Coil weight reduction device realized by spark gap discharge
By setting up a spark gap discharge system in the coil of the experimental device, a high -frequency pulse magnetic field is generated, and the problem of unable to achieve gravity interference and weight loss in the device itself is solved. And have the potential to transport long -distance transportation.
Patent Information
- Application Number
- CN202411844187.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-15
- Publication Date
- 2025-01-21
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
The prior art cannot achieve the interference and weight reduction effect of the gravity field in the experimental device itself, resulting in the inability to build a device that can achieve weight reduction in the entire system in the laboratory.
Design a coil weight loss device implemented by spark gap discharge. The power supply is set up in the coil, the DC high -voltage generator, the high -voltage capacitor, and the spark gap switch to generate high -frequency pulse magnetic fields, interfere with the gravity field, and realize the weight of the device itself.
It has achieved not only reduction of the weight of objects in the center of the device, but also expanded the scope of the impact of interference gravity fields, so that the system itself also benefits the weight loss effect and has the potential of long -distance transportation.
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Figure CN119339605A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the experimental field of gravity research, and in particular to a coil weight reduction device realized by spark gap discharge. Background Art
[0002] Gravity is everywhere. All massive celestial bodies, including the Earth, have gravity. People have been studying gravity-related technologies for many years and have indeed produced certain results. The patent with announcement number CN201310186964.5 discloses an experimental device for interfering with the gravity field, which interferes with the gravity field in the central area of the device through a magnetic field. There is also a patent with announcement number CN201310186996.5, which also discloses a ring-type gravity field interference device, which interferes with the gravity field in a certain area above the device through a magnetic field. The above patents can interfere with the gravity field through a magnetic field to reduce the weight of objects in the vicinity of the device, but the existing technology only interferes with the gravity field outside the device to reduce the weight of objects outside the system. The interfered gravity field has no effect on the system itself, so that the system itself will not produce a weight loss phenomenon. Therefore, humans have not yet built a set of devices for interfering with the gravity field in the laboratory to reduce the weight of the entire system. Summary of the invention
[0003] In order to solve the above-mentioned problems, the present invention constructs a weight reduction device, whose structure is to first use a coil to wind a hollow shell container. The shape of the container is arbitrary, and it can be a hollow sphere, a hollow discus, or a hollow cylinder. The purpose is that the magnetic field generated by the coil after power is turned on will tightly wrap the cavity, thereby achieving a substantial weight reduction inside.
[0004] In order to increase the ability to generate a magnetic field, the coil can also be wound around a magnetic conductive material having a cavity structure to form a cavity-shaped shell coil container.
[0005] At the same time, the electrical part of the present invention that supplies power to the coil can be arranged outside the shell-shaped coil, but in order to achieve a better weight reduction effect of the electrical part, the present invention places the electrical part in the cavity container of the weight reduction device so that it is wrapped by the coil.
[0006] At the same time, the electrical part of the present invention is mainly composed of a power supply, a DC high-voltage generator, a high-voltage capacitor and a spark gap switch. In order to make the present invention more effective in reducing weight, the spark gap switch in the present invention is designed to be filled with a certain amount of inert gas, mercury vapor or air in a closed vacuum container, and two high-temperature resistant electrodes are provided, and the distance between the two electrodes can be adjusted between 0.1 mm and 1000 mm. When the voltage of the capacitor reaches a certain high voltage, a breakdown phenomenon will be formed between the two electrodes, and the gas enclosed therein will be ionized, causing the resistivity of the gas to decrease until the charge release in the capacitor ends, and the voltage is not enough to maintain the breakdown condition between the two electrodes, thereby stopping the breakdown and stopping the ionization of the enclosed gas, and constructing a pulse cycle. The present invention has found through experiments that the distance between the spark gaps can control the pulse frequency of the switch, and the higher the frequency and the greater the voltage, the better the weight reduction effect. The present invention recommends that the adjustment frequency should preferably exceed 10Mhz.
