Annular honeycomb excitation vector-propelled double-rotor aircraft

Abstract

The invention discloses an annular honeycomb excitation vector-propelled double-rotor aircraft. The annular honeycomb excitation vector-propelled double-rotor aircraft comprises two rotor bodies and aconnecting bridge for connecting the two rotor bodies, wherein each rotor body comprises an excitation pole shell; the excitation pole shell is annular; an excitation wall is arranged on the inner wall of the excitation pole shell; a supporting frame is mounted on the upper part of the excitation pole shell; a ball hinge shaft is mounted at the center of the supporting frame; a propeller is mounted on the end part of the ball hinge shaft, so that the propeller rotates around the ball hinge shaft; a propeller ball hinge hole is formed in the center of the propeller, and is matched with the ball hinge shaft to form movable connection; the propeller has four blades; permanent magnets are arranged on the end parts of the blades; the permanent magnets are hollow; hollow cavities are formed inthe middle parts of the permanent magnets; springs are fixed to the inner walls of the cavities.

Description

technical field [0001] The invention relates to an annular honeycomb excitation vector propulsion double-rotor aircraft. Background technique [0002] At present, most aircraft adopt a single-rotor design. The improvement of flight speed and efficiency mainly depends on improving the engine design, and the development cycle of the engine is very long. It is difficult to improve the performance of the aircraft by increasing the thrust of the engine in a short period of time. The existing dual-rotor aircraft relies on ordinary propellers. The motor and control system cannot realize the flight of the aircraft. Contents of the invention [0003] In view of the above existing problems, the present invention provides a circular honeycomb excitation vector propulsion birotor aircraft, and the normal control of the biplane aircraft can be realized by vector propulsion of the screw motor. [0004] In order to achieve the above object, the technical solution provided by the present...

AI Technical Summary

Problems solved by technology

[0002] At present, most aircraft adopt a single-rotor design. The improvement of flight speed and efficiency mainly depends on improving the engine design, and the development cycle of the engine is very long. It is difficult to improve the performance of the aircraft by increasing the thrust of the engine in a short period of time. The existing dual-rotor aircraft relies on ordinary propellers. The motor and control system cannot realize the flight of the aircraft

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