JP3237079U - Flying car - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a so-called flying car which is a vehicle or a drone capable of flying in the sky. An electromagnetic propulsion unit 102 is provided at a plurality of locations of an airframe unit 101, and includes an asymmetric high-voltage capacitor that operates based on the Biefeld-Brown effect. A propulsive force is generated from the electrode surface of 1 toward the second electrode surface having a smaller size. The power generation unit 103 is provided in the machine body unit 101, and in each of the plurality of electromagnetic propulsion units 102, the positive charge electric power supplied to the first electrode surface and the negative charge supplied to the second electrode surface are provided. Generates electricity. The flight control unit 104 is provided in the body unit 101, and controls the amount of positive charge power and negative charge power supplied from the power generation unit 103 to the plurality of electromagnetic propulsion units 102, respectively, to control the direction of flight. Control altitude and speed. [Selection diagram] Fig. 1

Description

The present invention relates to a so-called flying car, which is a vehicle or drone that can fly in the sky.

Unmanned drones have become widespread in various industrial fields, and moreover, vehicles that allow humans to ride and fly in the sky, just like automobiles run on land, are being realized. Hereinafter, these will be collectively referred to as "flying cars".

Traditionally, aviation technology for flying has been based on engines and rockets.

Traditional engine and rocket-based aviation technology requires fossil fuels and has very high fuel costs. In addition, noise and vibration are also large.

Aircraft and drones equipped with motors instead of engines have also appeared, but noise and vibration cannot be completely suppressed due to the mechanical drive parts such as the motor body and propellers.

In addition, nuclear engines and hydrogen engines are not suitable for flying cars that require miniaturization.

All of the above-mentioned conventional techniques for flying cars are equipped with a propeller, a rotor, or a duct phone driven by an engine or a motor (for example, Patent Document 1), and cannot escape from some noise or vibration, and fly unmanned. In the case of a car, noise damage to the area around the flight course is unavoidable, and in the case of a manned flying car, there is a problem that more comfortable boarding is hindered.

Japanese Patent No. 6567652

Therefore, the present invention aims to realize a quiet and comfortable flying car by adopting a new drive system that does not require a mechanical drive part.

An example of an embodiment of a flying vehicle is an aircraft configured to carry a payload that does not include an occupant or contains one or more occupants, and has an airframe that has a structure that supports the total body weight together with the payload. It includes an asymmetric high-voltage capacitor that is provided at multiple locations in the section and operates based on the Beefeld-Brown effect. A plurality of electromagnetic propulsion units that generate propulsive force directed toward the electrode surface of the above, and positively charged electric power supplied to the first electrode surface in each of the plurality of electromagnetic propulsion units provided in the machine body. , A power generation unit that generates negative charge power supplied to the second electrode surface, and a positive charge power and negative charge that are provided in the machine body and are supplied from the power generation unit to a plurality of electromagnetic propulsion units, respectively. It includes a flight control unit that controls the direction, altitude, and speed of flight by controlling the amount of electric power.

According to the present invention, it is possible to realize a quiet and comfortable flying car by adopting a new drive system that does not require a mechanical drive part.

It is a block diagram of the flying car in embodiment of this invention. It is a principle sectional view of the electromagnetic propulsion part in embodiment of this invention.

Hereinafter, a mode for carrying out the present invention (hereinafter referred to as “the present embodiment”) will be described. FIG. 1 is a block diagram of a flying car 100 according to an embodiment of the present invention.

In FIG. 1, the flying vehicle 100 is an aircraft configured to carry a payload that does not include a occupant or contains one or more occupants. The size of a flying car is not a large one like a passenger plane, but an unmanned vehicle, or a small drone (unmanned aerial vehicle) or a passenger car that can accommodate one or several passengers.

The airframe section 101 has a structure that supports the total airframe weight together with the payload.

