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 M ₁ ^ meaning M _c = - M^ due the gyroscopic reactions

F^ which value is calculated with the formula : F^ = J ₂ - 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 K ₀ . - — - — — — - — — - — —

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 dot ⁰ angle to the OX axis after new

direction OZ' The force F _p develops the couple moment M _c and the existence of this moment applicable from the exterior on the gyroscope is due to the admission of the kinetic supplementary moment d K ₀ collinear with the moment M _c and then the total kinetic moment will be :

K ₀ = 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 JW ₁ - and angular speed ⁽ D ₁ 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 F ₁ ^ 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 W ₁ - 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 - (D ₁ - 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 O ₀ 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 OD ₁ ±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 = O ₀ O ₁ in the new position O ₀ Zi. 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 O ₂ 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 OG ₂ in the axis sense - OZ.

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

Through the arm rotating GiOG ₂ with the angular speed φ _o yvheτe _^ ^β i _o χ ^β \ an4

(O ₀ L(O ₂ in masses mi and IH ₂ 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 = IH ₂ are situated to equal distances Ri = R ₂ = OGi ⁼ OG ₂ between the centre O and rotate with angular speed ώ _x = - S ₂ perpendicular on the arm GiOG ₂ . 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

ώ ₀ _L ώ ₂ 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 F ₁ ^ 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 = —ώ ₂ of the

whirligigs perpendicular on the angular speed G ⁾ ₀ of the device so S ₀ ± S _x

and<ø _o X ώ ₂ 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 = IH ₂ rotate with the equal angular speed and the same sense S ₁ = ώ ₂ fixed in some forks Gi OG ₂ on the arm situated at the equal distances between the O and Ri = R ₂ = OGi = OG ₂ .

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

vectors of angular rotation S ₀ IlS _x IlS ₂ . Some kind of movement does not modify the angular direction of the vectors G) _x and S ₂ and in this case it does not appear the gyroscopic effect. Because the movement rotation vectors ώ _o llώ _λ llώ ₂ are parallel and

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 ώ ₂ \_V ₂ appear coriolis accelerations <z _cl and tf _c2 and

coriolis forces F _cl andF _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 fi5 ₂ it appears the secondary coriolis accelerations cC _cX and a' _c2 and secondary coriolis

forces respectively and F ^* _cX si F' _c2 where O ⁾ ₁ I. V _t -L tf' _cl and<0 ₂ -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 ώ ₂ 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 V ₁ because this is parallel with vectors G ⁾ _x and G) ₂ meaning (O ₁ HV ₁ and G) ₂ ZfV ₁ 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 m ₂ 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 // ώ ₂ .

There can be built devices with the possibility to vary the vectors position O) _x and G) ₂ between Gt ₀ thus it can obtain the optimal effect.

In the general movement case, 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.

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 - ω ₀ - ω _t

where 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 built device after Fig. Ie in the stationary state when the whirligigs do not function meaning ώ ₀ = ώ _λ = ώ ₂ = 0 will have the rest mass m _s .

In the situation in which the device functions, so ω ₀ ≠ 0, G) ₁ ≠ 0, ω ₂ ≠ 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 ώ ₂ 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 G ₀ 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 _m i = 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.