WO2023130168A1 - Système de propulsion utilisant des bobines - Google Patents

Système de propulsion utilisant des bobines Download PDF

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Publication number
WO2023130168A1
WO2023130168A1 PCT/BR2022/050531 BR2022050531W WO2023130168A1 WO 2023130168 A1 WO2023130168 A1 WO 2023130168A1 BR 2022050531 W BR2022050531 W BR 2022050531W WO 2023130168 A1 WO2023130168 A1 WO 2023130168A1
Authority
WO
WIPO (PCT)
Prior art keywords
coil
dielectric
propulsion system
coils
toroidal
Prior art date
Application number
PCT/BR2022/050531
Other languages
English (en)
Portuguese (pt)
Inventor
Alexandre TIAGO BAPTISTA DE ALVES MARTINS
Original Assignee
Tiago Baptista De Alves Martins Alexandre
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
Priority claimed from BR102022000458-7A external-priority patent/BR102022000458A2/pt
Application filed by Tiago Baptista De Alves Martins Alexandre filed Critical Tiago Baptista De Alves Martins Alexandre
Publication of WO2023130168A1 publication Critical patent/WO2023130168A1/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
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F5/00—Coils
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00—Magnets
    • H01F7/06—Electromagnets; Actuators including electromagnets

Definitions

  • the present invention relates to a new form of air, land, submarine or space propulsion, achieved by the use of suitable electromagnetic interactions that will be explained below.
  • E is the applied external electric field and P is the atomic polarization vector of a linear dielectric:
  • Equation (8) represents the total balance between force densities that should exist due to the conservation of the total linear momentum between the matter considered and the fields, that is: [012]
  • Equation (1) and (4) the linear momentum density of electric field P E in the capacitor can be written as:
  • Equation (2) the potential energy of interaction is negative for dielectrics subjected to electric fields, as shown in Equation (1). This negative moment means that the electric field moment is directed in the opposite direction to the applied electric field vector, as confirmed also by experimental observations. From Equations (8) and (10), the electrical displacement force becomes:
  • EJ E is the displacement current density in vacuum:
  • Equation (14) also includes forces related to the variation of Polarization P (Equation (2)) of the dielectric material 3 used, that is, it includes variations in time of two different variables: both the applied electric field E and the relative electrical permittivity s r of dielectric 3 used.
  • Equation (14) represents the time version of the Kelvin f KE spatial electric gradient force equation, given by:
  • Equation (17) which gives us the spatial gradient of the electric field in terms of the temporal variation of the electric field and its velocity.
  • Equation (11) and (14) denote an electrical displacement and polarization force that acts on dielectrics, which is completely electrical in origin.
  • this force is generated by interaction with the momentum of space-time itself, which is equivalent to the momentum of the electric field.
  • this force can also be called "space warp” force, due to the direct interaction with space-time and its deformation, that is, alteration of its momentum.
  • V x E — ôB/ôt(19)
  • A is the magnetic potential vector of the current I flowing in coil 1.
  • Equation (14) only develops directional forces when the derivative of the applied electric field is asymmetric. If in a given pulse of electric field, with vector directed to the right, the derivative of the first increase of the field ("rise time”) is faster than its subsequent decay (“fall time”), then a force will be generated in the direction of the electric field vector ( Figure 1.3)), and if the derivative of the decay (“fall time”) ") of the electric field is faster than its rise time derivative, then a force will be generated in the opposite direction to the applied electric field vector ( Figure 1.4)).
  • Equation (14) is unique because it is directly proportional to E - dE/dt, not requiring time integration as done for Lorentz forces and others that are initially formulated in steady state.
  • a great advantage of the electrical displacement or polarization force is that the shorter the applied pulse, the stronger the generated force, due to the fact that it is a time-dependent force where the momentary gradient of the electric field propagated in the dielectric increases. with the speed of the pulse. In this way, the propagation of a single voltage pulse or longitudinal electric field will directly generate the force given by Equation (14). If a single asymmetrical voltage pulse generates a force of 1 N, then if we apply a rate of 1000 pulses per second, the total force generated will be 1000 N. In this way we can generate small or giant forces using the same physical system.
  • the dielectric 3 will move in the direction necessary to satisfy the conservation of the total momentum of the spacetime around it. Any acceleration generated by mechanical forces will feel inertial forces, due to the relative movement of space-time opposite to the acceleration of the object, and where the momentum and temporal variation of the momentum of the mass involved and space-time should cancel according to Equations (7 ) and (9).
