WO2009102227A2 - Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction - Google Patents

Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction Download PDF

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Publication number
WO2009102227A2
WO2009102227A2 PCT/RO2008/000002 RO2008000002W WO2009102227A2 WO 2009102227 A2 WO2009102227 A2 WO 2009102227A2 RO 2008000002 W RO2008000002 W RO 2008000002W WO 2009102227 A2 WO2009102227 A2 WO 2009102227A2
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WO
WIPO (PCT)
Prior art keywords
mass
movement
assembled
devices
force
Prior art date
Application number
PCT/RO2008/000002
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English (en)
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WO2009102227A3 (fr
Inventor
Dumitru Ionescu
Original Assignee
Dumitru Ionescu
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 Dumitru Ionescu filed Critical Dumitru Ionescu
Priority to PCT/RO2008/000002 priority Critical patent/WO2009102227A2/fr
Publication of WO2009102227A2 publication Critical patent/WO2009102227A2/fr
Publication of WO2009102227A3 publication Critical patent/WO2009102227A3/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
    • 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
    • B64G1/408—Nuclear spacecraft propulsion
    • 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

Definitions

  • the invention refers to a achievement principle of an acceleration movement, of mass bodies so implicitly of some with direction and sense well determined, devices built on base of this movement principle which develop those forces and systems that use more devices of this kind.
  • the present invention shows many bodies systems with mass mi being in the
  • the gyroscope property to maintain the direction of the rotation axis is also used to cannon - balls which are shot with the help of the grooves inside the barred getting a rotation movement to increase the accuracy of shooting.
  • This invention presents the theoretical principle through which a gyroscope or more with rotation axis 6>, are rotated and in a revolution movement to a center with
  • the gyroscopic effect and coriolis effect are movement effect and produce forces and mass effect, the same as inertia forces and centrifugal force, which are also mass forces and we could say that it is the induction mass phenomenon.
  • the gyroscopic effect and coriolis effect produce forces which modify the body mass who produce this effect and act on this mass or can produce gravitational effect at the distance.
  • the invention can be used to the cloud condensation, making controlled rains that can be applied in agriculture, or in military area if the rains are abundant and produce material calamities. With the help of controlled mass forces, strong enough, the clouds can be condensed from a cyclonic atmosphere, controlling thus the evolution to diminish or avoid the damages which they can produce.
  • the invention will be used a lot in the terrestrial, naval and airspace vehicles propulsion, and consequently I will compare it with the existing solutions in this area.
  • the increase of the ejected gases assume a lot of costs of fuel but the fuel reserve of airplanes is limited and then the flight distance of those is also limited.
  • the impulse increases and if the speed of ejected matter also increases, but the burning chemical reactions cannot achieve great ejected jpeeds thus it cannot reach to distructive effects, this situation limited the impulse value.
  • the photon or/and ionic with plasm reaction engines which can develop great thrust forces are not built yet and all the reaction engines assume an ejected mass which it loses in space.
  • the technical problem that the invention solves in the propulsion area is that the thrust mass force results as movement effect in the gyroscope mass and acts without ejecting the mass as it happens to reaction engines.
  • F m • a
  • mass propulsion force depends of an acceleration which generates an accelerated movement of the aerospace ship which in time reaches great speed, values that cannot be achieved by the up-to- date propulsion systems with reaction at which the propulsion force depends on the impulse that is direct proportional with the speed.
  • G of the mass JW 1 - and angular speed ( D 1 situated on the axis OZ has the rotation axis mounted in the bearing from O' and O".
  • - j z is the inertia moment of the gyroscop after OZ axis to the fix point O.
  • - 1 0 0 " is the distance between bearings O' and O' ' .
  • F p is contained in the YOZ plan and OZ' axis is inclined in XOZ plan resulting that those two plans are perpendicular and are intersecting after OZ axis.
  • Fig. Ic is presented the same gyroscope with the O fix point situated in gravity center G of the mass W 1 - in its own rotation with the angular speed G ) x around the
  • whirligig of mass mi in the gravity center G is spinning with the angle speed G> t coaxial with the symmetry axe OZ and the fixed point O 0 is on the OZ axis to a R distance from G gravity center.
  • the complex movement of whirligig changes the angular moving d ⁇ of the whirligig in lineal moving dl t .
  • the present theoretical physics studies the gyroscope movement with the fixed point O gravity center and symmetrical G and sets out the gyroscopic effect, gyroscopic reactions and coriolis effect but it does not study completely the whirligig movement as being a theoretical physics limit.
  • the present invention studies the whirligig movement and Fig.l e, f, g, are presented three particular cases of whirligig movement and subsequently makes a generalization of this movement and sets out the movement effect which appear, resulting the movement principle subdued to patent.
  • whirligig device If in this moment it is not necessary it can be statically balanced, stiffening the whirligig device or it can be dynamically balanced providing this device with many whirligigs or/and gyroscopes thus positioned and with movement and constructive characteristics thus chosen so their moments to balance dynamically.
  • the arm spins with the angular speed G ) 0 which is parallel with the others two
  • the vectors S x and S 2 are all the time transported in parallel plan with the speed V 1 and V 2 because G ) x _L V x and ⁇ 2 ⁇ _V 2 appear coriolis accelerations ⁇ z cl and tf c2 and
  • the ⁇ leadery is F ⁇ x and F ⁇ 2 oppl)mifpCTfuTbatron ⁇ fofces F pl and
  • the angular speed O 0 , G ) x and G) 2 are neither parallel nor perpendicular having any directions in space and in this case it can obtain the gyroscopic effect and coriolis effect but this general case we have not represented graphically because it can be derived from others particular cases.
  • J 2 is the inertia moment of the gyroscop after OZ axis and G) 0 is gyroscopic angular speed of revolution rotation movement and G) 1 is its own gyroscopic mass angular speed and I 0 O" is the distance between the holders.
  • the mass force is oriented in the sense and on the direction of coriolis acceleration and is an active force generating an accelerated movement and is not a reactive force as the inertia force which is opposed to the accelerated movement.