Each of the plurality of points at the bottom of the machine body 101, for example, the four circular holes shown in the figure, is provided with four electromagnetic propulsion parts 102, for example, # 1 to # 4, toward the lower side of the machine part 101. Will be done. An electromagnetic propulsion unit 102 (not shown) for propulsion may be provided at the rear portion of the airframe unit 101 in the propulsion direction.

FIG. 2 is a cross-sectional view of the principle common to each of the electromagnetic propulsion units 102 of # 1 to # 4 when viewed from the direction A of FIG. The electromagnetic propulsion unit 102 includes an asymmetric high voltage capacitor 200 that operates based on the Biefeld-Brown effect. That is, the high voltage capacitor 200 has an asymmetric structure in which the first electrode surface 201 having a large size and the second electrode surface 202 having a small size are opposed to each other by the insulator 206. Then, a controlled amount of positively charged electric power is supplied to the first electrode surface 201 from the electric power generation unit 103 of FIG. 1, which will be described later, via the flight control unit 104. Further, a controlled amount of negatively charged electric power is supplied to the second electrode surface 202 from the electric power generation unit 103 via the flight control unit 104. As a result, in the high voltage capacitor 200, the electromagnetic propulsion unit 102 is directed from the first electrode surface 201 having a larger size to the second electrode surface 202 having a smaller size due to the Biefeld-Brown effect. Generates propulsion force 207. At the same time, an atmospheric flow shown as a broken line 208 in FIG. 2 is generated at the lower part of the second electrode surface 202 of the electromagnetic propulsion unit 102.

The first electrode surface 201 includes, for example, a pancake structure made of a thin film sheet of a nano-level multilayer composite material for supplying positively charged electric power from the electric power generating unit 103 of FIG. 1 via the flight control unit 104. preferable. As a result, the surface area of the first electrode surface 201 can be maximized at the micro level, and the required propulsive force 207 can be obtained.

The second electrode surface 202 preferably has, for example, a multi-layer grid mesh structure for supplying negatively charged electric power from the electric power generating unit 103 of FIG. 1 via the flight control unit 104. The total surface area is smaller than that of the first electrode surface 201. Due to the asymmetry of the surface areas of the first electrode surface 201 and the second electrode surface 202 and the mesh structure on the second electrode surface 202, the structure of the electromagnetic field is distorted, and the first electrode surface 201 to the first electrode surface 201 to the first. It is possible to generate an effective propulsion force 207 toward the electrode surface 202 of 2.

The inside of the high voltage capacitor 200 is preferably a closed chamber filled with the inert gas 205 having a large dielectric resistance, for example. The closed chamber makes it possible to protect the electronic device of the flight control unit 104, which will be described later, and the occupant of the flying car 100 from the high voltage field.

Various technical documents such as those exemplified below are known as practical techniques for asymmetric high-voltage capacitors that operate based on the Biefeld-Brown effect.

For example, US Pat. No. 4,1974,483, published September 1934, relates to a technique for producing force or motion by applying and maintaining a high potential static charge within a system of chargeable mass and associated electrodes. Is.

U.S. Pat. No. 2,949,550, published August 1960, relates to an electrokinetic device that realizes an electric potential for the generation of forces that generate relative motion between a structure and a surrounding medium.

U.S. Pat. No. 3,120,363, issued February 1964, relates to heavy aircraft equipment and propulsion / control technology using ion discharge.

U.S. Pat. No. 6,317,310, issued November 2001, relates to a high potential charged two-dimensional asymmetric capacitor for generating thrust.

The use of non-ionic air particles across the wing to cause ascent is seen in US Pat. No. 2,876,965, issued March 1959. This patent relates to a circular wing aircraft capable of vertical and horizontal flight using the radial cross section of the wing as a valid wing.

Japanese Patent Laid-Open No. 2008-516124, published in May 2008, relates to a technique for generating a practical starting force and other forces by introducing a plasma environment into an asymmetric capacitor.

As the electromagnetic propulsion unit 102 in the present embodiment, it is preferable to adopt the patent-related technology described in various technical documents exemplified above, which is suitable for the flying car 100. Of course, other techniques other than those described above based on the Biefeld-Brown effect may be adopted.

