The invention provides an aircraft which combines an air pressure power principle and a Gaussian electromagnetic propeller principle, and the inventor introduces a Gaussian electromagnetic propeller into a novel aircraft which originally integrates a lever principle and the air pressure power principle, so that the design that fuel propulsion is changed into electric energy propulsion is realized; the saucer-shaped aircraft is an olive-shaped control center, two aircraft compressor blades are annularly attached to each other up and down on the olive-shaped control center, each aircraft compressor blade is provided with a set of four to six Gaussian electromagnetic propulsion rings, and the four to six Gaussian electromagnetic propulsion rings are equidistantly assembled on the compressor blades surrounding an aircraft body. The upper Gaussian electromagnetic propulsion ring and the lower Gaussian electromagnetic propulsion ring are overlapped in a line ring between two compressor blades, the lower ring and the upper ring are located on the same section, convection is formed by currents of the two coils during power supply, an oxyhydrogen energy storage and power generation device is assembled in the olive-shaped aircraft life control center, and the aircraft body control center controls the voltage of a switch. Three exhaust ports which are opened and closed by valves and are vertical to the exhaust direction are arranged below the gas compressor, a main exhaust port which is opened and closed by a valve is arranged at the tail part of the aircraft, and two sides of the main exhaust port are respectively provided with an exhaust port which is opened and closed by a valve and can adjust the direction of the aircraft; and the flexible control of the flight state and direction of the aircraft is realized by controlling the opening and closing of the valves of the six exhaust ports.

    本发明提供一种将空气压力动力原理和高斯电磁推进器原理相结合的飞行器,发明人通过对自己原先综合杠杆原理和空气压力动力原理的新型飞行器引入高斯电磁推进器,从而实现原先由燃料推进改为电能推进的设计,具体包括:碟形飞行器是橄榄形控制中心,橄榄形控制中心上有两个飞行器压气机叶片呈环状一上一下贴合在一起,每个飞行器压气机叶片又分别装配有一套四至六个高斯电磁推进环,分别等距离装配在环绕飞行器本体的压气机叶片上,上下两套高斯电磁推进环在两个压气机叶片中间的线环重叠,下部的环和上部的环处于同一个截面,供电时两线圈电流形成对流,橄榄型飞行器生活控制中心里面装配有氢氧储能和发电装置,飞行器本体控制中心控制电门电压,压气机下面有三个有阀门控制开合的垂直排气方向的排气口,飞行器尾部有个有阀门控制开合的主排气口,主排气口两侧各有一个有阀门控制开合可调整飞行器方向的排气口,通过对这六个排气口阀门开合管控从而实现对飞行器飞行状态和方向的灵活操控。


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    Title :

    Aircraft combining air pressure power principle and Gaussian electromagnetic propeller principle


    Additional title:

    一种将空气压力动力原理和高斯电磁推进器原理相结合的飞行器


    Contributors:

    Publication date :

    2024-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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