CN-121990169-A - Aircraft using Gaussian electromagnetic propulsion device to compress air

CN121990169ACN 121990169 ACN121990169 ACN 121990169ACN-121990169-A

Abstract

The invention provides an aircraft for compressing air by utilizing a Gaussian electromagnetic propulsion device, wherein the center of the disc-shaped aircraft is an olive-shaped control center, an oxyhydrogen energy storage tank and an oxyhydrogen battery device are arranged in the olive-shaped aircraft living control center, an aircraft body provides electric energy through the oxyhydrogen energy storage battery as required, two aircraft air compressor blades are overlapped together in an annular shape, the upper part and the lower part of the aircraft air compressor blades are respectively distributed with a pair of electromagnetic propulsion coil groups, each pair of electromagnetic coil groups corresponds to a set of annular neodymium magnet guide rail, two sides of the guide rail are equally divided according to the radian of a circular sector, each equally divided radian is respectively provided with a set of neodymium magnet, and electromagnetic coils matched with the neodymium magnet are assembled into an electromagnetic propulsion device, the electromagnetic propulsion coil groups on the air compressor blade wheels enable the two air compressor blades to rotate oppositely after being electrified reversely, neodymium coils are additionally distributed on the outer edges of the large air compressor blade wheels, the neodymium coils are distributed in an array shape at positions corresponding to the positions on the air compressor blade wheels outside the aircraft body, and the large air compressor blade wheels are rotated along with the large air compressor blade wheels to generate electric energy. The lower part of the annular pipe of the air compressor is provided with three exhaust ports perpendicular to the exhaust direction, substances after being acted by the high-energy ionization accelerator are discharged out of the aircraft through the exhaust ports, the side surface of the aircraft is also provided with an exhaust port, the inside of the aircraft is provided with a direction regulator, and the attitude and the direction of the aircraft are controlled through an electro-hydraulic control valve, the direction regulator and the high-energy ionization accelerator.

Inventors

ZHOU WEIPING

Assignees

周维平

Dates

Publication Date: 20260508
Application Date: 20251010

Claims (9)

