WO2009102227A2

WO2009102227A2 - The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems

Info

Publication number: WO2009102227A2
Application number: PCT/RO2008/000002
Authority: WO
Inventors: Dumitru Ionescu
Original assignee: Dumitru Ionescu
Priority date: 2008-02-12
Filing date: 2008-02-12
Publication date: 2009-08-20
Also published as: WO2009102227A3

Abstract

The invention refers to raise theoretical some complex movements which generated well determined direction and sense accelerations, resulting an acceleration direction principle, and on the base of the principle it describes an acceleration direction device and with the help of many of these devices, it can conceive devices systems with direction acceleration. The actual theoretical physics on the base of relativity theory studies space, time and body mass in movement in physical inertness systems, without accelerate movement. The direction acceleration principle results from an acceleration general movement of a body and the analyse was extended to two or more bodies with synchronical movement. The terrestrial, naval and aerospace will be the areas with maximal practicability. On the base of the theoretical principle from the present invention, it can conceive many constructive solutions, but I opt for the constructive solution from Fig. 2 a, b which has to the base the theoretical principle from Fig. If where Formule (I). This device is compound from body 1 where are assembly two atomic reactors RA and RA' with identical parameters. In the reactor RA, the toroidal plasm 2, the working fluid from the cooler instalation 4, turbine 8 and current generator is spinning all of them in the same sense but to simplifying the draw i figured only the angular speed ϖ1. The reactor RA' is identical with the other reactor and for all the elements in rotation enumerate subsequent i figurated only the angular speed ϖ2 equal, parallel and contrary with angular speed ϖ1. For all these mass founded in own rotation with angular speeds ϖ1 or ϖ2 to produce mass effects all this device is spinning with angular speed ϖ0 perpendiculary on these two vectors i mean Formule (II) Term of applications can be used a single direction acceleration device or more devices resulting direction acceleration

Description

THE DIRECTION ACCELERATION PRINCIPLE,

THE DIRECTION ACCELERATION DEVICES AND

THE DIRECTION ACCELERATION DEVICES SYSTEMS

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.

Presently there are known different body movements in systems, devices and engines that develop acceleration and forces with direction and sense and well determined for example; pressure forces of working fluids, mechanical forces of expansion and compression reaction forces from reaction engines of flying airplanes, coriolis forces and so on. hi relation to acceleration and coriolis force, the theory presents the case of a body with mass mi which spins with an angular speed G⁾ _t around its symmetrical axis

in fact a gyroscope, and the^"Totation^~vector #>7 is moved parallel plan with the

translation speed V_t where those two vectors are perpendicular <», _L V_t and in this

case appears the coriolis acceleration a_c perpendicular on the other two vectors

meaning G⁾ ₁ _L V_t _|_ a_c .

Physics theory determined that if on the rotation axis G⁾ _i of a gyroscope it acts

with an perturbation force F_p perpendicular on the rotation axis inclining the direction of rotation axis G⁾ ₁ with the angle dβ° then the gyroscope axis inclines with the angle

dα° in a perpendicular plan on the force F_p phenomenon named gyroscopic effect.

Also if the rotation axe G⁾ ₁ of gyroscope spins with angular speed ^β>_o where

G⁾ ₁ -L ^β>_o then it appears a force couple gyroscopically resistent F^ which produces a

resistant gyroscopic moment M_rg with an opposite sense to G⁾ ₀.

So the perturbation forces ^ develops a couple M_c which twists the gyroscope

axe G⁾ ₁ with the speed G⁾ ₀ and this couple is equal and has an opposite sense with the

resistent gyroscopic moment M₁^ meaning M _c = - M^ due the gyroscopic reactions

F^ which value is calculated with the formula : F^ = J₂ - G⁾ ₀ . ^Q) ₁

The present invention shows many bodies systems with mass mi being in the

movement of their own rotation G⁾ ₁ and in their own revolution G⁾ ₀ movement compound that generates a gyroscopic and coriolis effect with accelerations, respectively gyroscopic and coriolis forces with direction and sense oriented in space after a direction and in the desired sense so that those forces can be used in different areas.

