A pure electric fluid-free spacecraft

Abstract

A pure electric, fluid-free spacecraft comprises a positive electrode disc, a battery, a accumulator ball, a high-voltage transformer, and a current collecting device. The accumulator ball and the positive electrode disc are both made of metal. A housing is connected between the positive electrode disc and the accumulator ball, and the housing is made of insulating material. The outer diameter of the positive electrode disc is more than twice the outer diameter of the accumulator ball, and the positive electrode disc and the accumulator ball form a pair of asymmetric electrodes. The battery is connected to the input end of the high-voltage transformer, and the positive electrode of the high-voltage transformer is connected to the positive electrode disc via a wire. The negative electrode of the high-voltage transformer output transmits negative charge to the current collecting device, which is connected to the accumulator ball and accumulates the negative charge on the accumulator ball. After the present invention begins operation, the negative charge ionized by the high-voltage transformer is continuously transported to the accumulator ball through the current collecting device and accumulated, generating a voltage difference of over one million volts between the positive electrode disc and the accumulator ball. This achieves the goal of generating a high voltage difference using an internal battery, without the need for an external high-voltage power supply. This relates to the field of aircraft technology.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft, and in particular to a pure electric fluid-free aerospace aircraft. Background Art

[0002] The Biefeld-Brown effect refers to the phenomenon in which a high voltage applied to an asymmetric electrode structure generates a force that tends to move the device. Current applications of this effect are similar to "hoist" devices, where asymmetric capacitor structures are placed side by side. The thrust generated is aligned with gravity and directed from the negative electrode to the positive electrode. However, a higher voltage is required to achieve a significant thrust.

[0003] In the book "Secrets of Antigravity Propulsion" (ISBN-13: 978-1591430780) written by Paul Laviolette, Brown invented a 15-inch diameter, dome-shaped dish in the 1960s while conducting electrogravity experiments. The dish automatically lifted when a voltage of 50 kilovolts was applied, and it remained stable at lower voltages. Brown later improved the device, designing a three-arc ballistic electrode as the anode, a smaller electrode below as the cathode, and a larger electrode made of an umbrella-shaped frame covered in aluminum foil. A thin glass strut insulator was attached to the cathode. Brown claimed the device could generate a lift of 125% of its own weight at a voltage of 170 kilovolts.

[0004] As a flying device, the above-mentioned device has the advantages of simple structure, no need to consume fuel and gas resources, and no bearings, blades or moving parts compared to traditional flying devices. However, this type of device requires an external high-voltage power supply to drive it. Currently, the power supply of this type of device is independent and requires an external high-voltage tower to provide negative high voltage. The cable of the external power supply will limit the range of movement of the aircraft, which is very inconvenient for the aircraft. Summary of the Invention

[0005] In view of the technical problems existing in the prior art, the purpose of the present invention is to provide a pure electric fluid-free aerospace vehicle that does not require an external high-voltage power supply.

[0006] In order to achieve the above-mentioned purpose, the present invention adopts the following technical solution: a pure electric fluid-free spacecraft, including a positive electrode disc, a battery, a storage ball, a high-voltage transformer and a collector device, the storage ball and the positive electrode disc are both made of metal materials, and a shell is connected between the positive electrode disc and the storage ball, and the shell is made of insulating material. The outer diameter of the positive electrode disc is more than twice the outer diameter of the storage ball, and the positive electrode disc and the storage ball constitute a pair of asymmetric electrodes; the battery is connected to the input end of the high-voltage transformer, the positive electrode of the output end of the high-voltage transformer is connected to the positive electrode disc through a wire, and the negative electrode of the output end of the high-voltage transformer transmits negative charge to the collector device, and the collector device is connected to the storage ball and accumulates the negative charge on the storage ball.

[0007] With this structure, once the device begins operation, the negative charge generated by the high-voltage coil is continuously transported to the accumulator sphere via a current collector, where it accumulates. This generates a voltage difference of over a million volts between the positive disc and the accumulator sphere, enabling the internal battery to generate this high voltage difference without the need for an external high-voltage power supply. Furthermore, the device uses an insulated casing to connect the positive disc and accumulator sphere, reducing the risk of breakdown in a vacuum and better utilizing the high thrust generated by the Biefeld-Brown effect at high voltage.

[0008] As a preferred embodiment, the storage ball is located below the positive electrode disc, the upper end of the shell is fixedly connected to the positive electrode disc, and the lower end of the shell is fixedly connected to the storage ball.