  • the force in the propulsion system of this patent is generated by direct interaction with space-time, where the moment of the electric field also corresponds to the moment of space-time, then the generated forces will be produced without inertia, that is, without resistance of the space-time and will affect the whole system.
  • the same process happens for bodies accelerated by gravitational forces that directly modify space-time, which according to the theory of Einstein's relativity will not feel any inertia force when being accelerated by a gravitational field.
  • Figure 2 represents various forms of application of propulsion systems using coils 1, toroidal, with a dielectric 3 in its central area.
  • Figure 3 represents various forms of application of propulsion systems using coils 1, toroidal, with a dielectric 3 in its internal and external zone.
  • Figure 4 represents various forms of application of propulsion systems using more than one coil 1, toroidal, around the dielectric or dielectrics 3.
  • Figure 5 represents various forms of application of propulsion systems using several coils 1, linear, around several dielectrics 3.
  • Figure 6 represents various forms of application of the propulsion units 4 in structures with different geometries.
  • Coil 1 and core 2 may have a global circular geometry as seen so far ( Figures 2.1 and 2.6), or their geometry may also be square, or triangular, or hexagonal, or any other geometry, including composite geometries isolated or interconnected, sharing one or more sides for example.
  • the various coils 1 used may be isolated and independent of each other, or on the contrary, the end of a coil 1 may be connected to the beginning of another coil 1 next or successively, so that several independent toroidal coils 1 behave as a unit, or a rigid or flexible toroidal wire can be used directly which generates a field equivalent to that of the toroidal coil 1, both applied over a large volume or length.
  • Another way to generate forces in dielectrics 3 will be by using coils 1, linear, arranged parallel to each other and separated by dielectrics 3 ( Figure 5.1).
  • propulsion units 4 that can be used and distributed around any mass 5.
  • Propulsion units 4 can be independent or on the contrary be connected together in any distribution or grid .
  • We can also use on all 4 propulsion units any power supply of high or low voltage or pulsed current, including pulses with current derivative or asymmetric voltage. Examples of non-limiting power supplies include Marx generators, inductive current or voltage pulse generators, microwave generators with asymmetric current or voltage pulses, among many other options.
  • Coil 1 may use any solid, or liquid, or gaseous material that is conductive, including gaseous or steam plasmas, or liquids of any material; or including superconducting materials and associated systems. Coil 1 can also use any support material for its physical structure.
  • the core 2 of coil 1 may consist of air or vacuum itself, or any gas at high, medium or low pressure, or any magnetic material, with positive or negative relative magnetic permeability, linear or non-linear, such as magnets permanent, or conductive or non-conducting ferromagnetic or ferrimagnetic cores, or ferrofluids, among other possibilities, that is, any combination of magnetic materials in the solid, and/or liquid, and/or gaseous state, which can be conductive or non-conductive, and with any type of particle or nano- particle in suspension, conductive, non-conducting, semi-conducting, magnetic or any other.
  • the dielectric 3 can be made of any solid, liquid or gaseous material, and may have a positive or negative, linear or non-linear relative permittivity, which will influence the direction and magnitude of the generated force, or even be the vacuum itself or a gas at low or high pressure.
  • This dielectric 3 may be pure or be a symmetrical or asymmetrical mixture of several different dielectrics and may optionally contain embedded within it, symmetrically or asymmetrically, any number of small conductive or semiconducting or non-conducting particles of permittivity or positive or negative, linear or non-linear permeability, such as powder or metallic paint, or magnetic, or semiconductor or other.
  • the dielectric 3 may include the use of piezoelectric materials, or pyroelectric materials, or ferroelectric materials, or metamaterials, or glasses, or quartz, or ceramics, or plastics, or any other type of dielectric. Where the dielectric 3 can also be any matrix composite material, including for example ceramic matrices, among many other possibilities.
  • any of the propulsion units 4 shown can be protected from electromagnetic fields by enclosures of any material, including Faraday cages or metal enclosures.
  • any desired shape for the ship or mass 5 can be used ( Figure 6).
  • the only important factor is the use of one or more propulsion units 4 in order to control the direction of propulsion, which can be on the periphery of the mass 5 or immersed in any position within it.
  • Other variations to be considered will be independent vertical, diagonal or horizontal parts of the ship or mass 5 which may contain propulsion units 4 and be movable and tiltable in any direction.