In the situation in which the two rotation vectors G⁾ ₁ and G>_O are oriented after two_ certain directions, then in_such a.movement. appears also the corriolis effect^and. gyroscopic effect and consequently two effects must be analysed altogether.

In present it is used only the property of gyroscope to maintain determined the

rotation direction G⁾ ₁ and on the base of mis property there were built so named gyroscopes used in navigation as aircraft instrument to indicate all the time one direction.

Those applications are based on the gyroscopic resistent moment and they are some transducers which show the position of a body in space, they are not aggregated by the force which generates forces or/and moments which can be used in different areas.

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.

Other areas of utilization of the gyroscope are not known and i do not know any area where the coriolis force is used.

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 angular speed &>_o case in which appear the gyroscopical reactions, gyroscopic effect or / and coriolis effect, generated effects continuously after a direction and a sense well determined, constant in time, this theoretical movement principle being the basis of presentation of an embodynment of the invention named device with acceleration and directioned forces and systems using such devices.

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.

^~ These forces are always oriented ^"after^" aT direction and a predetermined constructive sense if on their direction they meet a material body with mass, produce upon this at a distance, a gravitational force inverse proportional with the distance

square — according to the gravitational attraction law F_g = G- ¹ ₂ ² . In this

situation the invention has a large using area in military and civil area.

In transportation area it can be used to terrestrial, naval and airspace vehicle propulsion. As distance effects, 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.

A mass force powerful enough, directed from the ground to a flight plane it can attract it and shoot it down, so it has a military application in the military area.

It results the application areas are varied, some of then undetermined, and in some areas the invention is the only way to obtain the desired effect, so it cannot exist some other alternatively technical solutions to solve that problem.

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.

From these I consider that the mass propulsion, based on gyroscopical and coriolis mass forces will be indispensable in the space transportation area at long distances.

The thrust force of reaction engines used presently in aerospace area, depends on the impulse P of the ejected gases which is given by the product between speed V and mass m of the ejected gases, P = m • V, and to increase the impulse is neccesary to increase the mass or/and ejected gases speed. 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.

The mass force is calculated with the relation F = m ^• a where the gyroscope mass m suffers a gyroscopical acceleration ^a _g or a coriolis acceleration #_c In the case of cosmic transport to long distances acquiring a mass force without mass ejection is the only solution to achieve great speeds and in this case the principle and the solution from this invention are very important and even indispensable.

With the help of the total mass invention of aerospace vehicle will be made from the flight vehicle mass and the nuclear fuel mass which are transforming with great yield in the necessary energy to action the mass propulsion device and in space will be ejected only the nuclear waste from the reactor which are in a small quantity.

Another major advantage of mass propulsion is that the 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.

The other applications which refer to the action at the distance of the mass force which is in fact the gravitational force governed after a direction and a the desired sense cannot be compared because there are not solutions that can be compared.

A. In Fig. 1 a, b, c, d, e, f, g. Exhibit from theoretical point of view the gyroscopic and coriolis effects.

In Fig. Ia the gyroscope with O fixed point in the gravity center G and with mass mi in its own rotation with angular speed G>_t in rotation around the symmetry axis OZ having the kinetic moment K₀ . - — - — — — - — — - — —

If upon the rotation axe OZ we act with a perturbation force F_p parallel with

OY axis Trying to incline with the angle dβ° in a new position, simultaneously with the gyroscope axis which will incline with the dot⁰ angle to the OX axis after new

direction OZ' The force F_p develops the couple moment M_cand the existence of this moment applicable from the exterior on the gyroscope is due to the admission of the kinetic supplementary moment d K₀ collinear with the moment M_c and then the total kinetic moment will be : K₀ = K_c + άK_c and it will correspond with the new rotation axis OZ' .

This physical phenomenon is ended with the rotation axis of the gyroscope with the angle dα ° after OZ' axis is named gyroscopic effect.

