Fixed wing aircraft with four accelerators

Abstract

The invention discloses a fixed wing aircraft with four accelerators, and belongs to the technical field of aircrafts. The fixed wing aircraft with the four accelerators comprises a lift force platform, a controller, a fixed support, motors, propellers, wings, a nose, a tail and the accelerators. According to the operating principle, the four motors can synchronously drive the propellers to rotate, the wind direction generated by the propellers is basically centered on the center of the lift force platform, and the axes of the motors are tangent to the circumference of the radius from the center point of the lift force platform to the center point of the bottom face of the fixed support; and a generated vortex above the middle part of the lift force platform is similar to a tornado, and alow pressure area is formed in the middle part above the lift force platform. The fixed wing aircraft with the four accelerators fully utilizes the low pressure area which is similar to the tornado ofthe device to enable the lift force platform to generate large lift force, the efficiency of lift force device is improved, the fixed wing aircraft can accelerate forward takeoff and vertical takeoffand landing, the fixed wing aircraft can take off without a runway, and takeoff speed of the fixed wing aircraft is shortened.

Description

technical field [0001] A fixed-wing aircraft with four acceleration devices belongs to the technical field of aircraft, and in particular relates to a fixed-wing aircraft with four acceleration devices. Background technique [0002] Traditional fixed-wing aircraft need a long runway to take off, and the rotation speed of the rotor makes the aircraft take off at a certain take-off speed. The take-off speed is slow, the stability is low, and the safety is not high. There is no forward acceleration to take off, and there is no acceleration to take off and land upwards. The effect of making the fixed-wing aircraft take off is completely limited by the field. You can't change the direction of flight, you can only fly forward from the front of the fixed-wing aircraft; the fixed-wing aircraft does not have the take-off and landing function of the multi-rotor. Contents of the invention [0003] The purpose of the present invention is to overcome the deficiency of above-mentioned ...

AI Technical Summary

Problems solved by technology

[0002] Traditional fixed-wing aircraft need a long runway to take off, and the rotation speed of the rotor makes the aircraft take off at a certain take-off speed. The take-off speed is slow, the stability is low, and the safety is not high. There is no forward acceleration to take off, and there is no acceleration to take off and land upwards. effect, making the take-off of fixed-wing aircraft completely limited by the field

You can't change the direction of flight, you can only fly forward from the front of the fixed-wing aircraft; fixed-wing aircraft do not have multi-rotor takeoff and landing functions

Images