[0007] The present invention has the following beneficial effects: The present invention can not only interfere with the gravity field to reduce the weight of objects in the central area of the device, but also change the regional range of the interference gravity field, achieve the amplification of the influence range of the interference gravity field, and have an impact on the system itself. This has never happened before the disclosure of the present invention. This change is huge for the existing field of gravity research. This change also represents the final result of this type of experiment. It is no longer a weight reduction in a target area, but a weight reduction of the system itself and a larger area around it. Then the beneficial effects of the present invention are no longer limited to simulating the weak gravity environment in space within a certain area, but the system that interferes with the gravity field is turned into a carrier, thereby realizing the long-distance transportation function of goods and personnel. BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Figure 1 Schematic diagram of coil weight reduction devices of various shapes Figure 2 Electrical Part Structure Diagram Figure 3 Spark gap switch schematic Figure 4 Magnetic field diagram of the coil Description of the numbers in the figure: 1. Hollow spherical coil 2. Hollow discus coil 3. Hollow cylindrical coil 4. Power supply 5. DC high voltage generator 6. High voltage capacitor 7. Spark gap switch 8. Various coils of the present invention 9. Electrode plate 10. Screw 11. Coil magnetic field 12. Vacuum container 13. Inert gas or mercury vapor or air Implementation
[0009] like Figure 1The schematic diagram of the coil weight reduction device of the present invention shows that the structure of the coil weight reduction device of the present invention is a coil wound by a thin wire, forming a cavity-shaped shell structure, and its shape is arbitrary. As shown in the figure, it can be wound into a hollow spherical coil (1), a hollow discus-shaped coil (2), a hollow cylindrical coil (3), etc. In order to increase the magnetic field strength, the coil of the present invention can also be wound on a cavity-shaped magnetic conductive material such as silicon steel or ferrite to produce a stronger magnetic field effect.
[0010] like Figure 2 The electrical structure diagram of the present invention is shown in which a power source (4), a DC high voltage generator (5), a high voltage capacitor (6) and a spark gap switch (7) are arranged inside the cavity of the coil weight reduction device. The current output by the power source of the present invention is passed into the high voltage generator (5) to generate DC high voltage electricity, which is then input into the high voltage capacitor (6) for accumulation. The high voltage capacitor (6) is connected in series with the spark gap switch (7) and is further connected to the coil (8) of the present invention.
[0011] like Figure 3 The present invention is a schematic diagram of a spark gap switch (7), which has a structure in which two parallel electrode plates (9) are arranged in a closed vacuum container (12). The vacuum container (12) is also filled with a certain amount of inert gas (13) or mercury vapor (13), or even air (13). The purpose is that when the voltage of the high-voltage capacitor (6) accumulates to a certain height, the two electrode plates (9) will be broken down to form a closed circuit. At the same time, the breakdown also causes the gas (13) enclosed therein to produce ionization, so that the plasma of the ionized gas can achieve a decrease in the resistance between the two electrodes, thereby achieving the switch (7) continuing to conduct when the charge in the capacitor (6) is reduced and becomes low voltage, and finally achieving the complete release of the charge in the capacitor (6) to complete a pulse cycle. This process is completed instantaneously. The present invention spark gap switch (7) will continue this cycle. The other two plates (9) are fixed on the screws (10). The distance between the two plates can be easily adjusted by rotating the screws. The distance range is between 0.1 mm and 1000 mm, so as to facilitate the control of the switching frequency. The present invention has found through experiments that the higher the voltage between the two electrodes, the smaller the gap, and the faster the frequency, the more obvious the weight reduction effect.
[0012] like Figure 4 , is the coil magnetic field diagram of the present invention. When the above-mentioned electric energy is passed through the coil, the coil will generate a pulse magnetic field (11). This magnetic field constitutes a closed magnetic field environment, which can shield the external gravitational field and achieve the weight reduction phenomenon of the entire device.