But the inclination OZ axis produced by the gyroscopic effect with the angle dα° after new direction OZ' presumes an gyroscopic overset moment produced by the gyroscopic effect M^ about which the theoretical physics does not make any reference being a limit of the present physics.

According to physical theory any moment is due to a force which acts to on an

arm so the gyroscopic effect moment M_eg is due to a force of a gyroscopic effect F_eg that the theoretical physics does not underline but the present invention underlines the existence of that force and it applies it.

In Fig.l b, the same gyroscope with the fixed point O is situated in the barycentre

G of the mass JW₁- and angular speed ⁽D₁ situated on the axis OZ has the rotation axis mounted in the bearing from O' and O".

To incline it with the angle dβ° the gyroscope axis or to spin it with the angular speed G⁾ ₀ collinear with the OX axis where the two rotation speeds are perpendicular

G>i ±.<n_o there are necessary the perturbation forces F_p ' and F_p " and simultaneously in the bearings O' and O" emerge two equal and contrary forces with these

perturbation forces, named gyroscopicaϊ reactions F₁^ which oppose the inclination of the gyroscope axis.

Perturbation forces respectively gyroscopic reactions are calculated with the formula:

rg = |F>μ F' where:

/ oV

- 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' ' . Besides the gyroscopic reactions emerge the gyroscopic effect which tends to modify the axis rotation direction after OZ' axis inclined with the angle da° to the OZ axis, so 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.

The gyroscopic resistent moment M_n, given by the gyroscope reactions is along

the OX axis and the gyroscopic effect M_eg is along the OY axis so these two moments

are perpendicular M_n, JL M_eg and in this case the gyroscopic effect force F_eg is also

perpendicular on the perturbation force F_p i mean F_eg ± F_p

In Fig. Ic, is presented the same gyroscope with the O fix point situated in gravity center G of the mass W₁- in its own rotation with the angular speed G⁾ _x around the

symmetry axis OZ. If it is applied from the exterior the perturbation force F_p on the direction of OY axis and the gyroscope will be moved with the V_t speed to a new

position O' and because the transportation speed V_t is perpendicular on the rotation

speed CD_x it appears the coriolis effect and namely the acceleration^ and coriolis

force perpendicular^ on the others two vectors i mean #>, J_ F, JL <z_c and

G>i A-V_t ±F_c which tend to move the OZ axis with the distance dl_c after the new direction Oi Zi.

Coriolis acceleration is calculated with the formula a_c = 2 - (D₁ - V _t and coriolis

force with the formula r_c = m_t ^• a_c .

In the situation when the fix point O there is not in the G gravity center of the mass mi the gyroscope is a whirligig and we will study his movement.

In Fig. Id, 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 O₀ is on the OZ axis to a R distance from G gravity center.

If we spin the whirligig with the angle speed ω_o and the two angle speed are perpendicular i mean OD₁ ±ώ_o then OZ axis will incline and with the dβ° angle and mass m_c will be moved from G point to G' with the distance dl movement made with V_t speed and because the vectors G⁾ ₁ and V_t are perpendiculars meaning ώ_t± V, it

appears the coriolis acceleration tf_c and coriolis force F_c which will move OZ axis

with the distance di_e = O₀O₁ in the new position O₀Zi. But for the axis O_c to be inclined with the angle dβ°, simultaneously appears the gyroscopic effect and the gyroscopic reactions which tend to incline the axis OoZi with the angle dα° thus the new axis Gi Zi will be incliner with this angle after the direction O iG ₂-

In the situation when the arm OG is rigid this would not allow the axis inclination

OZ with the angle dα due to the gyroscopic effect and in this case the fix centre Oi will be moved with the distance dl_g after the direction O₂ Z ₂.

That result the whirligig device will be moved also with the distance di_e due to the coriolis effect and with the distance dl_g due to the gyroscopic effect and it results the total moving dl_t = dl_c + dl_g.

Concretely the complex movement of whirligig changes the angular moving dβ of the whirligig in lineal moving dl_t.

Coriolis force F_c and gyroscopic effect force F_eg being collinear will gather and

will result the force F_m = F_c + F_eg which is total mass force of the two effects.