  • the devices built according to the invention are based on the composition princioles of presented movement as in Fig.l a, b, c, d, e, f, g.
  • a built device after the movement principle as in Fig. Ie and f develops active mass forces which determines the acceleration movement of the device without exchanging of mass with the exterior.
  • a device with the rest mass built as in the principle scheme from Fig. Ig if it is weighed after the OY and OZ axis will have the equal masses but grater than rest mass m s i mean m s ⁇ m y m z .
  • the device In the fiinctioning state the device generates the mass force F n ⁇ and weighed after OX axis will have m x mass grater then the rest mass m s and after that direction -
  • OX will have the In x " jnass smaller than the rest mass ⁇ ⁇ i x > m s > m x " .
  • the principle according to the invention is based on a theoretical discovery which refers to mass induction through which the mass of a body is modified trough movement effects as mentioned in the relativity theory, as the mass alternates with the speed which means movement.
  • the theoretical principle according to the invention indicates what kind of movements are responsible of the mass alternation and on the basis of this theoretical principle are obtained mass forces which can be used in various areas.
  • the mass acceleration is in fact a gravitational acceleration and the mass force is in fact a gravitational force.
  • the acceleration and mass force developed by those devices and achieved systems based on these devices according to the invention generate in fact a force after a line of mass field which is a component of the gravitational field and produces at the distance gravitational effects on the direction of the field line of the mass force.
  • the mass force can be of attraction or rejection along the field mass line and a mass centre in water vapour cloud determines the condensation of the raindrops generating the artificial rain.
  • a repulsive mass force and a repulsive mass centre in a water vapour cloud leads to the dispersal of the raindrops and of the cloud.
  • a directioned mass force after a field line and focused on a body with the mass can attract that body or it can reject it depending on haw mass force is the attraction or rejection. So a device like that fixed on the ground which can generate a mass force directioned on a flight plane it can attract it or shoot it down or it can push it projecting or changing its direction.
  • the trajectory of the satellites, airspace ships and so on, can be modified from distance with the help of this mass force. It results that the present invention has a large using area.
  • Those masses can be solid, fluid, gaseous or plasm bodies.
  • Tokamak plasm installations with the help of a magnetic toroidal field is configured toroidal and this tor of plasm spins in the installation, behaving like a rotation mass.
  • the positive ions from plasm have a bigger mass than the free electrons and in this case the calculation is made taking into account the positive ions (atoms and molecule) mass, which can bring them to untouchable relativist speed in mechanical installations and in this case it imposes as an efficient solution.
  • the torodoidal plasm installations are used to nuclear reactors and such an atomic reactor presume using of a cooler fluid brought in the vapour state which will act a turbine, subsequently the vapour are recycled in the atomic reactor.
  • the turbine rotor mass in rotation will act as a whirligig and consequently the turbine rotor must be built and positioned as in Fig. 1 f __ —
  • Fig. 2a and b is presented a device in accordance with the invention which was conceived on the base of the principle from Fig. If and theoretical considerations developed earlier.
  • Fig. 2a is presented the section AB and in Fig. 2b section CDEF through such a device.
  • This device is comprised of body 1 where are mounted two atomic reactors R A si RA' with identical parameters where the toroidal plasm 2 circulates reversal to the plasm 2' from the other reactor.
  • the plasm is toroidal configurated between the coils 3 and 3', and the reactor is cooled with the cooler installation 4 and 4' where the working fluid is transformed in high pressure steam which is collected in the high pressure steam collectors 5 and 5' which are link together through the link tube of the high pressure steam 6 thus the steam pressure from two collectors 4 and 4' is equally.
  • the high pressure steam from the collectors 5 and 5' through some nozzles is led to the turbines blades 7 and T on the turbine rotors 8 and 8' on which are assembled the turbine axes 9 and 9' .
  • the turbine axles 9 and 9' drive a generator of compound current from the rotory coils of electric generator 14 and 14' mounted on the axles 9 and 9' and in body 1 is mounted the stators of the two current generators 15 and 15'.
  • the toroidal plasm 2 the working fluid from the cooler installation 4, turbine 8 and current generator spin all of them in the same sense but to simplify the drawing I figured only the angular speed G) x .
  • the reactor RA' is identical with the other reactor and for all the elements in rotation mentioned earlier I figurated only the angular speed G) 2 equal, parallel and contrary with angular speeds, .
  • the device axe at an end has a fixation piece 19 which spins in body 1 and at the other end has a fixation piece with fork 20 which spins also in body 1 and in the fork is mounted the cardan crass 21 from which is mounted the cardan fork 22 fixed on the fixation base 23.
  • fixation base 23 can be a base fixed in the ground.
  • the mass force built by the such a device has a direction and a sense-applied to ⁇ the movement mass by the whirligig and at the distance acts like a atractional gravitational force on a sense and mass rejected force on the other sense of direction.
  • the attraction mass force through the distance on the body mass which meet them on that direction attracts on the device, those bodies could collide with the device which can be destroyed. To avoid such destructive situations it could achieve systems with many devices which can have the parallel mass force, convergent, divergent or a direction in the effect that we desire to obtain. With the help of those devices on the airships we can realize an artificial gravitational field necessary to build life similar on the Earth. D.
  • Fig.3 is presented an embodiment of a system with four devices according to the invention from which three are identical drawn at 1, 2 and 3 in drawing disposed at the equal distances in the corners of the equilateral triangle ABC with the gravity center in G point.
  • the triangle plan ABC is perpendicular on the OG axis on which is found an airspace ship 5. These three devices 1, 2 and 3 are mounted thus the mass
  • the pilots bodies cannot support and is mounted the device 4 which generates mass force F m4 with a direction value and sense chosen depending in the necessity to create an optimal gravitational acceleration, supportable by the people who are on aerospace ship board.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

