WO2022208507A1 - Système de propulsion spatiale solaire - Google Patents

Système de propulsion spatiale solaire Download PDF

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Publication number
WO2022208507A1
WO2022208507A1 PCT/IN2021/050333 IN2021050333W WO2022208507A1 WO 2022208507 A1 WO2022208507 A1 WO 2022208507A1 IN 2021050333 W IN2021050333 W IN 2021050333W WO 2022208507 A1 WO2022208507 A1 WO 2022208507A1
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WO
WIPO (PCT)
Prior art keywords
space
propulsion
reaction force
force
probe
Prior art date
Application number
PCT/IN2021/050333
Other languages
English (en)
Inventor
Praveen KUMAR NARAYANAN
Original Assignee
Kumar Narayanan Praveen
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 Kumar Narayanan Praveen filed Critical Kumar Narayanan Praveen
Priority to PCT/IN2021/050333 priority Critical patent/WO2022208507A1/fr
Publication of WO2022208507A1 publication Critical patent/WO2022208507A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00—Subject matter not provided for in other groups of this subclass
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K99/00—Subject matter not provided for in other groups of this subclass
    • H02K99/20—Motors

Definitions

  • This invention is a space propulsion system that will replace rockets and ion propulsion systems.
  • This space engine has the capacity to operate as the electric rail route system between heavenly bodies so there will be stellar or planetary industrial revolution as we can transport materials and people between heavenly bodies with Hitech electric propelling vehicles or space probes.
  • T is the time taken by the 2nd magnet(Reaction force) to reach/interact with the surface of the space engine cylinder(that will be at a distance D) after the repulsion force is established between two magnets.
  • reaction force(or opposite force) can be delayed from not acting on the surface of the system thereby achieving acceleration of the closed system in one direction by the action force which instantly acts on the surface of the closed system and delaying the other reaction force, which does not hinder the work done by the action force, for a time period T.
  • This force due to delayed work done by the reaction force is the basic working principle of this propulsion system.
  • Ion propulsion has inert gases as fuel which again will drop its level with time and the thrust achieved is very low for higher payload capacity missions. Since its fuel lasts longer than rockets it reaches very high speed comparing the rocket system. • Nuclear propulsion is risky and radiations will cause permanent damages to the payload. So a risk free and fuel less propulsion system will make a revolution in the field of transport between heavenly bodies by reducing the transport cost with the use of solar power. With a space engine using solar power for propulsion the probe can travel anywhere within the solar system efficiently. IEF SUMMARY OF THE INVENTION i. The invention of the space engine that will work like an electric car to establish transportation in the vacuum of space.
  • the engine uses electro- magnetic repulsion force to propel the probes so by continuous strokes of the engine the probe will be sent to space and other heavenly bodies without the need of fuel as it completely works with the electrical system, solar energy can be used as the fuel source.
  • the magnetic repulsion force is used as the propelling force with which the probe will be moved between a distance.
  • the engine uses the concept of Delayed Newtonian reaction force. “Every action has equal and opposite reaction.” By intelligent design of engineering, the opposite reaction force is delayed to not act upon the surface of the probe for a time period T.
  • the action force interacts with the internal wall of the probe by the instant when the repulsion force is established, thereby pushing the probe in the direction of the action force until the reaction force hits the opposite end of the cylinder in the space engine after a time time T crossing a distance D inside the cylinder without interacting with the probe body. So when the reaction force acts upon the surface of the probe the push force of the action force is neutralised so the probe remains unaccelerated but the forward displacement achieved by delaying the reaction force remains unchanged. To keep the probe moving continuously, a soft braking system is used which converts kinetic energy to heat energy so the reaction force does not affet the work done by the initial action force. By doing this higher acceleration can be achieved. iii.
  • the figure [1] is the OFF mode of the space engine or 1st stroke.
  • the electromagnet and the small permanent magnet are close to each other. This is possible only when the electromagnet is demagnetised. The probe remains still without any propulsion.
  • the figure [2] is the ON mode or the 2nd stroke.
  • the electromagnet is magnetised such that the electromagnet and the permanent magnet repel each other. Due to this repulsion force between the magnets, there will be equal and opposite force between the magnets in both the directions.
  • the space engine cylinders are designed such that the permanent magnet does not interact with the walls of the space probe until a time period T. At the same time the electromagnet remains attached to the surface of cylinder so the force is transferred to the probe wall instantly in one direction, the opposite reaction force is delayed to interact with the probe so the reaction force is delayed and the action force starts to move the probe in one direction until the time period T.
  • the Figure [3] is the 3rd stroke of the engine. Now the permanent magnet hits the surface of the probe, so the acceleration of the probe in one direction is stopped but the probe continues to move with the velocity V m/s as there is a cushion that transfers kinetic energy to heat energy, by using a ideal cushion very high acceleration can be achieved.
  • the figure [4] is the 4th stroke where the motor is switched ON and the electromagnet is switched OFF. Now the screw mechanism will push the permanent magnet back to its original position, closer to the electromagnet. With the repetition of the cycle acceleration for time T is achieved again then the velocity of 2 V m/s is achieved in the 2nd cycle. With every cycle the velocity V increases which can be represented graphically.
  • the screw mechanism is represented in the figure[5] which will push the permanent magnet back to its original position for the continuity cycle of the engine at the stroke 4 of the space engine.
  • the Permanent magnet is designed such that there is a threaded hole in the middle, which will help in raising the permanent magnet back to its original by the clockwise rotation of the screw rod using the stepper motor.
  • the threaded hole then will be covered by the sliding bearing setup which will help the permanent magnet slide across the rod until it hits the cushion surface. Then again the threads are used to raise magnets back to its position.
  • slide rod and the screw rod can be a separate setup, which will make the magnet slide using sliding rod and recoil using screw rod. This is explained in Figure[6]