Because in nature the conservation of energy law is respected then the necessary energy overcoming the moment given by the gyroscopic reactions which are equal and

contrary with the perturbation forces moment F _p must be equal with the mass

force F_m which are moving the mass mi on the distance 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.

Before I showed that the gyroscopic effect tends to inline the rotation axis OZ in a new inclined position with the angle dot to the initial position so the gyroscopic

effect generates an overset moment M_eg of the rotation axis.

hi the situation which the perturbation forces F_c continuously act the gyroscopic

effect will be also generated continuously and in this case the moment M_eg tends to rotate continually the OZ axis in a new position

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.

In Fig. Ie, we extended the arm OGi with the arm OG₂ in the axis sense - OZ.

On the arm GiOG₂ there are mounted two whirligigs with the masses W; and m.₂ situated to the equal distances Ri = R₂ = GiO = OG₂ between the center O and they are contrary G⁾ ₂ rotating on this arm.

Through the arm rotating GiOG₂ with the angular speed φ_oyvheτe_^ ^βi_oχ^β\ an4

(O₀ L(O₂ in masses mi and IH₂ will exert the perturbation forces F_pl = - F_p2 situation which will determine the gyroscopic effect and coriolis effect in every of these masses mi and 1^2-

Because the two whirligigs are identical and are mounted in the mirror, the parameters G⁾ _x , G)₂ and F_pl , F_p2 are equal and contrary, the gyroscopic effect moments being equal and contrary are balanced in the same as coriolis force moments,

but the two mass forces F_ml and F_m2 being equal and with the same sense will gather resulting the total mass forces F_mt = F_mX + F_m2 which tends to move the device on the OX axis direction.

In Fig. If , the two whirligigs identical with the masses mi = IH₂ are situated to equal distances Ri = R₂ = OGi ⁼ OG₂ between the centre O and rotate with angular speed ώ_x= - S₂ perpendicular on the arm GiOG₂. In the situation when the arm rotate around the O point with angular speed O)₀ coaxial with OX axis where cό_Q _L ώ_x and

ώ₀ _L ώ₂ develop the perturbation forces F_pl and F_p2 which produce gyroscopic and

coriolis effect forces, respectively the mass force F_ml and F_m2 in this case the force

moments between the O is balanced but the resultant of mass force F₁^ summing up those two mass force along OX axis and tends to move the device along of this axis. So the movement from Fig. Ie and f with angular speeds S_x = —ώ₂ of the

whirligigs perpendicular on the angular speed G⁾ ₀ of the device so S₀ ± S_x

and<ø_o X ώ₂ determine the appearance of some mass forces whom resultant F_mt is coaxial with OX axis and determines the devices movement.

This is the theoretical principle through which it obtains the mass resultant force with direction and sense oriented after an imposed direction which can be used in different activities areas.

In Fig. Ig, the two identical whirligigs with masses mi = IH₂ rotate with the equal angular speed and the same sense S₁ = ώ₂ fixed in some forks Gi OG₂ on the arm situated at the equal distances between the O and Ri = R₂ = OGi = OG₂.

The arm spins with the angular speed G⁾ ₀ which is parallel with the others two

vectors of angular rotation S₀ IlS_xIlS₂ . Some kind of movement does not modify the angular direction of the vectors G)_x and S₂ and in this case it does not appear the gyroscopic effect. Because the movement rotation vectors ώ_o llώ_λllώ₂ are parallel and

the vectors S_x and S₂ are all the time transported in parallel plan with the speed V₁ and V₂ because G⁾ _x _L V_x and ώ₂ \_V₂ appear coriolis accelerations <z_cl and tf_c2 and

coriolis forces F_clandF_c2 where F_Λ = -F_c2 .

In this situation, the coriohs accelerations being turn to the rotation centre of O device, are centripete accelerated and coriohs forces respectively F_cX and ^_c2 are

centripet forces, so in thus device the mass force is given by the coriolis force F_cl and

F_c2 which being equal and contrary are nullified.