[0009] As a preferred embodiment, the shell has a hollow structure with openings at the upper and lower ends respectively. The positive electrode disc is sealed to the upper end of the shell, and the storage ball is sealed to the lower end of the shell, thereby forming a closed cavity inside the shell. The cavity is filled with air, and the battery and the high-voltage package are both located in the upper part of the cavity.

[0010] As a preferred embodiment, the current collecting device includes an electric motor, a first pulley, a second pulley, a rubber belt and a current collecting comb. The electric motor is connected to the first pulley and drives the first pulley to rotate. The rubber belt is connected end to end and passes around the first pulley and the second pulley. The negative pole of the output end of the high-voltage transformer is connected to a discharge tip, the discharge tip faces the rubber belt and sprays negative charge on the rubber belt. The current collecting comb contacts the surface of the rubber belt. The current collecting comb is connected to the storage ball through a bracket. The current collecting comb and the bracket are both made of metal materials.

[0011] As a preferred embodiment, the interior of the storage ball is hollow, and the second pulley and the current collecting comb are both installed in the storage ball.

[0012] As a preferred embodiment, the bracket includes a support member, a screw and a moving block. The support member is located inside the storage ball and is fixedly connected to the inner wall of the storage ball. A threaded hole is opened on the support member, and the screw is threadedly connected to the support member through the threaded hole. The screw is rotated to connect to the moving block. The screw is also provided with a nut for locking the moving block; the second pulley is rotatably mounted on the moving block, so that when the screw rotates, the second pulley is driven to move through the moving block.

[0013] As a preferred embodiment, the first pulley is installed on the upper part of the cavity and is located directly above the second pulley, and the screw is arranged vertically; there are two brackets, and the two brackets are symmetrically arranged. The center of the second pulley is connected to a rotating shaft, and the two ends of the rotating shaft are rotatably installed on the two moving blocks respectively; the current collecting comb is U-shaped, and the two ends of the current collecting comb are installed on the moving blocks by screws.

[0014] As a preferred embodiment, the storage ball is composed of two hemispherical structures.

[0015] As a preferred embodiment, the positive electrode disc is mushroom-shaped, and the central axis of the positive electrode disc passes through the center of the storage ball.

[0016] As a preference, the battery is a lithium battery.

[0017] The principle of the present invention is as follows: a lithium battery is used to power a high-voltage package and an electric motor. The high-voltage package generates a high voltage of nearly 30,000 volts and ejects negative charges through tip discharge and attaches them to the rubber belt. The motor drives the first pulley to rotate, thereby driving the rubber belt to move. The rubber belt carries negative charges to the collector comb, which then transfers the charges to the storage ball. The metal ball shell can store a large amount of negative charges, giving its surface a negative high potential of over one million volts. The positive charges ionized by the high-voltage package are transferred to the positive electrode disc. Ultimately, the storage ball forms a high potential difference with the positive electrode disc under continuous charge accumulation, thus forming a nonlinear gradient electric field between the two. According to the Befeld-Brown effect, this device generates thrust from the negative electrode to the positive electrode, causing the aircraft to move toward the positive electrode disc in space.

[0018] In summary, the present invention offers the following advantages: Compared to conventional aircraft utilizing the Befeld-Brown effect, the present invention's purely electric, fluid-free spacecraft splits its high-voltage power supply into two components. One component is a miniaturized ion generator powered by a lithium battery. A high-voltage transformer inverts 24 volts to tens of thousands of volts for air ionization. The other component is a current collector utilizing the principle of a generator. A rubber belt transports negative charges to a storage sphere. The metal shell can store a large amount of negative charge, resulting in a high negative potential of millions of volts on its surface. Because these components are all integrated internally, they eliminate the constraints of an external power source, making them safe, reliable, convenient, and flexible to use. Furthermore, the present invention's purely electric, fluid-free spacecraft boasts low power consumption, requiring only lithium batteries for power. There is no voltage loss during operation. While reaching high voltages exceeding millions of volts, the current draw is limited to microamperes, resulting in a superior thrust-to-power ratio compared to existing Hall effect propulsion technology. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a front view of a pure electric fluid-free spacecraft.

[0020] Figure 2 A three-dimensional view of a purely electric, fluid-free spacecraft.

[0021] Figure 3 This is a schematic diagram of the internal structure of a pure electric fluid-free spacecraft.

[0022] Figure 4 Schematic diagram of the structure of the battery, high-voltage package and collector device.

