WO2018095505A1 - Propulsion par gravité basée sur un principe d'induction par gravité - Google Patents

Propulsion par gravité basée sur un principe d'induction par gravité Download PDF

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Publication number
WO2018095505A1
WO2018095505A1 PCT/EP2016/025153 EP2016025153W WO2018095505A1 WO 2018095505 A1 WO2018095505 A1 WO 2018095505A1 EP 2016025153 W EP2016025153 W EP 2016025153W WO 2018095505 A1 WO2018095505 A1 WO 2018095505A1
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WO
WIPO (PCT)
Prior art keywords
rotation
subdesign
magnetic field
ring
rotating
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Application number
PCT/EP2016/025153
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English (en)
Inventor
Zhan B. NURGALIYEV
Jan VAN TOOR
Original Assignee
Nurgaliyev Zhan B
Van Toor Jan
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 Nurgaliyev Zhan B, Van Toor Jan filed Critical Nurgaliyev Zhan B
Priority to PCT/EP2016/025153 priority Critical patent/WO2018095505A1/fr
Publication of WO2018095505A1 publication Critical patent/WO2018095505A1/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

Definitions

  • the invention relates to the ways of propulsion of a space or aerial vehicle. Background of the invention
  • Propulsion in general refers to a means of creating a force leading to movement.
  • the majority of the current propulsion methods used in space or aerial vehicles are based on creation of a flow of gas or air in the direction opposite to the movement of a vehicle. This is achieved by propellers or by creation of a jet by means of a reaction engine, which can be a jet engine than can operate in the atmosphere or a rocket engine that can be used in space.
  • a reaction engine which can be a jet engine than can operate in the atmosphere or a rocket engine that can be used in space.
  • These types of propulsion are implemented in planes, helicopters and space rockets.
  • There are other proposed types of space propulsion such as ion engines, solar sails and laser propulsion, but they are not used by now.
  • Jet propulsion engines need to throw gases to move a craft. It causes a dependency on the speed of gases, which results in limitations on an achievable acceleration and speed of a vehicle. For example, a journey to Mars can take about eight months using a contemporary rocket engine. Also long space trips require more rocket propellant on board. But the most important limitations of all the current propulsion means are a necessity to overcome the gravity attraction to space bodies and a need to counteract the forces of inertia during an acceleration of a vehicle.
  • the disclosed invention is based on a research into specific effects of gravitational interaction, which allows a construction of a propulsion system of a new type that can cause an acceleration of a vehicle without limitations of the gravity and inertial forces in our present understanding.
  • the proposed design is based on a new theory of gravity and is supported by experimental data. Summary of the invention
  • the proposed gravity propulsion method is based on the principle of gravity induction described by the Four-Dimensional Kinetic Theory of Gravity (FDK) by Zhan Nurgaliyev.
  • the gravity induction principle is based on the phenomenon of gravity induction that follows from the FDK theory.
  • the gravity induction is a production of mass current as a result of a changing surrounding gravity field.
  • a specially oriented acceleration of masses in our three-dimensional space can result in an acceleration of an object in the three-dimensional space.
  • an accelerated movement of masses along special trajectories will cause an acceleration of a space or aerial vehicle.
  • the trajectories of masses can be circular along a surface of an imaginable torus or spiral, which are basically the same circular trajectories with a slight shift.
  • Another approach to realization of the principle is based not on a direct acceleration of masses but only on a rapid change of their trajectories. This is the basic design of a gravity propulsion device.
  • Subdesign 1 Rotation of ions with a rotating ring and an alternating magnetic field.
  • Subdesign 2 Rotation of ions with a rotating magnetic field and an alternating magnetic field.
  • Subdesign 3 Rotation of ions with an electric field and an alternating magnetic field.
  • Subdesign 4 Rotation of ferrofluid with static rings and a magnetic field.
  • Subdesign 5 Rotation of ferrofluid with a static spiral and a magnetic field.
  • Subdesign 6 Rotation of molecules with a static ring and a rotating magnetic field.
  • Subdesign 7 Rotation of fixed solid rings.
  • the trajectories of masses in the propulsion device can be circular along a surface of an imaginable torus.
  • the trajectories of masses in the propulsion device can be spiral along a surface of an imaginable torus.
  • FIG. 3 The parts of the propulsion device and the trajectories of masses in two dimensions. Drawings illustrating the subtypes of the basic design of a gravity propulsion device:
  • Subdesign 1 Rotation of ions with a rotating ring and an alternating magnetic field.
  • Fig. 7 The formation of a dense plasma cord in the center of the torus.
  • Fig. 8 Rotation of ions in the ring by a magnetic field.
  • Subdesign 3 Rotation of ions with an electric field and an alternating magnetic field.
  • Fig. 9 The electric field is used to create a flow of charged particles along the torus.
  • Subdesign 4 Rotation of ferrofluid with static rings and a magnetic field.
  • Fig. 10 The rings with ferrofluid, its movement direction, electromagnetic coils and the central mass (view from the side).
