[go: up one dir, main page]

WO2011089481A1 - Procédé de mouvement en trois dimensions - Google Patents

Procédé de mouvement en trois dimensions Download PDF

Info

Publication number
WO2011089481A1
WO2011089481A1 PCT/IB2010/053240 IB2010053240W WO2011089481A1 WO 2011089481 A1 WO2011089481 A1 WO 2011089481A1 IB 2010053240 W IB2010053240 W IB 2010053240W WO 2011089481 A1 WO2011089481 A1 WO 2011089481A1
Authority
WO
WIPO (PCT)
Prior art keywords
movement
vehicle
energy
space
angular momentum
Prior art date
Application number
PCT/IB2010/053240
Other languages
English (en)
Russian (ru)
Inventor
Руслан Николаевич Дейкарханов
Original Assignee
Deykarkhanov Ruslan Nikolaevich
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 Deykarkhanov Ruslan Nikolaevich filed Critical Deykarkhanov Ruslan Nikolaevich
Priority to EA201101043A priority Critical patent/EA201101043A1/ru
Priority to PCT/IB2010/053240 priority patent/WO2011089481A1/fr
Publication of WO2011089481A1 publication Critical patent/WO2011089481A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/409—Unconventional spacecraft propulsion systems
    • 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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/10—Alleged perpetua mobilia
    • F03G7/104—Alleged perpetua mobilia continuously converting gravity into usable power