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

L'invention concerne des systèmes de propulsion spatiale sans fusée qui seront une nouvelle révolution dans le domaine des explorations spatiales. Le système est un moteur électrique qui est capable de se propulser lui-même dans l'espace à l'aide d'énergie solaire et sans utiliser de carburant qui se dissipe au fil du temps. Ainsi, la propulsion peut être plus longue et ainsi le système permet d'atteindre des vitesses très élevées. L'unité utilise une répulsion électromagnétique et une force de réaction retardée dans le système pour déplacer le système dans l'espace. Grâce à cette propulsion, même un astéroïde de taille considérable peut être propulsé dans l'espace à l'aide uniquement de l'exploitation de l'énergie solaire. En ajoutant les moteurs dans les aubes du générateur, l'énergie solaire peut ainsi mieux être exploitée que si des panneaux solaires ont été utilisés. Un mouvement et un déplacement globaux dans l'environnement spatial est obtenu à l'aide de cette technologie.
PCT/IN2021/050333 2021-04-03 2021-04-03 Système de propulsion spatiale solaire WO2022208507A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/IN2021/050333 WO2022208507A1 (fr) 2021-04-03 2021-04-03 Système de propulsion spatiale solaire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IN2021/050333 WO2022208507A1 (fr) 2021-04-03 2021-04-03 Système de propulsion spatiale solaire

Publications (1)

Publication Number Publication Date
WO2022208507A1 true WO2022208507A1 (fr) 2022-10-06

Family

ID=83458383

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IN2021/050333 WO2022208507A1 (fr) 2021-04-03 2021-04-03 Système de propulsion spatiale solaire

Country Status (1)

Country Link
WO (1) WO2022208507A1 (fr)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IN201941047499A (fr) * 2019-11-21 2020-08-07 Praveen Kumar N.

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IN201941047499A (fr) * 2019-11-21 2020-08-07 Praveen Kumar N.

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