Aircraft for compressing air by using Gaussian electromagnetic propulsion device

Abstract

The invention provides an aircraft using a Gaussian electromagnetic propulsion device for air compression, the center of a saucer-shaped aircraft is an olive-shaped control center, an oxyhydrogen energy storage tank and an oxyhydrogen battery device are assembled in the olive-shaped aircraft life control center, and an aircraft body provides electric energy as required through an oxyhydrogen energy storage battery; two aircraft compressor blades are annularly stacked together in a big-end-up mode, a pair of electromagnetic propulsion coil sets is distributed on the edge of each of the upper compressor blade and the lower compressor blade of the aircraft, each pair of electromagnetic propulsion coil sets corresponds to a set of annular neodymium magnet guide rail, and the two sides of each guide rail are equally divided according to the sector radian of a circle. An inner arc and an outer arc of each equally-divided radian are each provided with a neodymium magnet, the neodymium magnets and electromagnetic coils matched with the neodymium magnets form an electromagnetic propeller, an electromagnetic propelling coil set on a gas compressor blade wheel enables two gas compressor blades to rotate oppositely after being powered on reversely, and power generation coils are additionally distributed on the outer edge of the large gas compressor blade wheel. Neodymium magnets distributed in an array shape are arranged at the positions, corresponding to the coils on the large compressor blade wheel, outside the aircraft body to form a generator device, and electric energy is generated along with rotation of the large compressor blade wheel. Three exhaust ports perpendicular to the exhaust direction are formed in the bottom of an annular pipe below the gas compressor, substances treated by the high-energy ionization accelerator are exhausted out of the aircraft through the exhaust ports, an exhaust port is also formed in the side face of the aircraft, and a direction adjuster is arranged in the aircraft. The attitude and direction of the aircraft are controlled through an electric hydraulic control valve, a direction regulator and a high-energy ionization acceleration device.

Description

Technical Field

[0001] This invention provides an aircraft that uses a Gaussian electromagnetic propulsion device for compressed air, belonging to the field of manned aviation and aerospace technology. Background Technology

[0002] The inventors, building upon the existing aircraft structure based on the lever principle and air pressure dynamics, introduced a hydrogen-oxygen fuel cell to provide kinetic energy. This energy was then transferred to a Gaussian electromagnetic propulsion system, a compressor, and an ionization acceleration device, transforming the original fuel-driven compressor impeller into an electromagnetically propelled one. The aim is to replace traditional methods of reaching space, such as rocket launches. Summary of the Invention

[0003] This invention provides a spacecraft that uses a Gaussian electromagnetic propulsion device for air compression. It is a spacecraft device that organically combines a Gaussian electromagnetic propulsion device with an air pressure power device and a high-energy electric acceleration device, mainly using hydrogen-oxygen fuel cells to provide electrical power.

[0004] In one alternative embodiment, the aircraft using a Gaussian electromagnetic propulsion device for compressed air is disc-shaped. The aircraft is powered by a hydrogen-oxygen battery and specifically includes: an olive-shaped main control room, in which a hydrogen-oxygen fuel cell is installed, and hydrogen-oxygen energy storage tanks are installed around it to provide fuel for the disc-shaped aircraft. The voltage and current of the hydrogen-powered battery can be adjusted and controlled by controlling the flow rate of the exhaust port of the hydrogen-oxygen energy storage tank valves. The bottom of the olive-shaped control center of the aircraft has an entrance and exit for easy access for personnel.

[0005] In one optional embodiment, the aircraft utilizing a Gaussian electromagnetic propulsion system for air compression includes two sets of compressor blades, one larger than the other, surrounding an olive-shaped main control chamber. The compressor blades are constructed with a steel frame and lightweight, high-strength alloy blades forming a converging tube channel. A ring-shaped pipe with three outlets at the bottom communicates with the smaller compressor impeller's tube. In another optional embodiment, the aircraft utilizing a Gaussian electromagnetic propulsion system for air compression includes a pair of propulsion electromagnetic coils symmetrically mounted on the edges of the upper and lower compressor impellers. On the aircraft body, neodymium magnets are arranged in a ring on neodymium magnet rails, matching the electromagnetic propulsion coils on the upper and lower compressor impellers. The neodymium magnets on the rails are assembled according to a design where the inner and outer rails have equal arc lengths but unequal lengths, thus forming a Gaussian electromagnetic propulsion system with the electromagnetic coils. When the electromagnetic coils move in a circular motion under the influence of the magnetic field, the two compressor impellers also move in a circular motion around their axes.

[0006] In one alternative embodiment, the aircraft utilizing a Gaussian electromagnetic propulsion system for air compression features coils distributed along the outer edge of the large compressor blades. A neodymium magnet array is located at the maximum radius of the aircraft's disc-shaped body. The frequency of the current generated by the coils within each pair of neodymium magnet arrays is synchronized with the frequency of the current on the Gaussian electromagnetic propulsion rails. When two pairs of Gaussian electromagnetic propulsion coils are powered in opposite directions, the coils on the large and small compressor blades undergo counter-clockwise circular motion within the neodymium magnet rail rings, thus achieving air compression. As the large compressor blades rotate, the neodymium magnets on the edge of the compressor blades and the coils on the edge of the aircraft constitute a power generation device, generating high-energy electricity under the influence of the magnetic field when the compressor blades rotate.