Definitions

  • the Deikarkhanov method of three-dimensional motion is a method of initiating (at rest and motion) and continuing (including zero speed) the own inertial motion of a material object of any technical purpose in ground, air, underwater, near-Earth and in another permeable the medium of space, the anisotropy of which is determined only by a centrally symmetric gravitational field, in particular the earth.
  • Initiations of the movement of material technical objects contain a common sign of the initiation of movement of a material technical object due to its energy interaction with the surrounding space, as well as when moving by the Deikarkhanov method.
  • the described methods for initiating the movement of material technical objects is a method of following the present gradient of the potential gravitational field.
  • the closest analogue to motion by the Deikarkhanov method is the method of orbital gravitational motion.
  • the orbital gravitational method has an inherent set of features that is closest to the set of essential features of the Deikarkhanov method, which is listed below.
  • TS A technical tool, a material technical object that implements independent movement by the Deikarkhanov method.
  • GTSSP Centrally Symmetric Space the anisotropy of which is determined by the action of those present in space
  • FIG. 1 “The occurrence of a radial driving force” is a drawing illustrating a description of the occurrence of a radial driving force of a gravitational field.
  • a separately moving material particle along an equipotential surface of the gravitational GSCP has an angular momentum relative to the axis passing through the center of the GSCP, which is directed perpendicular to the line of its motion and is equal to the vector product of mass, velocity and radius vector particles in the center.
  • FIG. 1 The final forced particle motion is depicted in FIG. 1.
  • a material particle moves uniformly centrifically in any orbit on the shown pair of orbits from the whole set of pairs of possible ring orbits on an equipotential surface (depending on the magnitude and direction of the force moment).
  • the upper orbit shown in FIG. 1 can be considered as a constant rotation orbit. Evenly filling the entire orbit with equivalent points and connecting them with a rigid connection, we obtain an equivalently moving ring, which for the implementation of this movement is no longer necessary to experience the influence of a force moment of force, since the rigid connection of the material points of the ring eliminates the precession of the Equatorial axis for each point of the ring, compensating component of centrifugal force, see Formula 1, acting on a material particle parallel to the equatorial plane.
  • the three-dimensionality of the GSSP and the central symmetry of the ring exclude the precession of the points of the ring.
  • each point of the formed ring each moment of time has at the same time two components of the angular momentum relative to two axes, one of which is the spatial radial axis, and the second is the prima-Equatorial axis, in the sense one of the axes lying in the primary Equatorial plane.
  • the ring will be in equilibrium if the centrifugal force from the prima-Equatorial component of the angular momentum of each point of the ring is equal to the value, opposite in direction and compensated by the radial force of gravity, and the centrifugal force from the radial component is compensated by the rigid connection of the material points of the ring .
  • the design of the vehicle includes special internal structural elements - propulsors, for example, as shown in the figure depicted in Figure 2 "Location of propulsors".
  • the figure in Fig. 2 shows the location of the propulsors creating the motive force of the gravitational field to initiate the motion of the vehicle by the Deikarkhanov method in any radial and parallel equipotential surface of the space direction.
  • the moment of force of the gravitational field begins to act on the center of mass of the vehicle, initiating the movement of the vehicle along the equipotential surface in the direction of maintaining the radial projection of the axial momentum of the vehicle in the center of gravity.
  • the angular momentum of the TS is perpendicular to the direction of motion of the TS and, therefore, parallel to the prima-equatorial axis of the arising moment of the TS momentum relative to the central axis of the GSCP.
  • the reactive moment of the gravitational field begins to act on the center of mass of the vehicle, which initiates its motion parallel to the axis of the surface component of the intrinsic moment of the momentum of the vehicle in the direction of maintaining the radial projection surface component in the GSCP. Since the TS angular momentum maintains a constant value of its radial projection in the center, then the TS makes the same rotation of its own direction of motion relative to the same axis as the prima-equatorial component of the TS natural moment of momentum and the TS moment of the TS when it moves along an equipotential surface relative to the center GTSSP.
  • the TS makes a controlled turn, the action of the moment of force of the gravitational field perpendicular to the direction of the TS movement and is directed along the equipotential surface of the GSCP.
  • the energy costs of the vehicle’s energy source are equal to the work accomplished by the moment of gravitational force as a centripetal turning force and can be calculated by the uniform accelerated radial rotation of the vehicle if the value of the deflecting moment of the vehicle’s force was constant in time. Those.
  • the TS carries out a controlled change in the direction of its motion along the equipotential surface of the GSCP.
  • the power of vehicle motion initiation depends only on the energy power of the momentum change of the vehicle in magnitude and direction.
  • the TC axial angular momentum maintains a constant direction relative to the radius vector of the GCSP at any point where the vehicle is located, and in the state of stopping the movement and with uniform movement along the equipotential surface, the energy consumption of the vehicle is necessary only to overcome environmental resistance.
  • internal structural elements are movers in such a way that the axis of the momentum of each mover after the start of its operation passes through the center of mass of the vehicle, which allows the vehicle to have its own axial angular momentum equal to the sum of the own axial angular momenta of the working movers.
  • the energy source of the vehicle can be any substance
  • the transport energy of the vehicle is equal to the sum of the kinetic energy of the vehicle and the energy of the axial angular momentum of the vehicle.
  • the initiating power of the vehicle motion in the GSCP is determined by the energy power of the change in the axial angular momentum of the vehicle.
  • the movement of the vehicle by the Deikarkhanov method is initiated when the potential energy of the energy source is converted into the energy of movement of the vehicle.
  • the energy of the TS movement at the moment of stopping is equal to its potential energy in the gravitational field of the GSCP.
  • a TS is capable of instantly starting movement in a GSCP, when its displacement energy is equal to the potential energy of the SC in the gravitational field of a GSCP.
  • the mass of the TS determines the density of the arrangement of equipotential gravitational surface of the vehicle in the direction of the radius vector of the vehicle in the center.
  • the invention recommends converting the potential energy of energy sources into the energy of vehicle motion by those technical methods that provide the possibility of mutual conversion of the potential energy of energy sources of the vehicle and the energy of motion of the vehicle.
  • the direction of the axial angular momentum of the pulse does not affect the ability to initiate and carry out the movement of the vehicle.
  • the vehicles are driven by the Deikarkhanov method.
  • the TS stops its movement in the radial direction on the equipotential surface of the GSCP.
  • the magnitude and direction of the own axial angular momentum of the TS have the ability to establish an adjustable rest of the TS at any point in the GSCP and the resumption of controlled three-dimensional movement at a selected speed in any direction of the GSC using forces, see
  • FIG. 1 “Occurrence of a radial driving force”, is a drawing illustrating a description of the occurrence of a radial driving force of a gravitational field.
  • a material particle moving at a constant speed along a spherical equipotential surface of the gravitational field has an angular momentum relative to an axis passing through the center of the center of gravity and two components of this moment relative to two selected perpendicular spatial axes.
  • FIG. 1 “Location of propulsors.” The figure shows the location of the movers creating the driving force of the gravitational field to initiate the motion of the vehicle by the Deikarkhanov method in any direction of space in a radial and parallel equipotential surface.
  • the energy source of the vehicle can be any external and / or internal energy sources.
  • the energy of all ring movers is part of the vehicle's energy of movement and is transmitted between the ring movers and energy sources through energy conversion devices.
  • the design of the vehicle includes at least two engines of equal power with a radial direction of angular momentum, which are a device initiating and controlling the direction of equipotential movement, and at the same time, with the aforementioned device for initiating and controlling the speed of radial movement.
  • the design of the vehicle includes at least one mover with an axis parallel to the equipotential surface, which is a device for initiating and controlling
  • Stop moving The design of the vehicle includes navigation equipment for spatial stabilization of their own spatial position.
  • the design of the vehicle includes equipment and mechanisms for navigation, for interacting with the environment in motion or during a temporary stop, and for a permanent stop after the movers are completely turned off.
  • the invention recommends converting the potential energy of energy sources into the energy of vehicle movement by those technical methods that provide the possibility of mutual conversion of the potential energy of energy sources of the vehicle and the energy of movement of the vehicle.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Earth Drilling (AREA)