[0023] Figure 5 This is a schematic structural diagram of the battery, high-voltage package and current collector from another angle.

[0024] Among them, 1 is the positive electrode disc, 2 is the battery, 3 is the storage ball, 4 is the high-voltage package, 5 is the current collecting device, and 6 is the shell.

[0025] 501 is the motor, 502 is the first pulley, 503 is the rubber belt, 504 is the second pulley, 505 is the current collecting comb, 506 is the support member, and 507 is the moving block. DETAILED DESCRIPTION

[0026] The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0027] Example 1

[0028] like Figures 1 to 5 As shown, a pure electric fluid-free spacecraft includes a positive electrode disc, a battery, a storage ball, a high-voltage transformer and a collector. The storage ball and the positive electrode disc are both made of metal materials. A shell is connected between the positive electrode disc and the storage ball. The shell is made of insulating material. The outer diameter of the positive electrode disc is more than twice the outer diameter of the storage ball. The positive electrode disc and the storage ball form a pair of asymmetric electrodes; the battery is connected to the input end of the high-voltage transformer, the positive electrode of the output end of the high-voltage transformer is connected to the positive electrode disc through a wire, and the negative electrode of the output end of the high-voltage transformer transmits negative charge to the collector. The collector is connected to the storage ball and accumulates the negative charge on the storage ball.

[0029] The storage ball is located below the positive electrode disc, the upper end of the shell is fixedly connected to the positive electrode disc, and the lower end of the shell is fixedly connected to the storage ball.

[0030] The shell is a hollow structure with openings at the upper and lower ends. The positive electrode disc is sealed to the upper end of the shell, and the storage ball is sealed to the lower end of the shell, thereby forming a closed cavity inside the shell. The cavity is filled with air, and the battery and high-voltage package are both located in the upper part of the cavity.

[0031] The entire pure electric fluid-free spacecraft can be used in a vacuum environment. The cavity is filled with air at a certain pressure so that the high-voltage package can ionize the air to obtain positive and negative charges. In the process of generating a high voltage difference as a whole, there is almost no leakage loss at various positions of the device. Moreover, since the aircraft is driven by the Biefeld-Brown effect, although the voltage of the entire aircraft is high, the current is very small. Therefore, the power of the aircraft is low and the propulsion efficiency is high.

[0032] The current collecting device includes an electric motor, a first pulley, a second pulley, a rubber belt and a current collecting comb. The electric motor is connected to the first pulley and drives the first pulley to rotate. The rubber belt is connected end to end and passes around the first pulley and the second pulley. The negative pole of the output end of the high-voltage transformer is connected to the discharge tip, which faces the rubber belt and sprays negative charge on the rubber belt. The current collecting comb contacts the surface of the rubber belt. The current collecting comb is connected to the storage ball through a bracket. The current collecting comb and the bracket are both made of metal materials.

[0033] The high-voltage package can adopt an existing high-voltage package, and the negative pole of its output end has a needle-shaped discharge tip. The negative charge ejected by the discharge tip adheres to the surface of the rubber belt and is transferred to the collecting comb, and then accumulated through the bracket and transferred to the storage ball.

[0034] The motor and the first pulley are both located at the upper part of the cavity.

[0035] The electric motor, high-voltage package and battery are installed and positioned respectively through clamps and positioning blocks, and the positioning blocks and clamps are made of stainless steel.

[0036] The interior of the electricity storage ball is hollow, and the second pulley and the electricity collecting comb are both installed in the electricity storage ball. The upper end of the electricity storage ball is open and sealed to the lower end of the shell.

[0037] The bracket includes a support member, a screw, and a moving block. The support member is located inside the battery ball and fixedly connected to the inner wall of the battery ball. The support member has a threaded hole, through which the screw is threadedly connected to the support member. The screw rotates to connect to the moving block. The screw is also covered with a nut for locking the moving block. The second pulley is rotatably mounted on the moving block. When the screw rotates, the second pulley moves through the moving block. As the screw rotates, the vertical position of the second pulley can be adjusted, thereby adjusting the tightness of the rubber belt.

[0038] The first pulley is installed on the upper part of the cavity and is located directly above the second pulley, and the screw is arranged vertically; there are two brackets, which are symmetrically arranged. The center of the second pulley is connected to a rotating shaft, and the two ends of the rotating shaft are rotatably installed on the two moving blocks respectively; the collecting comb is U-shaped, and the two ends of the collecting comb are installed on the moving blocks by screws.