In the situation in which the vector G⁾ ₀ is antiparallel with the vectors G⁾ _x and

G⁾ ₂ it is obtained a coriohs centrifugal accelerations and respectively centrifugal coriolis forces.

The movement from Fig. Ig in which appear centripete coriolis accelerations and respectively centripet coriolis forces diminish the centrifugal forces which appear in the device, during functioning time, favorable situation which can be used to drafting and achieving of such devices with great performances.

In the situation in which assambles as those in Fig. Ie are moved along the OX axis with V_t speed, this being perpendicular on the rotation vectors^ and fi5₂ it appears the secondary coriolis accelerations cC _cX and a'_c2 and secondary coriolis

forces respectively and F^* _cX si F'_c2 where O⁾ ₁I. V_t -L tf'_cl and<0₂ -L V_t -L tf'_c2 •

m Fig. Te, the^{^}secundary is F\_x and F\₂ oppl)mifpCTfuTbatron^~fofces F_pl and

F_P2 which rotate the device and together give a couple which appose the device rotation with the angular speed fi>₀ situation which diminish the transport yield.

The assambly from the Fig. If if it is moved with the V_t speed this being perpendicular on the vectors G⁾ _x and ώ₂ appear the coriohs secundary centripetal

accelerations 5'_{cl j} a\₂ respectively coriolis secundary centripetal forces F^% _cλ and

F\₂ which are perpendicular on the moving direction OX does not oppose to the movement, the solutions being optimal from the point of view of the transport yield. The assambly from the Fig. Ig if it is transported with speed V₁ because this is parallel with vectors G⁾ _x and G)₂ meaning (O₁HV₁ and G)₂ ZfV₁ does not appear the secundary coriolis acceleration and neither the secundary coriolis force.

It results that the variant from the Fig. If is the optimal variant in case when the device moves with a V, great speed.

In Fig. Ie and f the gyroscopic mi, and m₂ rotate with angular speed G⁾ _x and G)₂ which are perpendicular on the angular revolution speed G)₀ meaning G)₀ ± O⁾ _x

and<^y _o -L^₂ and in Fig.lg angular speed are parallel G⁾ ₀ // G⁾ _x// ώ₂ .

There can be built devices with the possibility to vary the vectors position O)_x and G)₂ between Gt₀ thus it can obtain the optimal effect.

In the general movement case, the angular speed O₀ , 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.

The gyroscopic effect force and coriolis force being mass forces they are

computed on the basic of the general formula F = m - a where m is the whirligig mass and the acceleration a must be an acceleration based on the gyroscope mass m and it is computed from the general formula of gyroscopic reaction F_rg = J_z - ω₀ - ω_t

where J₂ 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 I₀O" 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 built device after Fig. Ie in the stationary state when the whirligigs do not function meaning ώ₀ = ώ_λ = ώ₂ = 0 will have the rest mass m_s.

In the situation in which the device functions, so ω₀ ≠ 0, G)₁ ≠ 0, ω₂ ≠ 0 and we weigh such a device after OX axis this device will have a greater mass m _x than the device in rest m_s i mean m _x > m_s.

In the situation in which we weigh the device after - OX axis this device will have the mass lower than the device mass in the rest m_s > m_x ^~ and so

m_x ^" < m_s < m_x . In the situation in which the mass force F_nit is greater enough this can cancel the device weight which rises up from the ground.

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.

A device built as in Fig. If in the rest state has the mass m_s.

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^ πi_x > m_s > m_x ^". This device in the functioning state weighed after OY and OZ axis will have equal masses m_y = m_z but greater than the state mass Iϊl_s i mean m_y = m_z > m_s due to secondary

coriolis forces F' _cl and^'_c2 .

Practically 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. Moreover 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.

Through the focalization of many forces and mass field lines it obtains in the intersection point a mass centre which produces gravitational effects. 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.

In some areas there are other alternative solutions but are also some areas where are not alternative solutions to solve those problems and in this case the actual invention is the only way to solve this kind of problem.