Abstract

Le procédé de l'invention peut s'utiliser dans n'importe quels domaines pour assurer le mouvement contrôlé en trois dimensions d'un véhicule techniques dans l'espace terrestre, marin, sous-marin, aérien, ou orbital dans les environs de la terre ou de n'importe quel système gravitationnel symétrique. Le procédé consiste à transformer l'énergie de l'interaction de l'impulsion axiale propre du couple du moyen technique, avec le champ gravitationnel qui l'entoure, en une énergie de mouvement du moyen technique dans n'importe quelle direction verticale (radiale) ou horizontale (équipotentielle) de l'espace. Le moyen technique utilisant le procédé de l'invention est capable de commencer, d'arrêter, de modifier ou de rapprocher son propre mouvement ou demeurer inactif sans consommer d'énergie dans n'importe quel point d'un espace gravitationnel.
PCT/IB2010/053240 2010-07-15 2010-07-15 Procédé de mouvement en trois dimensions WO2011089481A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EA201101043A EA201101043A1 (ru) 2010-07-15 2010-07-15 Способ дейкарханова трехмерного движения
PCT/IB2010/053240 WO2011089481A1 (fr) 2010-07-15 2010-07-15 Procédé de mouvement en trois dimensions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2010/053240 WO2011089481A1 (fr) 2010-07-15 2010-07-15 Procédé de mouvement en trois dimensions

Publications (1)

Publication Number Publication Date
WO2011089481A1 true WO2011089481A1 (fr) 2011-07-28

Family

ID=44306433

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2010/053240 WO2011089481A1 (fr) 2010-07-15 2010-07-15 Procédé de mouvement en trois dimensions

Country Status (2)

Country Link
EA (1) EA201101043A1 (fr)
WO (1) WO2011089481A1 (fr)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2090404A (en) * 1980-05-22 1982-07-07 Russell Geoffrey Colin A gyroscopic propulsion system
US5279483A (en) * 1990-12-21 1994-01-18 Aerospatiale Societe Nationale Industrielle Attitude control system for a three-axis stabilized satellite especially a remote sensing satellite
RU99121536A (ru) * 1999-10-13 2001-09-10 Эдвид Иванович Линевич Способ запуска космического спутника и его устройство

