WO2020035740A1 - Picky engine by electric discharge force - Google Patents

Picky engine by electric discharge force Download PDF

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Publication number
WO2020035740A1
WO2020035740A1 PCT/IB2019/000948 IB2019000948W WO2020035740A1 WO 2020035740 A1 WO2020035740 A1 WO 2020035740A1 IB 2019000948 W IB2019000948 W IB 2019000948W WO 2020035740 A1 WO2020035740 A1 WO 2020035740A1
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WO
WIPO (PCT)
Prior art keywords
electromagnetic impact
pistons
impact thrust
magnets
electromagnetic
Prior art date
Application number
PCT/IB2019/000948
Other languages
French (fr)
Inventor
Gholamreza BORD BAR
Original Assignee
Bord Bar Gholamreza
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bord Bar Gholamreza filed Critical Bord Bar Gholamreza
Publication of WO2020035740A1 publication Critical patent/WO2020035740A1/en

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Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05HPLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00Generating plasma; Handling plasma
    • H05H1/54Plasma accelerators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00Subject matter not provided for in other groups of this subclass

Definitions

  • the technical problem is related to low-speed of spacecraft to travel interplanetary and high-consume fuel and diminish saved fuel to continue the path.
  • the aim of this invention is to reduce travel time interplanetary and access to the unreachable universe.
  • it causes countries military superiority in possible wars and less-consumed boats (floating) fuel.
  • it can be effective on the Earth and other planets.
  • cooling equipment strong cooling system
  • sheep around the cylinder to keep the piston and the cylinder cool and intact.
  • Fig (1) is considered as the static electricity power supply.
  • Fig (4) is a power supply to generate electricity that uses sunlight to generate electricity and is used extensively as a power source outside the atmosphere, but the main work is on Figs (2) and (3), that is, two inventions types with a mechanism and in different ways to produce energy and motion, that in both Figs chamber material and used-material in piston, cylinders, conductors’ plates and the electrical magnet are low-weight and resistant. So our invention contains Figs (2) and (3). In Fig (2), the repulsive force between analogous charges or electrical discharge impact is used to drive, and in Fig (3), the repulsive force between magnet analogous charges is used to move.
  • this device needs a system out of the main chamber to move, in other words, needs an external factor to move.
  • it uses gravity and repulsive force among embedded winding in rails and trains to move backward and forward, no electric magnet.
  • My device works based on electromagnetic force impacts (electric explosion); not only magnetic repulsion. This phenomenon is modeled from the sun's electromagnetic waves on the Earth's magnetic shield.

Abstract

1. Invention title: impact thrust by electromagnetic forces (invention supplement with number 95625) 2. We need propulsion engine in space trips to move forward that this engine consumes a lot of fuel and energy. To save consumed fuel we can use spacecraft driver helper propulsion considering considerations in terms of initial energy generation in the places in the solar system where there is no the planet's gravity and in the places far from the solar system. 3. The basis of this device is based on Newton's action and reaction force that here we want to challenge this formula outside the planet's gravity circuit. Also, the impact of a beaten object and kind of motion which is created has been used. 4. This innovation is in the field of electromagnetic knowledge.