  • Fig. 11 The rings with ferrofluid and central mass (view from the top).
  • Subdesign 5 Rotation of ferrofluid with a static spiral and a magnetic field.
  • Fig. 12 The toroidal spiral with ferrofluid and central mass.
  • Subdesign 6 Rotation of molecules with a static ring and a rotating magnetic field.
  • Subdesign 7 Rotation of fixed solid rings.
  • FIG. 14 Several rotating rings or disks arranged in a torus-like formation.
  • Subdesign 8 Rotation of solid rings as gyroscopes.
  • Fig. 15 A set of gyroscopes on a circular rotatable frame (view from the top).
  • Fig. 16 A set of gyroscopes on a circular rotatable frame (view from the side).
  • Fig. 17 The position of the circular frame before rotation.
  • the proposed gravity propulsion method is based on the principle of gravity induction described by the Four-Dimensional Kinetic Theory of Gravity (FDK) by Zhan Nurgaliyev.
  • the FDK theory is based on an assumption that all masses move in the same direction along the fourth coordinate, perpendicular to the observable three-dimensional space.
  • the assumption is in accordance with the theory of the Big Bang and the expanding Universe, which can be described as an expanding four-dimensional sphere.
  • the flows of mass can be called the currents of mass.
  • the gravity attraction forces are the result of attraction of these currents of mass, that occur due to their movement in the same direction, similar to the Ampere's attraction forces of two electric currents in electromagnetism, but the currents of mass are of another nature and they flow in the four-dimensional space.
  • the gravity field is propagated through a three-dimensional space. That is why the forces are inversely proportional to a square of the distance between masses unlike in the case of the Ampere's attraction of two electric currents.
  • the gravity induction principle is based on the phenomenon of the gravity induction that follows from the FDK theory.
  • the gravity induction is a production of mass current as a result of a changing surrounding gravity field.
  • a specially oriented acceleration of masses in the three-dimensional space can result in an acceleration of an object in the three dimensional space.
  • an accelerated movement of masses along special trajectories will cause an acceleration of a space or aerial vehicle.
  • the trajectories of masses can be circular along a surface of an imaginable torus (Fig. 1) or spiral (Fig. 2), which are basically the same circular trajectories with a slight shift.
  • the trajectories of masses are labeled by T and the resulting acceleration of the central mass M and the vehicle is labeled by A.
  • the trajectories are vortex-like and are oriented in the common direction toward the center of the torus.
  • the central mass M is not necessarily a certain special mass. It can be made of any material, but it must be a part of the rigid structure of the vehicle.
  • the central mass is the place where the most of the accelerating force will be applied.
  • the inertial forces counteracting an acceleration are expected to be decreased or neutralized since the gravity propulsion will directly affect the movement of all the masses of the vehicle, not acting as an external force, but changing a field that is directly connected with the essence of movement according to the FDK theory.
  • the propulsion method is also expected to lower a load on pilots and a vehicle during accelerations, since the mass flow induced by the propulsion device is caused by a field that covers the whole vehicle. It will result in a near simultaneous acceleration of all the parts of a vehicle and the bodies of pilots.
  • Subdesign 1 Rotation of ions with a rotating ring and an alternating magnetic field.
  • Working body has a form of a ring that can have a circular cross section (a torus shape) or other cross section (Fig. 4).
  • Working body W is a substance that consists of ions - electrically charged atoms or molecules in an ionized state (ionized hydrogen, deuterium, noble gas or mercury, for example).
  • the substance should as dense as possible to maximize the propulsion effect.
  • the substance can be, for example, an ionized liquid or gas, or plasma.
  • the ring with the working body W is put into constant rotation, which continues at each further stage of the device's operation.
  • the propulsion device has the following stages of operation.
  • a strong magnetic field B with field lines directed along the ring is applied (Fig. 5).
  • the coils with electric current that create the magnetic field are shown schematically on Fig. 5 as C, their real shape can vary.
  • the magnetic field causes a spiral movement of all the ions m of the working body (Fig. 6).
  • the central mass M experiences an acceleration A due to the gravity induction. All the parts of the vehicle, which are located along the central line of the ring, are also accelerated.
  • the propulsion device accelerates the vehicle.
  • the magnetic field is turned off.
  • the device is decelerating, since at this stage an acceleration is directed opposite to the movement of the vehicle.
  • the ring can heat up at this stage. A cooling system will be needed to avoid overheating of the device.
  • Each cycle of the propulsion device pushes the vehicle forward.
  • the resulting motion of the vehicle has an impulse character.
  • Subdesign 2 Rotation of ions with a rotating magnetic field and an alternating magnetic field.
  • the design is different from the Subdesign 1 in how ions are put into initial rotation along the ring. Instead of rotating the ring, ions of the working body W in this design are rotated within the ring by a magnetic field B (Fig. 8).
