Full electromagnetic suspension type magnetic control rotor system

Abstract

A full electromagnetic suspension type magnetic control rotor system comprises variable magnetic controllers, a rotor ball, a stator magnetic coil, an inner curved surface ring stator and a rotor fusion, wherein the stator magnetic coil is fixed on the outer ring of the inner curved surface ring stator, and the outer ring of the stator magnetic coil is sleeved with the rotor fusion; the variable magnetic controllers are mounted at the top of the rotor ball, and a control system is arranged in the rotor ball and used for controlling magnetic change of the variable magnetic controllers; the rotor ball is sleeved with the inner curved surface ring stator. The system is simple and reliable on the whole, and mechanical friction among structures is effectively reduced; when a rotor rotates to produce lift force, repulsive force of a variable magnetic part can be changed, so that a rotor disc swings around the rotor ball in a controllable range, and pitching and roll control of a rotor craftis realized; the full electromagnetic suspension type magnetic control rotor system adopts simple and reliable principles and has more concise and higher efficiency as compared with a main rotor system of a helicopter.

Description

technical field [0001] The invention relates to the technical field of control of a rotor unmanned helicopter power system, in particular to a full electromagnetic levitation magnetically controlled rotor system. Background technique [0002] Today, with the rapid development of drones, its application has penetrated into various fields. The control of the power system, throttle response, and rotor attitude of the electric rotor unmanned helicopter has been affected by traditional mechanical control. Limited by the storage capacity of the battery, it is required that the energy consumption loss should be as small as possible when the electric energy is converted into lift, so as to improve the endurance of the aircraft; when there is a new breakthrough in the battery energy storage technology, it will lay the foundation for the development of the electric rotor unmanned helicopter. Existing technical problems: 1. Regarding the throttle response of the rotor unmanned helicop...

AI Technical Summary

Problems solved by technology

Existing technical problems: 1. Regarding the throttle response of the rotor unmanned helicopter: the throttle control of the electric rotor is usually achieved by changing the pitch, and it also includes a complex and heavy reduction gear mechanism, and there are multiple mechanical friction factors. Reduced efficiency of converting electrical energy into lift

2. The attitude control problem of the rotor unmanned helicopter: the conventional electric unmanned helicopter controls the pitch and roll of the rotor disc through the steering gear

There is mechanical friction directly in the mechanical connecting rod, and the messy control mechanism increases the flight resistance

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