[0013] In addition, since the present invention adopts a high-voltage arc form, it will generate a high-voltage electric field and affect the reading of the electronic scale. Therefore, in order to more effectively verify the weight loss effect, the present invention recommends the use of a mechanical scale to place the entire coil weight loss device on the tray of the mechanical scale to facilitate more rigorous weight loss data.
[0014] The above description is only a preferred embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification under the principle and concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.
Claims
1. A coil weight reduction device implemented by spark gap discharge, characterized in that: The coil weight reduction device of the present invention adopts a multi-turn coil (8) to be wound into a cavity-shaped shell container, and the electrical part of the present invention is installed in the cavity container. The structure includes a power supply (4), a DC high-voltage generator (5), a high-voltage capacitor (6), and a spark gap switch (7) with a closed structure and filled with a certain gas. The switch allows the electric energy accumulated in the high-voltage capacitor (6) to be released to the end of the shell coil (8), forming a magnetic field (11) that wraps the entire weight reduction device and produces a weight reduction phenomenon.
2. A coil weight reduction device implemented by spark gap discharge according to patent claim 1, characterized in that: the weight reduction device uses a multi-turn coil (8) to be wound into a cavity-shaped shell container, such as a hollow spherical coil (1), a hollow discus-shaped coil (2), a hollow cylindrical coil (3), etc. In order to increase the magnetic field strength, the coil of the present invention can also be wound on a cavity-shaped magnetic conductive material such as silicon steel or ferrite to produce a stronger magnetic field effect.
3. A coil weight reduction device realized by spark gap discharge according to patent claim 1, characterized in that: the electrical part of the present invention can be arranged outside the coil, but in order to achieve a better weight reduction effect of the electrical part, the present invention arranges it in the cavity wound by the coil and is tightly wrapped by the magnetic field (11) generated by the coil.
4. A coil weight reduction device realized by spark gap discharge according to patent claim 1, characterized in that: the electrical part is provided with a power supply (4) and a DC high voltage generator (5), and the generated high voltage is stored and accumulated by a high voltage capacitor (6).
5. A coil weight reduction device realized by spark gap discharge according to patent claim 1, characterized in that: a spark gap switch (7) is connected in series between the coil (8) and the high-voltage capacitor (6), and the electricity supplied to the coil must pass through the spark gap switch (7).
6. A coil weight reduction device realized by spark gap discharge according to patent claim 1, characterized in that the voltage accumulated by the high-voltage capacitor (6) is released to the coil end by ionizing inert gas (13), mercury vapor (13) or ionized air (13).
7. A coil weight reduction device realized by spark gap discharge according to patent claim 1, characterized in that: the two electrode plates (9) in the spark gap switch are enclosed in a vacuum container (12), and a certain amount of inert gas or mercury vapor or air (13) is also filled in the container. The characteristic of the gas is that after being ionized, it becomes plasma, and its resistance will drop rapidly, so that when the charge in the capacitor decreases and the voltage becomes low, the circuit is turned on as usual until the charge of the capacitor (6) is completely released, thereby completing a pulse discharge.
8. A coil weight reduction device implemented by spark gap discharge according to patent claim 1, characterized in that: the distance between the two electrode plates (9) of the spark gap switch can be adjusted by a screw (10), and the distance is between 0.1 mm and 1000 mm, which is convenient for controlling the voltage and frequency output to the coil (8) end.
9. The coil weight reduction device realized by spark gap discharge according to patent claim 1 is characterized in that: the present invention tries to use high power, high voltage and small gap to match the discharge, which is convenient for increasing the discharge frequency. The higher the frequency, the better the weight reduction effect. The discharge frequency is preferably greater than 10Mhz.
10. A coil weight reduction device implemented by spark gap discharge according to patent claim 1, characterized in that: the magnetic field (11) generated by the coil wraps around the entire weight reduction device.
Citation Information
Patent Citations
Interfered gravity field experiment device
CN103226908A
Ring type gravitational field interfering device
CN103247206B