[0007] In one alternative embodiment, the aircraft using a Gaussian electromagnetic propulsion device generates a large amount of heat when the electromagnetic coils on the compressor blades are supplying or generating electricity. Since these coils are distributed on the compressor blade impeller, the coils are cooled by air compression and conduction inside the compressor blades. At the same time, the lower part of the annular pipe connected to the compressor impeller constriction chamber has three exhaust ports, which are mainly responsible for controlling the direction of the aircraft. On the side of the annular pipe, there is an exhaust port with a rudder that is connected to the outer side between the upper and lower compressor blades through a pipe and controlled by an electro-hydraulic valve. The attitude and direction of the aircraft are controlled by an electro-hydraulic device.

[0008] In one alternative embodiment, the aircraft using a Gaussian electromagnetic propulsion device for compressed air is equipped with a set of hollow, high-energy plasma acceleration propulsion devices at each of its exits. These devices resemble bamboo shoots with multiple layers of outer sheaths that are about to be unearthed. Each layer of outer sheath has numerous air outlet holes at its connection point with the bamboo shoot-shaped body. Each layer of outer sheath is made of conductive metal and is connected to a high-energy power source with alternating positive and negative charges to form a plasma accelerator. The root of the bamboo shoot-shaped object is sealed and connected to the compressed air contraction pipe. The inner wall of the air outlet chamber is also covered with multiple layers of funnel-shaped conductive metal, which are connected to a high-energy power source to form a plasma accelerator. The material compressed by the compressor is accelerated and ejected through the air outlet holes by the high-energy plasma acceleration device, giving the aircraft kinetic energy.

[0009] In one alternative embodiment, the aircraft using a Gaussian electromagnetic propulsion device for compressed air is equipped with multiple microwave photonic radar transmitters and receivers at the top and bottom of the disc-shaped control center and even at fixed locations throughout the aircraft, thereby ensuring that the aircraft can avoid obstacles in a timely manner during high-speed maneuvers.

[0010] In one alternative embodiment, the aircraft utilizing a Gaussian electromagnetic propulsion system for compressed air is equipped with a switch assembly at its disc-shaped control center. This assembly allows for adjusting the electrical input to the electromagnetic propulsion rails. The switch assembly is connected to annular neodymium magnet rails, with power supplied in a circumferentially partitioned manner. This allows for adjusting the power supply coverage area of ​​the circumferential neodymium magnet rails according to the aircraft's flight requirements, enabling power supply transitions from a small, locally symmetrical section to a quarter, half, or even the entire rail area. This allows the operator to flexibly control the aircraft's start-up, hovering, rapid movement, and full-speed operation.

[0011] Those skilled in the art can conduct in-depth research and modifications on the technical details related to high-strength magnetic materials, microwave photonic radar, hydrogen-oxygen fuel cells, etc. in this invention. However, if the modifications involve using the principle of forward and reverse Gaussian electromagnetic propulsion to rotate and push the compressor blades and using this neodymium magnet structure to form a large-span generator assembly to generate high-energy electricity, and do not depart from the spirit and scope of this invention, and fall within the scope of the claims of this invention and their equivalents, then this invention also intends to include these modifications and variations.

Claims

1. This invention provides an aircraft that utilizes a Gaussian electromagnetic propulsion device for compressed air, characterized in that: At the center of the disc-shaped aircraft is an olive-shaped control center equipped with hydrogen-oxygen energy storage tanks and hydrogen-oxygen battery devices to provide power to the aircraft. Two compressor blades, one large and one small, are stacked together. An electromagnetic coil is symmetrically distributed on the edge of each of the upper and lower compressor blades. Each pair of electromagnetic coils corresponds to a set of annular neodymium magnet rails. The two sides of the rails are divided into equal arcs according to the fan-shaped arc. A set of neodymium magnets in the same direction is installed on the inner and outer arcs of each equal arc. Together with the matching electromagnetic propulsion coils, they form a Gaussian electromagnetic thruster. Coils are distributed on the outer edge of the large compressor blades. The array of neodymium magnets on the aircraft forms a high-energy power generation device, which generates electricity as the large compressor blades rotate. A high-energy electric accelerator acts on the material inside the compressor blade duct. A ring-shaped tube at the bottom of the compressor has three vertically downward exhaust ports arranged in an equilateral triangle. After passing through the high-energy accelerator, the exhaust is discharged from the aircraft. An additional exhaust port on the side of the ring-shaped tube leads to the side of the aircraft. Attitude and direction control of the aircraft are achieved through an electro-hydraulic device and an electromagnetic propulsion accelerator. An olive-shaped control center houses microwave photonic radar rangefinders at its top and bottom, as well as a switch assembly for adjusting the electrical input to the electromagnetic propulsion guide rails.