1. The invention provides an aircraft for compressing air by utilizing a Gaussian electromagnetic propulsion device, which is characterized in that an olive-shaped control center is arranged at the center of the saucer-shaped aircraft, an oxyhydrogen energy storage tank and an oxyhydrogen battery device are assembled at the control center to provide electric energy for the aircraft, two compressed air blade wheels which are big one by one and small one are overlapped together, the edges of the upper and lower air compressor blades of the aircraft are respectively symmetrically distributed with an electromagnetic coil, each pair of electromagnetic coils corresponds to a set of annular neodymium magnet guide rail, the two sides of the guide rail are equally divided according to the arc of a sector, a set of homodromous neodymium magnets are assembled at the inner arc and the outer arc of each equally divided arc, the electromagnetic propulsion coils matched with the homodromous neodymium magnets form the Gaussian electromagnetic propulsion device, the coils are distributed at the outer edges of the large air compressor blades, and the array neodymium magnets on the aircraft form a high-energy power generation device along with the rotation of the large air compressor blade wheels to generate electric energy. The high-energy electric accelerator acts on substances in the air compressing blade pipeline, a ring pipe at the lower part of the air compressor is in an equilateral triangle shape and is provided with three exhaust ports which exhaust vertically downwards, the exhaust ports are discharged out of the aircraft through the exhaust ports after being acted by the high-energy accelerator, the side surface of the ring pipe is also provided with an exhaust port which is led to the side surface of the aircraft, and the attitude and the direction of the aircraft are controlled through an electro-hydraulic device and an electromagnetic propulsion accelerator. The top (bottom) of the olive-shaped control center is provided with a microwave photon radar range finder. And a switch assembly for controlling the input of electric energy to the electromagnetic propulsion guide rail.
2. The aircraft combining the aerodynamic pressure principle and the Gaussian electromagnetic propulsion principle by utilizing the Gaussian electromagnetic propulsion device to carry out air compression according to the invention is characterized in that the saucer-shaped aircraft adopts an oxyhydrogen power battery to provide electric energy, and the aircraft specifically comprises an olive-shaped aircraft main control room, wherein oxyhydrogen fuel cells are arranged in the main control room, oxyhydrogen energy storage tanks are respectively arranged on the periphery of the main control room to provide fuel sources for the saucer-shaped aircraft, the voltage and the current of the oxyhydrogen power cells can be regulated and controlled by controlling and adjusting the flow of an exhaust port of a valve of the oxyhydrogen energy storage tank, and an inlet and an outlet are arranged at the bottom of an olive-shaped control center of the aircraft, so that personnel can conveniently go in and go out at destination.
3. The aircraft compressed air by utilizing the Gaussian electromagnetic propulsion device according to claim 1, wherein the aircraft compressor blade wheel specifically comprises two sets of compressor blades with a large upper part and a small lower part, which respectively encircle an olive-type main control chamber of the aircraft, and the compressor blades are formed by steel frames and are attached with light high-strength alloy blades to form a contracted type pipe cavity channel. The circular pipe with three air outlets at the bottom is communicated with the small air impeller pipe cavity.
4. The aircraft for compressed air by using the Gaussian electromagnetic propulsion device according to claim 1, wherein the Gaussian electromagnetic propulsion device specifically comprises a pair of electromagnetic coils symmetrically arranged at the edges of the upper and lower compressor blade wheels respectively. The neodymium magnets on the guide rail are assembled according to the design of different radians such as inner and outer track circular arcs and the like, so that the Gaussian electromagnetic propeller is formed by the neodymium magnets and the electromagnetic coils. When the electromagnetic coil moves circularly under the action of a magnetic field, the two air compressing blade wheels also move circularly around the shaft.
5. The aircraft using the Gaussian electromagnetic propulsion device for air compression according to claim 1, wherein the built-in high-energy power generation device specifically comprises coils distributed on the outer edge of a large air compressor blade wheel of the aircraft, neodymium magnet arrays are arranged at the position with the largest radius of a disc-shaped body of the aircraft, the current direction frequency corresponding to the electric energy generated by the coils in each pair of neodymium magnet arrays is exactly synchronous with that on a Gaussian electromagnetic propulsion guide rail, and when two Gaussian electromagnetic propulsion coils are reversely powered, the upper coils of the large air compressor blade and the small air compressor blade do reverse circular motion in the neodymium magnet guide rail ring so as to realize air compression of the air compressor blade. When the large compressor blade wheel rotates circumferentially, the neodymium magnet at the edge of the compressor blade wheel and the coil at the edge of the aircraft form a power generation device, and high-energy electricity is generated under the action of a magnetic field when the compressor blade wheel rotates.
6. The aircraft using the Gaussian electromagnetic propulsion device for air compression according to claim 1, wherein the compression cooling air collecting device and the aircraft exhaust port concretely comprise a large amount of heat generated when an electromagnetic coil on an air compressor blade supplies power or generates power, the coil is cooled through air compression and conduction of the air compressor blade, three exhaust ports are distributed on the triangular equilateral lower part of an annular tube connected with a compression tube cavity of the air compressor wheel of the aircraft, the control of the running direction of the aircraft is mainly responsible, an exhaust port with a rudder communicated with the outer side between an upper air compressor blade and a lower air compressor blade through a pipeline is arranged on the side surface of the annular tube, and the control of the attitude and the direction of the aircraft is realized through the control of an electro-hydraulic device.
7. The aircraft that utilizes gaussian electromagnetic propulsion unit to carry out the air compression of one kind according to claim 1, wherein the high-energy plasma accelerates propulsion unit, specifically include each export of the aircraft and assemble a series of hollow appearance similar to many layers of wrapped bamboo shoots shape high-energy plasma that will go out of the earth respectively, each layer of wrapping closely distributes the air vent hole with the place that the bamboo shoots body combines, each layer of wrapping is formed by conductive metal, a positive negative interval connects with high-energy power supply respectively and forms the plasma accelerator, the root of bamboo shoots and the air compression pipeline seal link, the inner wall of air outlet cavity also distributes the conductive metal of multilayer funnel shape, connect with high-energy power supply respectively and form the plasma accelerator, the material compressed through the air compressor is through the air vent hole and then through the high-energy plasma accelerator acceleration device acceleration erupts, make the aircraft obtain kinetic energy.
8. The aircraft using the Gaussian electromagnetic propulsion device for air compression according to claim 1, wherein the microwave photon radar comprises a plurality of microwave photon radar transmitting and receiving devices respectively arranged at the upper top end and the lower top end of an olive-shaped control center of a disc-shaped aircraft and even at the whole body fixed position of the aircraft, so that obstacles can be avoided timely when the aircraft maneuvers at a high speed.
9. The aircraft that utilizes gaussian electromagnetic propulsion device to carry out pressure air, wherein the switch assembly that can regulate and control electromagnetic propulsion guide rail electric energy input specifically includes, on circumference form neodymium magnet guide rail, according to circumference subregion ratio power supply, according to the power supply coverage area of the requirement of aircraft flight status adjustment circumference form neodymium magnet guide rail, thereby realize from symmetrical local fritter, to symmetrical quarter, to symmetrical half, even whole guide rail regional power supply's conversion demand, with this realization manager to the start-up of aircraft body, hover, move fast to full speed flexible control.