  • the coils with electric current that create the magnetic field B are shown schematically on Fig. 8 as C, their real shape can vary.
  • Subdesign 3 Rotation of ions with an electric field and an alternating magnetic field.
  • the design is different from the Subdesign 1 in how ions are put into initial rotation along the ring. Instead of rotating the ring, an electric field is used to create a flow of ions along the torus (Fig. 9). A flow of ions appears between positively and negatively charged electrodes Ei and E 2 . There can be one or more sections contacting a pair of electrodes within the torus.
  • Subdesign 4 Rotation of ferrofluid with static rings and a magnetic field.
  • Working body is a ferrofluid that is a liquid with ferromagnetic particles.
  • the liquid is contained in several circular rings R (Fig. 10) that are arranged in a torus-like formation around the central mass M (Fig. 11).
  • the ferrofuid F is magnetic and is accelerated by electromagnetic coils C.
  • the coils are shown schematically, their real shape can vary. There can be one portion of ferrofuid per ring or several ones. For example, if we rotate two portions of ferrofluid in one ring (Fig. 10), then the ring will not vibrate during operation.
  • a superfluid for example, superfluid helium
  • a superfluid helium can be used as a carrier for the ferrofluid. In this case, there will no energy losses on friction of the rotating ferrofluid.
  • the propulsion device has the following stages of operation.
  • the electromagnetic coils C accelerate the ferrofluid portions in the rings in the common direction toward the center (Fig. 10).
  • the central mass M experiences an acceleration A due to the gravity induction. All the parts of the vehicle, which are located along the central line, are also accelerated.
  • the propulsion device accelerates the vehicle.
  • Subdesign 5 Rotation of ferrofluid with a static spiral and a magnetic field.
  • the design is different from the Subdesign 4 in the form of the container for the ferrofluid. Instead of rings, the ferrofluid F is contained and accelerated inside a toroidal spiral (Fig. 12). A part of the spiral is shown on Fig. 12, with the direction of the ferrofluid's rotation.
  • Subdesign 6 Rotation of molecules with a static ring and a rotating magnetic field.
  • Working body has a form of a ring that can have a circular cross section (a torus shape) or other cross section.
  • Working body is a substance that consists of polar molecules, that is molecules with a nonzero magnetic dipole moment, in a liquid, gaseous or other state (like water, for example).
  • Rotation of the electromagnetic field B causes rotation of each molecule of the working body W in the plane of the cross section of the torus (Fig. 13).
  • the coils with electric current that create the magnetic field B are shown schematically on Fig. 10 as C, their real shape can vary.
  • the propulsion device has the following stages of operation.
  • the rotating magnetic field is turned on, that causes a circular movement of all molecules in the common direction toward the center (Fig. 13).
  • the central mass experiences an acceleration due to the gravity induction. All the parts of the vehicle, which are located along the central line of the ring, are also accelerated.
  • the propulsion device accelerates the vehicle.
  • the magnetic field is turned off or significantly diminished either in terms of strength or in terms of frequency.
  • the device is decelerating, since at this stage an acceleration is directed opposite to the movement of the vehicle.
  • the ring can heat up at this stage. A cooling system will be needed to avoid overheating of the device.
  • Each cycle of the propulsion device pushes the vehicle forward.
  • the resulting motion of the vehicle has an impulse character.
  • Subdesign 7 Rotation of fixed solid rings.
  • Working body consists of several rotating solid rings or disks R (Fig. 14) that are arranged in a torus-like formation around the central mass M.
  • the rings are simultaneously accelerated by motors with a high torque or other sources of mechanical rotation capable of fast acceleration.
  • the rings can be made of metal or other durable material.
  • the propulsion device has the following stages of operation.
  • the motors are turned on, that causes rotation of all the rings R in the common direction toward the center (Fig. 14).
  • the central mass M experiences an acceleration due to the gravity induction. All the parts of the vehicle, which are located along the central line of the ring, are also accelerated.
  • the propulsion device accelerates the vehicle.
  • Subdesign 8 Rotation of solid rings as gyroscopes.
  • Working body consists of several rotating solid rings or disks R (Fig. 15 and 16) in a simple gyroscopic suspension installed on a circular frame F.
  • the resulting arrangement is basically a set of gyroscopes on a circular rotatable frame.
  • the rings can be made of metal or other durable material.
  • the suspension of a single disk Ri attached to the circular rotatable frame F is shown on the Fig. 16.
  • the propulsion device has the following stages of operation.
  • the rotating circular frame F is turned by 90 degrees (Fig. 17 and 18), which causes all the gyroscopes to change their orientation in relation to the center of the circle.
  • the rotation of one of the gyroscopes R in marked in gray. Its axis of rotation is keeping its direction in space.
  • the central mass M experiences an acceleration due to the gravity induction. All the parts of the vehicle, which are located along the central line of the ring, are also accelerated.
  • the propulsion device accelerates the vehicle.