Description

The invention description
1- Invention title: impact thrust by electromagnetic forces ((invention supplement with number 95625)
2- This invention technical field: it is about aerospace dynamics and objects aerodynamics.
3- Technical problem and invention goals: the technical problem is related to low-speed of spacecraft to travel interplanetary and high-consume fuel and diminish saved fuel to continue the path. The aim of this invention is to reduce travel time interplanetary and access to the unreachable universe. In addition, it causes countries military superiority in possible wars and less-consumed boats (floating) fuel. Also, it can be effective on the Earth and other planets.
4- Description of previous knowledge and advances history in terms of claimed invention: about work already have been done in this field is using solid and liquid fuel engines to generate running force by the vehicle inside and outside of the atmosphere. In addition, electromagnetic gravity and the repulsive force is used to create motion in Meglo trains and using electric cells to in-spacecraft energy supply and recently using gas as spacecraft propulsion. It means, gas ions have been accelerated and are thrown into the chamber that enters force to the front of the spacecraft and causes spacecraft goes forward. But this method is a theory and has not been implemented.
5- provide a solution to solve existing technical problem with invention detailed, sufficient, and integrated description: to solve relevant problem, we use the defect in Newton's third law in association with objects motion in planets outside circuit, so that because in planets outside circuit gravity effect is low and friction force caused by air molecules is disappeared. So that entered-object force causes driving forward with the least resistance. It means the reaction force is entered to the object in the opposite direction of the object but inequality and less than it. Therefore, considering we intend to use a dissimilar force with solid fuel engine power to save energy, so energy source must be something more powerful than initial propulsion force outside the planets orbit. As a result, we decided to use the electric cells and its generated electric power to generate motion for spacecraft using driver helper. In this engine, which includes technical drawing Fig.2 and Fig.3, electric power in Fig. 2, using the repulsive force property between the analogous loads, and in Fig. 3, using the repulsive force generated by the magnetic induction between the analogous loads, causes the piston motion in the cylinder to forward and push to system chamber and thus vehicle motion forward or backward. It should be noted that the Figs (1) and (4) are used only to provide the power supply. It should be noted that aside from the mentioned case, the required force in figure (2) can also be provided by electrical discharge effect and its explosion effect through injecting a mi ture of oxygen and hot dense air adjacent to the power house of the ship. It is also worth mentioning that generation of hot dense air is feasible by a compressor in proximity of the power house and using the electric energy of the ship. In order to diminish the abundant heat of the cylinder, cooling equipment (strong cooling system) is to be used inside the sheep around the cylinder to keep the piston and the cylinder cool and intact.
- Figures, designed, and graphs explanation: As shown in the technical plane, four titles with the names of the form (1), Fig. 2 (Fig. 3) and Fig. 4, are shown on the technical plane that Fig (1) is considered as the static electricity power supply. Fig (4) is a power supply to generate electricity that uses sunlight to generate electricity and is used extensively as a power source outside the atmosphere, but the main work is on Figs (2) and (3), that is, two inventions types with a mechanism and in different ways to produce energy and motion, that in both Figs chamber material and used-material in piston, cylinders, conductors’ plates and the electrical magnet are low-weight and resistant. So our invention contains Figs (2) and (3). In Fig (2), the repulsive force between analogous charges or electrical discharge impact is used to drive, and in Fig (3), the repulsive force between magnet analogous charges is used to move.
- Clear and accurate advantages of the invention than previous ones: In previous inventions, solid fuels and in stages liquid fuel or a combination were used to drive spacecraft or vehicle, this has caused excessive fuel consumption in spacecraft and inability to continue between planets. In addition, spacecraft did not have sufficient speed and acceleration, using this method, due to use solar energy to provide invention power cause saving solid fuel consumption in the vehicle and more acceleration and speed in spacecraft to traverse interplanetary and reduce space missions time cause floating engines have many noises. Also, the high-power force outside the planet's plates becomes obvious moreover, if impact thrust is used along with electrical discharge force, we will have a power more than when we use the electric or magnetic repulsion force between similar charges or poles, since by using this force, we can move on the Earth and other planets that have gravity as well.
About electromagnetic or Meglo trains, this device needs a system out of the main chamber to move, in other words, needs an external factor to move. In addition, it uses gravity and repulsive force among embedded winding in rails and trains to move backward and forward, no electric magnet. Also, their high set up cost, maintaining, high vulnerability against earthquake, lack of technology, low safety, and not having a long distance history because this technology is used by few wealthy countries and the areas where there is a little earthquake. Therefore, my device in both operation and price is better than same samples. Actually, no similar sample in terms of performance, lack of limitation in places, and pricing not been seen. My device works based on electromagnetic force impacts (electric explosion); not only magnetic repulsion. This phenomenon is modeled from the sun's electromagnetic waves on the Earth's magnetic shield.
- explain at least an executive method to apply invention on the Earth needs physics labs and create vacuum and weightlessness conditions but it could be shown in floating (boats) easily for example in ships that are made of light and resistant materials and also in submarines that have proper aerodynamic shape and are made of resistant materials. Using this energy, we have both energy saving and more speed to travel between countries harbors, which reduces travel time. Of course, one application is related to the military debate, which is imaginable in high-range ballistic missiles and in the situation that ships need to travel in full silence. In addition, impact thrust can move on the Earth and can be used in today's transport equipment (don’t forget this is a driver helper or propellant, not a propulsion engine).- The explicit mention of invention industrial application: technical plane pr plans based on Article 11 of the executive bill of patent law are designed. These plans have to be designed by software programs and are represented in details. Provide the actual image of the invention is not acceptable as a technical plane. If your claim is a new process, draw a block diagram: As mentioned before, of this invention industrial application is in spatial industry, maritime transportation, and military industry that shipping industry contains ships, submarines, and military industries, includes high- range ballistic missiles and space industry includes long-term missions in space traveling. Of course, impact thrust can be used on the Earth and planets with gravity that it is an advantage than spacecraft helper. In addition, the invention of technical design has been sent as the attachment.

