Flying motorcycle or automobile and flight attitude adjustment method thereof

Abstract

The invention discloses a flying motorcycle or automobile and a flight attitude adjustment method thereof. A flying motorcycle or automobile body is provided with a thruster and a thruster driving device. A propeller is mounted in the thruster. The thruster driving device controls rotation direction of the thruster. The thruster comprises a left front thruster body, a right front thruster body and a rear thruster body, wherein the left front thruster body and the right front thruster body are mounted on the left side and the right side of the front portion of the motorcycle or automobile body symmetrically, and the rear thruster body is mounted on the rear side of the motorcycle or automobile body. According to the flight attitude adjustment method, angle inclination of the thruster bodies mounted on the two sides and the rear portion of the flying motorcycle or automobile is driven by the thruster driving device to achieve turning, forward movement, backward movement, left translation and right translation of the flying motorcycle or automobile. The flying motorcycle or automobile can be always kept in a horizontal state during flight, can be applied to the field of manned flight and is quite wide in application range.

Description

technical field [0001] The invention relates to a small aircraft and an operation control method thereof, in particular to a flying motorcycle or automobile and a method for adjusting its flight attitude. Background technique [0002] Personal aircraft is a new application field of small aircraft. Most of the existing small aircraft are used to carry various measuring instruments for high-altitude detection or high-altitude object throwing. They can be used in various fields such as agriculture, detection, meteorology, disaster forecasting, and rescue. field. However, there are not many small aircraft that can carry people, and there is a lot of room for research. [0003] Existing aircraft is divided into two kinds of fixed-wing aircraft and multi-rotor aircraft. Fixed-wing aircraft generally use two methods of steering, one is purely by the vertical tail steering, and the other is the wing ailerons combined with the horizontal tail steering. Turning purely by the vertic...

AI Technical Summary

Problems solved by technology

The aileron of the wing cooperates with the steering of the horizontal tail, through the lifting of the aileron, the fuselage is tilted, and the corner is turned by the action of centrifugal force. This method requires the aircraft itself to tilt, and it will increase the number of pilots when it is applied to the personal aircraft. It is not suitable for the use of personal aircraft, it is used in observation and monitoring, and it is not conducive to the loading and transportation of equipment and instruments.

[0004] Existing multi-rotor aircraft all use changing the output power of the aircraft engine, or changing the pitch of the blades to achieve the attitude change of the aircraft; in order to make the aircraft fly smoothly, when adjusting each flight attitude, how to change the speed of the engine and how to change it? The pitch of the propeller needs to be calculated accurately by computer programming. The process is cumbersome and difficult to popularize, and it is not easy to cope with the complex and changeable flight environment. With this method of flight attitude control, the aircraft will still tilt during flight. Increase the safety risk of riding

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