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

Abstract

L'invention concerne les moyens de propulsion d'un véhicule spatial ou aérien. L'invention concerne la conception de base du dispositif de propulsion par gravité sur la base du principe d'induction par gravité et de ses six sous-conceptions. La conception de base réalise une rotation rapidement accélérée de masses le long de trajectoires circulaires ou en spirale suivant le long de la surface d'un tore pouvant être imaginable ou une acquisition rapide des trajectoires nécessaires par des masses rotatives. Cette accélération des masses tournantes provoque une accélération de la masse centrale et d'autres parties de la structure du véhicule. Les sous-conceptions comprennent trois procédés de rotation d'ions, deux procédés de rotation de ferrofluide, une conception de rotation moléculaire, une rotation d'anneaux solides fixes et une conception basée sur une rotation de gyroscopes.
PCT/EP2016/025153 2016-11-22 2016-11-22 Propulsion par gravité basée sur un principe d'induction par gravité WO2018095505A1 (fr)

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PCT/EP2016/025153 WO2018095505A1 (fr) 2016-11-22 2016-11-22 Propulsion par gravité basée sur un principe d'induction par gravité

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20010032522A1 (en) * 2000-01-24 2001-10-25 Ulysses Davis Vectored inertia drive wobble drive
WO2009102227A2 (fr) * 2008-02-12 2009-08-20 Dumitru Ionescu Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction
WO2011158048A2 (fr) * 2010-06-17 2011-12-22 Grigorios Karamitsos Mécanisme de propulsion de l'impulsion inertielle double

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20010032522A1 (en) * 2000-01-24 2001-10-25 Ulysses Davis Vectored inertia drive wobble drive
WO2009102227A2 (fr) * 2008-02-12 2009-08-20 Dumitru Ionescu Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction
WO2011158048A2 (fr) * 2010-06-17 2011-12-22 Grigorios Karamitsos Mécanisme de propulsion de l'impulsion inertielle double

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
"Conservation of momentum", INTERNET CITATION, 2007, pages 1, XP002447082, Retrieved from the Internet <URL:http://www.britannica.com/eb/article-9053290> [retrieved on 20070903] *
"Mechanics (Page: Conservation of momentum)", INTERNET CITATION, 2007, XP002447083, Retrieved from the Internet <URL:http://www.britannica.com/eb/article-77548> [retrieved on 20070816] *
ZHAN NURGALIYEV: "ON POSSIBLE CONSEQUENCES OF AN ALTERNATIVE APPROACH TO UNDERSTANDING GRAVITATIONAL INTERACTION ON POSSIBLE CONSEQUENCES OF AN ALTERNATIVE APPROACH TO UNDERSTANDING GRAVITATIONAL INTERACTION", 24 November 2016 (2016-11-24), XP055393967, Retrieved from the Internet <URL:https://hal.archives-ouvertes.fr/hal-01401931/document> [retrieved on 20170725] *

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