La présente invention se rapporte à la hausse théorique de certains mouvements complexes ayant généré des accélérations de direction et de détection bien déterminées, résultant d'un principe d'accélération de direction. L'invention concerne également un dispositif d'accélération de direction basé sur le principe de l'invention. Grâce aux dispositifs de l'invention, il est possible de concevoir des systèmes de dispositifs d'accélération de direction. La physique théorique réelle, basée sur la théorie de la relativité, étudie l'espace, le temps et la masse corporelle en mouvement dans des systèmes d'inertie physique, sans accélération de mouvement. Le principe d'accélération de direction résulte d'un mouvement général d'accélération d'un corps et l'analyse a en outre été étendue à au moins deux corps à mouvement synchronique. Les zones terrestres, navales et aérospatiales sont les zones présentant une praticabilité maximale. Sur la base du principe théorique issu de la présente invention, on peut concevoir de nombreuses solutions constructives, mais la solution constructive choisie est celle de la figure 2 a, b, qui a pour base le principe théorique de la figure (formule (I)). Ce dispositif se compose d'un corps 1 où sont assemblés deux réacteurs atomiques RA et RA' aux paramètres identiques. Dans le réacteur RA, le plasma toroïdal 2, le fluide de travail provenant de l'installation de refroidissement 4, la turbine 8 et le générateur de courant tournent tous dans le même sens, mais pour simplifier le dessin, seule la vitesse angulaire ϖ1 est représentée. Le réacteur RA' est identique à l'autre réacteur et pour tous les éléments en rotation énumérés, seule la vitesse angulaire ϖ2 égale, parallèle ou opposée à la vitesse angulaire ϖ1 est représentée. Pour toutes les masses en rotation ayant pour vitesses angulaires ou ϖ1 ou ϖ2 et afin de produire des effets de masse, l'ensemble du dispositif tourne à la vitesse angulaire ϖ0, perpendiculairement aux deux vecteurs précédents (formule (II)). L'invention peut être appliquée à un ou plusieurs dispositifs d'accélération de direction, ce qui permet ainsi d'obtenir des systèmes de dispositifs d'accélération de direction. La figure 3 représente l'utilisation, sur un aéronef, d'un système de trois dispositifs identiques, disposés dans le coin d'un triangle équilatéral et ayant développé la force de pression nécessaire au vol, et d'un quatrième dispositif produisant des effets locaux de gravitation sur les hommes qui se trouvent à l'intérieur de l'appareil, l'accélération à laquelle ils sont soumis devant être maintenue à un niveau confortable.
PCT/RO2008/000002 2008-02-12 2008-02-12 Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction WO2009102227A2 (fr)