Abstract

La présente invention concerne un nouveau mode de propulsion aérienne, terrestre, sous-marine ou spatiale, mis au point par utilisation d'interactions électromagnétiques appropriées. Lors de l'utilisation d'une bobine (1) toroïdale, avec noyau magnétique interne (2), il est possible de générer des forces dans un diélectrique (3) placé au voisinage de la bobine (1), par variation asymétrique des champs électriques appliqués à celui-ci, du fait de la variation du flux magnétique présent à l'intérieur de la bobine. Cela est possible grâce à un nouveau mécanisme de propulsion électromagnétique qui utilise la conservation du moment total où la somme du moment mécanique avec le moment du champ électrique doit toujours être conservée, donnant lieu à une somme totale constante et nulle des deux composantes, la variation du moment de champ électrique générant alors un changement correspondant du moment mécanique du diélectrique (3), d'où la génération de forces de propulsion.
PCT/BR2022/050531 2022-01-10 2022-12-30 Système de propulsion utilisant des bobines WO2023130168A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BR1020220004587 2022-01-10
BR102022000458-7A BR102022000458A2 (pt) 2022-01-10 Sistema de propulsão usando bobinas

Publications (1)

Publication Number Publication Date
WO2023130168A1 true WO2023130168A1 (fr) 2023-07-13

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BR2022/050531 WO2023130168A1 (fr) 2022-01-10 2022-12-30 Système de propulsion utilisant des bobines

Country Status (1)

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WO (1) WO2023130168A1 (fr)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6317310B1 (en) * 2000-03-08 2001-11-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus and method for generating thrust using a two dimensional, asymmetrical capacitor module
US6492784B1 (en) * 1999-03-05 2002-12-10 Gravitec, Inc. Propulsion device and method employing electric fields for producing thrust
WO2012053921A2 (fr) * 2010-10-22 2012-04-26 Alexandro Tiago Baptista De Alves Martins Système de propulsion électromagnétique et applications
US10006446B2 (en) * 2015-01-07 2018-06-26 James Wayne Purvis Electromagnetic segmented-capacitor propulsion system
US10513353B2 (en) * 2019-01-09 2019-12-24 James Wayne Purvis Segmented current magnetic field propulsion system
US20210159005A1 (en) * 2020-08-06 2021-05-27 James W. Purvis Pulsed E-field Propulsion System

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6492784B1 (en) * 1999-03-05 2002-12-10 Gravitec, Inc. Propulsion device and method employing electric fields for producing thrust
US6317310B1 (en) * 2000-03-08 2001-11-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus and method for generating thrust using a two dimensional, asymmetrical capacitor module
WO2012053921A2 (fr) * 2010-10-22 2012-04-26 Alexandro Tiago Baptista De Alves Martins Système de propulsion électromagnétique et applications
US10006446B2 (en) * 2015-01-07 2018-06-26 James Wayne Purvis Electromagnetic segmented-capacitor propulsion system
US10513353B2 (en) * 2019-01-09 2019-12-24 James Wayne Purvis Segmented current magnetic field propulsion system
US20210159005A1 (en) * 2020-08-06 2021-05-27 James W. Purvis Pulsed E-field Propulsion System

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