Description

Aircraft using Gaussian electromagnetic propulsion device to compress air Technical Field The invention provides an aircraft for compressing air by utilizing a Gaussian electromagnetic propulsion device, and belongs to the technology in the fields of manned aviation and aerospace. Background The inventor introduces a hydrogen-oxygen fuel cell to provide kinetic energy based on the existing aircraft structure of the windlass lever principle and the air pressure power principle, and then changes the original fuel-propelled air-compressing blade wheel into an aircraft propelled by electromagnetic air-compressing blade wheel through a Gaussian electromagnetic propulsion device, an air compression device and an ionization acceleration device. Is intended to replace the traditional way of entering space, such as by rocket launching. Disclosure of Invention The invention provides an aircraft for compressing air by utilizing a Gaussian electromagnetic propulsion device, which is an aerospace aircraft device organically combined with an air pressure power device and a high-energy electric acceleration device by utilizing the Gaussian electromagnetic propulsion device under the condition that an oxyhydrogen fuel cell provides electric energy. In an alternative example, the aircraft that uses the gaussian electromagnetic propulsion device to perform air compression is in a disc shape, and the aircraft adopts the oxyhydrogen power battery to provide electric energy, which specifically includes: the hydrogen-oxygen fuel cell is arranged in the overall control chamber of the olive-shaped aircraft, the hydrogen-oxygen energy storage tanks are respectively arranged on the periphery of the overall control chamber, a fuel source is provided for the disk-shaped aircraft, the voltage and the current of the hydrogen-oxygen fuel cell can be regulated and controlled by controlling and adjusting the flow of the valve exhaust port of the hydrogen-oxygen energy storage tank, and an inlet and an outlet are arranged at the bottom of the olive-shaped control center of the aircraft, so that personnel can conveniently go in and out at the destination. In an alternative example, the aircraft using the gaussian electromagnetic propulsion device for compressing air comprises two sets of compressor blades with a large upper part and a small lower part, which respectively encircle an olive-type main control chamber of the aircraft, wherein the compressor blades are formed by a steel frame and a light high-strength alloy blade forms a contracted type pipe cavity channel, and an annular pipe with three air outlets at the bottom is communicated with a pipe cavity of the small air compressing impeller. In an alternative example, the aircraft that utilizes gaussian electromagnetic propulsion device to carry out the air compression includes two upper and lower compressor blade wheel edges and is equipped with a pair of propulsion electromagnetic coil group respectively symmetry, and on the aircraft body with the electromagnetic propulsion coil group on two upper and lower compressor blade wheels matched with be the ring form and distribute on neodymium magnet guide rail, neodymium magnet on the guide rail is assembled according to the design of the equal difference of radian such as inside and outside track circular arc to constitute gaussian electromagnetic propulsion with electromagnetic coil group. When the electromagnetic coil group moves circularly under the action of a magnetic field, the two air compressing blade wheels also move circularly around the shaft. In an alternative example, the coil is distributed on the outer edge of a vane wheel of a large air compressor of the aircraft, a neodymium magnet array is arranged at the position with the largest radius of the disc-shaped body of the aircraft, the current direction frequency corresponding to the electric energy generated by the coils in each pair of neodymium magnet arrays is exactly synchronous with that on a Gaussian electromagnetic propulsion guide rail, and when two pairs of Gaussian electromagnetic propulsion coil sets are reversely powered, the coil sets on the large air compressing vane and the small air compressing vane do reverse circular motion in the neodymium magnet guide rail ring so as to realize air compressing of the air compressing vanes. When the large compressor blade wheel rotates circumferentially, the neodymium magnet at the edge of the compressor blade wheel and the coil at the edge of the aircraft form a power generation device, and high-energy electricity is generated under the action of a magnetic field when the compressor blade wheel rotates. In an alternative example, the air compressing aircraft using the gauss electromagnetic propulsion device generates a large amount of heat when power is supplied or generated by electromagnetic coils on the air compressor blades, and the coils are just distributed on the air compressor blade wheels, so that the cooling o