The theoretic principle as the invention allows a better understanding of the gravitational field and the internal structure of elementary particles representing a progress in development of theoretical physics which allows realization of some atomic fusion reactors or/and atomic fission of great efficiently. In connection with the movement principle presented in Fig. If, I make an analysis of the possibilities to achieve such a device with acceleration and oriented force as the invention says.

From the point the view of the building up any device with the acceleration and mass forces oriented presumes the existence of some rotation mass with an angular speed.

Those masses can be solid, fluid, gaseous or plasm bodies. In 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.

In the situation when we mount two installations with toroidal plasm in rotation as in Fig. If it will result the mass force F^ which projects this device and it can be acted from the distance.

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 __ —

Also the working fluid of the reactor found in fluid and gaseous state in the reactor installation will have a rotation movement in the same sense with the rotation movement of turbine.

In this situation results a device which has in the component installations with toroidal plasm and turbines which work together resulting a constructive solution optimal that to a spaceship deck will produce also the mass force for propulsion and electrical energy necessary to function the ship. This double utilization of the device according to the invention diminishes the aerospace ship mass and leads to the increase of the transport efficiency. In the situation when at taking off are necessary bigger propulsion forces it can build aerospace ship having reactive propulsion systems as those used in present and with devices with the mass propulsions as these described in this present invention or on the ground are mounted some kind of devices which help the ships take off.

B. In 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.

In 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' .

Over the turbines with the help of fixations elements 10 10' are mounted the turbine caps 11 and 11' having chambers to collect the low pressure steam 12 and 12' and which the help of pump systems and working fluid transfer 13 and 13' sends back in the cooler installations 4 and 4' of those two toroidal reactors and the working fluid cycle is repeating.

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'.

In the reactor RA, 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, .

For all these masses found in their own rotation with angular speeds G)_x or ώ₂ to produce mass effects all this device spins with angular speed G⁾ ₀ perpendicularly on these two vectors i mean G)₀ ± G)_x and G⁾ ₀ JLo)₂ . The device can spin with angular

speed G⁾ ₀ it must have rotation axe of 16 device electrical engine stator 17 and in the body 1 of the device where is mounted the exterior coils of the rotor 18 of the electric engines, this having an inverted construction.

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.

In the situation where the device according to the invention is used to the propulsion of a spaceship fixation base is itself the body of the ship. If the device is used for example to produce artificial rains, fixation base 23 can be a base fixed in the ground.

C. It can be used a device or many devices creating a device systems.

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. In 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

forces F_{mλ y} F_m2 and F_n^ should intersect in a common point O situated in front of the airspace ship and form whit G axis the angle γ°. In this case the mass forces of attraction attract material bodies from the O point to one of the three directions OA, OB or OC thus it will obtain a dispersion of matter to points A, B and C and the ship with the gravity center G₀ is situated on the axis OG forwarding to the directions OG to meet less material bodies or not at all lowering thus the collision risk of material bodies and in the atmospherical flight the air will be thinner thus the aerodynamic shape will be less important.

An airspace ship to fly in the straight line those three forces must be equal

F_mi = F_m2 = F_m3 and their resultant F_m = ( F_mλ + F_m2 + F_m3 ) • cos γ° is situated on the OG axis realizing the ship propulsion and the transversal components

F_mλ _L F_m2 J_ F_m3 _]_ F_m • sin γ° which are perpendicular on the fly direction OG realise the matter dispersion.

To change the flight direction is necessary that those three mass forces-should not" be equal, obtaining thus an other resultant force F_^, oriented after another direction, respectively other flight direction.

If the aerospace ship moves with great accelerations 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.

Claims

1. The principal movement of the bodies following those resulting the accelerations and mass forces with imposed direction and senses can be used in practical applications, consist in a whirligig or many whirligigs of the mass Di₁ found in its own rotation with angular speed G)₁ which spins in a revolution movement with the angular speed G⁾ ₀ ^an(i ^m the general movement case of the two vectors G⁾ ₁ and G⁾ ₀ are oriented on any directions in space or in the particular movement cases of these being perpendicular or parallel meaning G)₁ LG)₀ or G)₁ //ώ_Q movement which appear accelerations and mass forces with the directions and sense pre-established used in different areas.