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PCT/RO2008/000002 WO2009102227A2 (fr) 2008-02-12 2008-02-12 Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction

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PCT/RO2008/000002 WO2009102227A2 (fr) 2008-02-12 2008-02-12 Principe d'accélération de direction, dispositifs d'accélération de direction et systèmes de dispositifs d'accélération de direction

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018095505A1 (fr) * 2016-11-22 2018-05-31 Nurgaliyev Zhan B Propulsion par gravité basée sur un principe d'induction par gravité

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509899A (en) * 1983-03-28 1985-04-09 Frederick Larry J Traversing blade-rotary propeller
RU2120061C1 (ru) * 1997-07-10 1998-10-10 Илья Иванович Лаптев Плазменный двигатель
US6279314B1 (en) * 1998-12-30 2001-08-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. Closed electron drift plasma thruster with a steerable thrust vector
US20040240998A1 (en) * 2001-08-06 2004-12-02 Eric Ashworth Fluid flow control mechanism
WO2007084092A1 (fr) * 2006-01-20 2007-07-26 Yuriy Makarovych Lykhovyd 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

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509899A (en) * 1983-03-28 1985-04-09 Frederick Larry J Traversing blade-rotary propeller
RU2120061C1 (ru) * 1997-07-10 1998-10-10 Илья Иванович Лаптев Плазменный двигатель
US6279314B1 (en) * 1998-12-30 2001-08-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. Closed electron drift plasma thruster with a steerable thrust vector
US20040240998A1 (en) * 2001-08-06 2004-12-02 Eric Ashworth Fluid flow control mechanism
WO2007084092A1 (fr) * 2006-01-20 2007-07-26 Yuriy Makarovych Lykhovyd 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

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
GORELENKOV N N ET AL: "Toroidal plasma thruster for deep space flights" AIAA JOURNAL AIAA USA, vol. 41, no. 5, May 2003 (2003-05), pages 774-784, XP008098164 ISSN: 0001-1452 *
HALL T W: "ARTIFICIAL GRAVITY AND THE ARCHITECTURE OF ORBITAL HABITATS" JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY, BRITISH INTERPLANETARY SOCIETY, LONDON, GB, vol. 52, no. 7/08, 1 July 1999 (1999-07-01), pages 290-300, XP000828681 ISSN: 0007-084X *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018095505A1 (fr) * 2016-11-22 2018-05-31 Nurgaliyev Zhan B Propulsion par gravité basée sur un principe d'induction par gravité

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