Returning to the description of FIG. 1, the power generation unit 103 is provided in the machine body unit 101, and is, for example, the positively charged electric power supplied to the first electrode surface 201 in each of the electromagnetic propulsion units 102 of # 1 to # 4. , Generates negatively charged power supplied to the second electrode surface 202.

The operating voltage generated by the power generating unit 103 is preferably in the range of 300,000 to 1,500,000 volts.

The power generation unit 103 is preferably a lithium ion battery, for example. Further, the power generation unit 103 preferably includes a solar panel battery for charging the lithium ion battery.

The power generation unit 103 is preferably a cold fusion power generation device. As a result, the flying car 100 in the present embodiment can fly at high speed for a long time.

In FIG. 1, the flight control unit 104 is provided in the body unit 101, and controls the amount of positive charge power and negative charge power supplied from the power generation unit 103 to the plurality of electromagnetic propulsion units 102, respectively. Control the direction, altitude, and speed of flight. The flight control unit 104 can be easily realized, for example, by diverting a known control technique established among those skilled in the art as a multi-rotor control technique for a drone.

In the embodiment having the above configuration, as shown in FIG. 1, the flight control unit is connected to each of the electromagnetic propulsion units 102 of # 1 to # 4, and the direction of the propulsive force 207 generated by the electromagnetic propulsion unit 102 is set. Further, the actuator unit 105 of # 1 to # 4 that controls the direction of flight may be further provided by changing the control of 104.

The electromagnetic propulsion unit 102 according to this embodiment is completely quiet and environmental because it does not use any fuel components, has no combustion and exhaust gas, is powerful enough, and has endless possibilities for next-generation electric power development. It is possible to realize an eco-friendly flying car 100.

The electromagnetic propulsion unit 102 of the flying car 100 according to the present embodiment can be easily controlled from the flight control unit 104 by a motion vector, and the flight direction, altitude, and speed of the flying car 100 can be freely controlled. be.

The creation of an aircraft like the Flying Car 100 by this embodiment will bring a new big leap in all advances in science and technology, opening up the possibility of much more active development of air and space for humankind. Become.

100 Flying car 101 Body part 102 Electromagnetic propulsion part 103 Power generation part 104 Flight control part 105 Actuator part 200 High voltage capacitor 201 First electrode surface 202 Second electrode surface 203 Positive charge power 204 Negative charge power 205 No Active gas 206 Insulator 207 Propulsion force 208 Large airflow

Claims (5)

A flying vehicle that is an aircraft that is configured to carry a payload that does not include or contains one or more crew members.
An airframe unit having a structure that supports the total airframe weight together with the payload,
The high-voltage capacitor includes an asymmetric high-voltage capacitor that is provided at a plurality of locations on the machine body and operates based on the Biefeld-Brown effect. Multiple electromagnetic propulsion units that generate propulsive force directed toward the second electrode surface of the
Each of the plurality of electromagnetic propulsion units provided in the machine body generates positively charged electric power supplied to the first electrode surface and negatively charged electric power supplied to the second electrode surface. Power generator and
The direction, altitude, and speed of flight by controlling the amount of the positively charged electric power and the negatively charged electric power provided in the aircraft unit and supplied from the electric power generating unit to the plurality of electromagnetic propulsion units, respectively. And the flight control unit that controls
A flying car equipped with. A plurality of actuator units that are connected to each of the plurality of electromagnetic propulsion units and that control the direction of the flight by changing the direction of the propulsive force generated by the electromagnetic propulsion unit by the control of the flight control unit are further provided. The flying car according to claim 1. The flying car according to claim 1 or 2, wherein the power generation unit is a lithium ion battery. The flying car according to claim 3, wherein the electric power generating unit includes a solar panel battery for charging the lithium ion battery. The flying car according to claim 1 or 2, wherein the electric power generation unit is a cold fusion power generation device.

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