate to generate adjustable lift force, the movement in all the vertical horizontal directions and the adjustment of all postures in the air can be completed by adjusting the corresponding direction adjusting plates, and the counter-rotating gears enable the fixed-angle upper rotors and the angle-adjusting lower rotors to reversely rotate to prevent the aircraft from spinning. Compared with the prior art, the unmanned aerial vehicle has the advantages that gyroscope mechanical energy is formed through the weight of the main battery and the weight of the control device, flying is stable through gyroscope inertia, various postures can be stably kept in the air, and under the action of the adjustor, the postures are diversified, safety is high, applicability is good, and popularization is convenient.

Description

Technical field [0001] The present invention relates to aircraft, and specifically a uniaxial rotator. Background technique [0002] Ordinary rotor aircraft divided by single shaft and multi-axis, uniaxial and multi-axis propeller directly mounted on the spindle of the engine, change the rotor to the wind angle to achieve the adjustment of the aerial gesture of the aircraft, change the speed to achieve lift, rely on the gyroscope to fly, air The posture change is less, the rise and falling speed is slow, the posture position of the gyroscope feedback is transmitted to the controller, and the controller issues an instruction to the executive delay, so the stability is not good, the helicopter is a typical single-axis aircraft, generally relying on the tail to prevent self Switch, once the tail fault, the body began to rotate, and there is also a method of adopting the engine spindle and the center of gravity. Other aircraft of the multi-axis is dependent on multiple engines in the...

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is that due to the deficiencies in the structural design of the existing aircraft, the flight principle and the use of kinetic energy are unreasonable, the flight of the aircraft is not stable enough, the safety is not high, the scope of use is limited, and it does not meet the current needs.

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