Claims

Invention Claim
[Claim 1] Electromagnetic impact thrust is made of one vandograph, four Power supplies or solar cells and a main chamber, two cylinders and two pistons inside it plus an electric motor, two fixed magnets, cylinder holders, eight rechargeable capacitors, two fixed conductive plates and two meters of thin lacquer wire, an non-metallic bar, two iron nails and two small electric magnets, and power supply switch and a DC step-up transformer.
[Claim 2] Electromagnetic impact thrust has used a vandograph based on the first claim, which has used a power supply to generate power for electric repulsion creation by a power supply switch.
[Claim 3] Electromagnetic impact thrust based on the first claim has used two cylinders and two pistons inside it and two conductive plates, where two ends of pistons and conductive plates are connected to the vandograph. Fig.(2-(l-l)).
[Claim 4] Electromagnetic impact thrust based on the first claim is made of two pistons, that one end of pistons are in proximity of conductive plates or capacitors and other ends are connected to chamber wall or base structure.
[Claim 5] Based on the first claim, Electromagnetic impact thrust, is made of a step-up transformer and two cylinders. The step-up transformer generates the voltage needed for explosion and the cylinders can have two entrance or exit bars for air or gas. Fig.(2-(2-l)).
[Claim 6] Based on the fifth claim, Electromagnetic impact thrust has two entrance or exit bars of gas or air which are set in a way that they suck the oxygen or ozone gas long with dense hot air from one end and exhaust the impurity caused by the explosion through the other end.
[Claim 7] Electromagnetic impact thrust based on the first claim has eight rechargeable capacitors that four of them are connected to pistons’ ends and other are placed fixed in their proximity: figure (2-(2-l)).
[Claim 8] Based on the first claim, electromagnetic impact thrust is made of eight rechargeable capacitors that four of them are placed in the two ending leads of cylinders and pistons to create aa strong reaction mode when using an electrical vacuum motor is needed.
[Claim 9] Based on the seventh claim, electromagnetic impact has eight capacitors, four of which are connected to the pistons and start of the cylinder connect to the power supply and the step-up transformer via a wire that passes through wall of the cylinder, and the other four connect to the other lead of the power supply (when using electrical vacuum motor).
[Claim 10] Based on the first claim, electromagnetic impact thrust has four power supplies, one of which is used in figure (2) and the other three are used in figure (3).
[Claim 11] Electromagnetic impact thrust based on the tenth claim has used two electric magnets which are placed on a base that can be placed inside or outside of the chamber.
[Claim 12] Electromagnetic impact thrust based on the eleventh claim is made of an electric motor and two fixed magnets and a non-metal bar those two magnets are placed on two ends of a bar and the bar is as an electric motor propeller. Fig.3
[Claim 13] Electromagnetic impact thrust based on the twelfth claim is made of one electric motor and two fixed magnets which are used as a strong magnet that can connect and disconnect the current in a fraction of a second.
[Claim 14] Electromagnetic impact thrust based on the thirteenth claim is made of two fixed magnets and one electric motor that all of them are in the vicinity of two fixed electric magnets (interaction of repulsive forces).
[Claim 15] Electromagnetic impact thrust based on the fourteenth claim, consists of two permanent magnets and an electrical motor, the set of which is in proximity of two electromagnets (pistons) (for the purpose of interaction of repulsive forces).
PCT/IB2019/000948 2018-08-08 2019-08-12 Picky engine by electric discharge force WO2020035740A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IR13973004370 2018-08-08
IR139750140003004362 2018-08-08
IRNONE 2018-12-08

Publications (1)

Publication Number Publication Date
WO2020035740A1 true WO2020035740A1 (en) 2020-02-20

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PCT/IB2019/000948 WO2020035740A1 (en) 2018-08-08 2019-08-12 Picky engine by electric discharge force

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WO (1) WO2020035740A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112618865A (en) * 2020-12-21 2021-04-09 吉林大学 Be applied to infusion autoalarm among vein treatment

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140013724A1 (en) * 2011-03-25 2014-01-16 Cannae Llc Electromagnetic thruster

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140013724A1 (en) * 2011-03-25 2014-01-16 Cannae Llc Electromagnetic thruster

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112618865A (en) * 2020-12-21 2021-04-09 吉林大学 Be applied to infusion autoalarm among vein treatment

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