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2090404A (en) * 1980-05-22 1982-07-07 Russell Geoffrey Colin A gyroscopic propulsion system
US5279483A (en) * 1990-12-21 1994-01-18 Aerospatiale Societe Nationale Industrielle Attitude control system for a three-axis stabilized satellite especially a remote sensing satellite
RU99121536A (ru) * 1999-10-13 2001-09-10 Эдвид Иванович Линевич Способ запуска космического спутника и его устройство

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
ANDREEV A. V.: "Ob absoljutnom dvizhenii protyazhennykh bystro vraschajuschikhsya sistem v gravitatsionnom pole. Raboty K. E. Tsiolkovskogo i nekotorye zadachi mekhaniki kosmicheskogo poleta, Trudy chetyrnadtsatykh Chteny, posvyaschennykh razrabotke nauchnogo naslediya i razvitiju idei K. E. Tsiolkovskogo. Sektsiys", M., IIET AN SSSR, 1980, pages 90 - 95 *
RAUSHENBAKH B. V. ET AL., UPRAVLENIE ORIENTATSIEI KOSMICHESKIKH APPARATOV. IZDTELSTVO "NAUKA". M., 1974, pages 120 - 124 *
VASILCHIKOVA E. N. ET AL.: "Elementarnaya fizika. Spravochnik., M.", STOLETIE, vol. 40, 1996, pages 51 - 54 *

Also Published As

Publication number Publication date
EA201101043A1 (ru) 2012-06-29

Similar Documents

Publication Publication Date Title
US7900874B2 (en) Device to move an object back and forth
US5685196A (en) Inertial propulsion plus/device and engine
Mahboubi et al. Design and implementation of a novel hybrid quadruped spherical mobile robot
Janhunen Electric sail, photonic sail and deorbiting applications of the freely guided photonic blade
Sheng et al. Kinetic model for a spherical rolling robot with soft shell in a beeline motion
WO2011089481A1 (fr) Procédé de mouvement en trois dimensions
Loukanov Application of inertial forces for generating unidirectional motion
RU82277U1 (ru) Устройство для получения силы инерции
CN104679961A (zh) 电磁对接控制方法及装置
US6955235B1 (en) Torque platform transport device
RU2338669C1 (ru) Способ перемещения объекта в космическом пространстве
Provatidis et al. A New Concept and Design Aspects of an'Antigravity'Propulsion Mechanism Based on Inertial Forces
RU2630275C2 (ru) Способ создания тяги и энерго-двигательное устройство для перемещения объекта в пространстве
US20240376869A1 (en) Torque Driven Dynamic Generator with Inertia Sustaining Drive
Khmelnik Levitation of rotating discs
WO2023007579A1 (fr) Dispositif de génération de force de propulsion
Wei et al. Spherical mobile robot driven by biorthogonal omnidirectional wheels
Loukanov Using inertial forces as a source of forward motion
Ciulin System to produce mechanical inertial force and/or torque
Provatidis et al. 2. An antigravity propulsion mechanism
Bergstrom Gravity-assist engine for space propulsion
WO2007084092A1 (fr) Procédé permettant de générer une force de poussée à l'aide des forces de coriolis, dispositif gyroturbine destiné à sa mise en oeuvre et moyen de transport faisant appel à un dispositif gyroturbine
Chase Analysis of a dual scissored-pair, variable-speed, control moment gyroscope driven spherical robot
Rollo et al. The Analysis Of Payload Exchange Failures Between Staged Space Tethers
US20230031448A1 (en) Vehicle propulsion unit and the manner of its operation

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 201101043

Country of ref document: EA

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 10843795

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 10843795

Country of ref document: EP

Kind code of ref document: A1