2. The aircraft according to claim 1, which combines the principles of air pressure dynamics and Gaussian electromagnetic propulsion, is characterized in that: The disc-shaped aircraft is powered by a hydrogen-oxygen battery. Specifically, it includes an olive-shaped main control room, in which a hydrogen-oxygen fuel cell is installed, and hydrogen-oxygen energy storage tanks are installed around it to provide fuel for the disc-shaped aircraft. The voltage and current of the hydrogen battery can be adjusted and controlled by regulating the flow of the exhaust port of the hydrogen-oxygen energy storage tank valve. There are entrances and exits at the bottom of the olive-shaped control center of the aircraft for easy access for personnel.

3. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The aircraft compressor impeller specifically includes two sets of compressor blades, one larger than the other, surrounding the aircraft's olive-shaped main control room. The compressor blades are constructed of a steel frame with lightweight, high-strength alloy blades forming a converging cavity channel. Connected to the cavity of the smaller compressor impeller is a ring pipe with three outlets at the bottom.

4. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The Gaussian electromagnetic propulsion system specifically includes: a pair of electromagnetic coils symmetrically mounted on the edges of the upper and lower compressor blades. On the aircraft body, neodymium magnets are arranged in a ring on guide rails, matching the electromagnetic propulsion coils on the upper and lower compressor blades. The neodymium magnets on the guide rails are assembled according to a design where the inner and outer rails have equal arc lengths but unequal arc lengths, thus forming a Gaussian electromagnetic thruster with the electromagnetic coils. When the electromagnetic coils move in a circular motion under the influence of the magnetic field, the two compressor blades also move in a circular motion around their axes.

5. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The aircraft features a built-in high-energy power generation device, specifically including: coils distributed along the outer edge of the large compressor blades; and a neodymium magnet array at the largest radius of the aircraft's disc-shaped body. The frequency of the current generated by the coils within each pair of neodymium magnet arrays is synchronized with the frequency of the current on the Gaussian electromagnetic propulsion rails. When the two Gaussian electromagnetic propulsion coils are powered in opposite directions, the coils on the two compressor blades move in opposite circular motions within the neodymium magnet rail rings, thus achieving compressor blade compression. When the large compressor blades rotate, the neodymium magnets on the edge of the compressor blades and the coils on the edge of the aircraft constitute a power generation device, generating high-energy electricity under the influence of the magnetic field when the compressor blades rotate.

6. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The compression cooling gas collection device and the aircraft exhaust port specifically include: Since the electromagnetic coils on the compressor blades generate a large amount of heat when supplying or generating electricity, the coils are cooled by the compression and conduction of air through the compressor blades. At the same time, there are three exhaust ports distributed equilaterally in the lower part of the annular tube connected to the compressor wheel constriction chamber, which are mainly responsible for controlling the direction of the aircraft's operation. On the side of the annular tube, there is an exhaust port with a rudder that is connected to the outer side between the upper and lower compressor blades through a pipe and controlled by an electro-hydraulic valve. The attitude and direction of the aircraft are controlled by an electro-hydraulic device.

7. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The high-energy plasma acceleration propulsion device specifically includes: a hollow, bamboo shoot-shaped high-energy plasma acceleration propulsion device with multiple layers of skin, resembling a bamboo shoot about to be unearthed, is installed at each of the spacecraft's exits. Each layer of skin is densely covered with exhaust pores where it connects to the bamboo shoot-shaped body. Each layer of skin is made of conductive metal and is connected to a high-energy power source in alternating positive and negative directions to form a plasma accelerator. The root of the bamboo shoot is sealed and connected to the compressed air contraction pipe. The inner wall of the exhaust chamber is also covered with multiple layers of funnel-shaped conductive metal, which are connected to a high-energy power source to form a plasma accelerator. The material compressed by the compressor is accelerated and ejected through the exhaust pores by the high-energy plasma acceleration device, giving the spacecraft kinetic energy.

8. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The microwave photonic radar specifically includes multiple microwave photonic radar transmitters and receivers installed at the top and bottom of the olive-shaped control center of the disc-shaped aircraft, as well as at fixed locations throughout the aircraft, to ensure that the aircraft can avoid obstacles in a timely manner when maneuvering at high speeds.

9. The aircraft using a Gaussian electromagnetic propulsion device for compressed air as described in claim 1, characterized in that: The adjustable electromagnetic propulsion rail power input switching assembly specifically includes a circumferential neodymium magnet rail with power supplied in a circumferentially partitioned manner. The power supply coverage area of ​​the circumferential neodymium magnet rail is adjusted according to the needs of the aircraft's flight status, thereby realizing the power supply change from a small symmetrical local area to a quarter of the symmetrical area, to a half of the symmetrical area, and even the entire rail area. This enables the administrator to flexibly control the aircraft's start-up, hovering, rapid movement, and full-speed movement.