[0039] The support member is L-shaped.

[0040] The battery ball is composed of two hemispherical structures. The two hemispherical structures are arranged one above the other. When making it, you can first install the upper hemispherical structure, then install the bracket, second pulley and current collecting comb inside the upper hemispherical structure, and then put the two hemispherical structures together.

[0041] The positive electrode disc is mushroom-shaped, and the central axis of the positive electrode disc passes through the center of the storage ball.

[0042] The positive electrode disc consists of a middle disc segment and an outer ring segment. The outer ring segment connects to the outer edge of the middle disc segment. The cross-sectional profile of the middle disc segment is a normal curve. The inner edge of the outer ring segment is smoothly connected to the outer edge of the middle disc segment. From the inner edge to the outer edge, the outer ring segment bends and extends outward and downward.

[0043] The battery is a lithium battery.

[0044] The above embodiments are preferred implementations of the invention, but the implementation of the present invention is not limited to the above embodiments. Any other changes, modifications, substitutions, combinations, and simplifications that do not deviate from the spirit and principles of the present invention should be considered equivalent replacement methods and are included in the scope of protection of the present invention.

Claims

1. A pure electric fluid-free aerospace vehicle, characterized by: The device comprises a positive electrode disc, a battery, a storage ball, a high-voltage transformer, and a current collector. The storage ball and the positive electrode disc are both made of metal. A shell is connected between the positive electrode disc and the storage ball, and the shell is made of insulating material. The outer diameter of the positive electrode disc is more than twice the outer diameter of the storage ball. The positive electrode disc and the storage ball form a pair of asymmetric electrodes. The battery is connected to the input end of the high-voltage package, and the positive pole of the output end of the high-voltage package is connected to the positive disc through a wire. The negative pole of the output end of the high-voltage package transmits negative charge to the collector, which is connected to the storage ball and accumulates the negative charge on the storage ball. The shell is a hollow structure with openings at the upper and lower ends. The positive electrode disc is sealed to the upper end of the shell, and the storage ball is sealed to the lower end of the shell, thereby forming a closed cavity inside the shell. The cavity is filled with air, and the battery and high-voltage package are both located in the upper part of the cavity. The current collecting device includes a motor, a first pulley, a second pulley, a rubber belt and a current collecting comb. The motor is connected to the first pulley and drives the first pulley to rotate. The rubber belt is connected end to end and passes around the first pulley and the second pulley. The negative pole of the output end of the high-voltage transformer is connected to a discharge tip, which points toward the rubber belt and sprays negative charges onto the rubber belt. The collecting comb contacts the surface of the rubber belt and is connected to the storage ball through a bracket. Both the collecting comb and the bracket are made of metal materials. The interior of the electricity storage ball is hollow, and the second pulley and the electricity collecting comb are both installed in the electricity storage ball.

2. A pure electric fluid-free spacecraft according to claim 1, characterized in that: The storage ball is located below the positive electrode disc, the upper end of the shell is fixedly connected to the positive electrode disc, and the lower end of the shell is fixedly connected to the storage ball.

3. A pure electric fluid-free spacecraft according to claim 1, characterized in that: The bracket includes a support member, a screw and a moving block. The support member is located inside the storage ball and is fixedly connected to the inner wall of the storage ball. A threaded hole is opened on the support member. The screw is threadedly connected to the support member through the threaded hole. The screw is rotated to connect to the moving block. A nut is also sleeved on the screw for locking the moving block. The second pulley is rotatably mounted on the moving block, so that when the screw rotates, the second pulley is driven to move through the moving block.

4. A purely electric, fluid-free spacecraft according to claim 3, characterized in that: The first pulley is installed at the upper part of the cavity and is located directly above the second pulley, and the screw is vertically arranged; There are two brackets, which are symmetrically arranged. The center of the second pulley is connected to a rotating shaft, and both ends of the rotating shaft are rotatably mounted on the two moving blocks. The current collecting comb is U-shaped, and both ends of the current collecting comb are mounted on the moving block by screws.

5. The pure electric fluid-free spacecraft according to claim 1, characterized in that: The battery ball is composed of two hemisphere structures.

6. A pure electric propellant-free spacecraft according to claim 2, characterized in that: The positive electrode disc is mushroom-shaped, and the central axis of the positive electrode disc passes through the center of the storage ball.

7. The pure electric fluid-free spacecraft according to claim 1, characterized in that: The battery is a lithium battery.

Images