2. Device which generates accelerations and mass forces realized on the bases of the principle claiming to the 1 point, and connected with Fig. 2 a and b characterized through that is composed of a body 1 in which are assembled two atomic reactors identical, with the toroidal plasm 2 and 2' having a coils systems 3 and 3 'and cooler installations 4 and 4' in which circulates a working fluid system which is transformed in steams, collected in steam high pressure collectors 5 and 5' which communicate between them trough the link tube 6 equalizing the steam pressure which through nozzles is directed to the turbine blades 7 and7' fixed on the two turbine rotors 8 and 8' assembled on the turbine axes 9 and 9'.

Over the turbine with the fixation elements help 10....10' are assembled those two turbine caps 11 and 11' which inside them create the collecting chambers of the steam of low pressure 12 and 12' in which is assembled the pump systems and the working fluid transfer 13 and 13' which pumps the working fluid back in the cool installations 4 and 4' of the reactors and the working fluids cycle repeats. On each axle of the turbines is assembled a coils of the electric current generator rotors 14 and 14' and in the device body is assembled the coils of the stator of the electric current generator 15 and 15'. All the device spins around the rotation axle of the 16 device with the help of the electric engine of the compound inverted from the coils stator electric engine 17 assembled on the device axle and the exterior coils rotor of the electrical engine 18 assembled in the device body and an the device axle at an end is assembled a fixation piece 19 which spins in the device body and at the other end, the axle is provided with the fixation piece with the fork 20 which spins all in the device body.

All the rotation mass of each reactor spins in the same sense G⁾ ₁ respectively G)₂ , ^d because the rotors are assembled in the mirror these vectors are antiparallel but equal as absolute value G)₁ = ώ₂ and for those two reactors that are identical the total mass in rotation will be the same meaning mi = m₂. All the device spins with angular speed which is perpendicular on the others two angular speed G⁾ ₀ i mean

G)₀ _L G)_x and G)₀ _1_ ώ₂ movement which generates two parallel and equal mass forces

F_m\ = F_m2 and their resultant will be a mass force F_mt coaxial with the rotation

vector G)₀. For the orientation of mass force F_mt in the desired direction, on the axle fork is assembled cardan cross 21 in the cardan fork fixed 22 which is assembled on the fixation base 23. _____

Cardan articulation allows the orientation device on the desired direction with the help of a mechanic, electric, hydraulic or/and pneumatic adequate mechanism.

The changing of the sense of mass force F_mt can be made of by the changing of the rotation sense of the vector G⁾ ₀ .

3. The devices systems according to the invention characterized through as two or more devices are working together thus the attraction mass forces or rejection generated by this devices are directed after the parallel axis, antiparallel, convergent, divergent or some directions, obtaining mass effect different depending on the necessity including the creation of the artificial gravitational field in the system.

4. The devices systems according to the invention with Fig. 3 characterized trough that is compound from four devices of which three devices identical 1, 2 and 3 are disposed to equal distances in the corner of an equilateral triangle ABC with the gravity center in G point and on the OG axis perpendicular on the triangle plan ABC is situated the airspace ship 5 which has the gravity center G₀ found on the OG axe.

These three identical devices will generate the mass forces F_{ml j} F_m2 and

F_m3 which are oriented thus their direction is focalized in the O point forming with OG axis with the angle γ° and in this case the projections of these three mass forces on

the OG axis will sum up resulting the total mass force F_mt which has the application point O situation which creates the flight direction stability and the transversal components of those three mass forces F_mI-IP_m2-LF_mS realizes the dispersation of some material bodies and rarefaction the atmosphere on the flight direction, and for the change of the flight direction the balance is broken for the three mass forces thus their

resultant F_mt will have another direction and the spaceship will change the flight change.

On the airspace ship is assembled at least a device 4 which generates the mass

force F_m4 which creates in the ship a gravitational acceleration similar to that on the Earth for achieving optimal life conditions for the travelers on the spaceships.