The principal new element of the invention is the fact that the superior discoidal turning platform (12) solidarilly with flange (17) and the superior frame(25) as the inferior discoidal turning platform (13) solidarilly with flange (28) and the inferior extern frame(32), are not compact indestructible mass but are made up by assemblage - but with a radial level of liberty - by equal couples of circular crown sectors diametrically opposed located (preferentially grouped by four or six according to the size of the vessel by much more couples for each turning platform) each couple in a turning movement (on contrary directions) generate centrifugal forces tending to remove them (by expandation) from instant relative turning centre.

Each couple of sectors being located symmetrically and diametrically opposed generates centrifugal forces with the same size and diametrical opposed by their direction having the original centre placed on vertical symmetrical axis (z-z) of the whole functional system and being functionally connected through a hydraulically connection of energy and force.

Between the exterior frames and the turning platforms which compose each of them one circularly crown sector being constructively located: goods, food stock, fuel and liquid symmetrically placed at equal quantity in each discoidal sector through volumic segment of circular crown which form together the two turning circularly platforms (12) respectively (13).

Those centrifugal forces are put together from all sectors with a radially grade of liberty which constitute the two turning platforms due to the hydraulic amplifier of force and energy (21) with the same shape and construction with the genuine part presented in the [2 page 279] linked by which links all those circular crown sectors generating by putting together for each turning platform symmetry of the whole functional system (z-z), vertically orientated and on a contrary direction to gravitation as shown in Fig.(4).

 
 

 
 

Fig.4

The addition, the amplification, the auto-centralisation and the progressive an concomitant annulment of stokes are realised with the progressive increase of revolution. In contrary direction of the two turning platforms, the technical processing is realised especially due to the effect of the banded plane (breakdown) existing in the amplifier of energy and force (2) mentioned and similar with the one described and presented in the [2 pag. 152 - 156], picture from pag. 279 and represented as the place on the cinematic scheme of the whole system from Fig. Nr. (3), genuine parts (21).

So, as the mass of has circular crowns put together and combined in a turning platforms is bigger, as the area is bigger as the angular turning speeds (w) respectively revolution (n) is bigger so as the forces accumulated (Ec.tot) due to rotation being added and accumulated and conserved by the superior platforms (12) and the inferior one (13) will be bigger. The kinetic energy stocked will be directly proportional with the same parameter proportional with motor (Cm) rotator generated by the flow of gases from the two burning chambers opened - in the isobar evolution - at a constant pressure (4) and (5) [statoreactors] diametrically opposed and fixed at the extremity of the fix stationary platform.

Centrifugal forces diametrically opposed [linked between them by the hydraulical circuits with force an energy] generated by the volumic sectors of diametrically opposed circular crown are those dozed and permanently controlled through an hydraulic command system integrated and the pressure generated by the hydraulical auxiliary pump controlled from the cockpit by a remote control, two assisted engines One of them on each turning platform - amplify and reduce till annulment and weight of the central discoidal system respectively of the platform (1) through a transfer in action of the weight of this one from the vertical direction - as kinetic energy on horizontal plane of rotation of the two turning platforms, conform cinematic scheme of Fig. Nr.(3) and graphic representation of Fig. Nr. (4).

Another new element of the invention in that due to the big diameter of the radial centrifugal compressor unique the steps, through the alimentation of this by the air that gets in the first step by of compression through the holes (26) uniformly distributed on the superior frame(25), is obtained also a specifically uniform depression distribute on the surface of the superior frame25, in obtained also a specifically uniform depression distribute on the surface of the superior frame which depression has as immediate effect a tendency of absorption up of the whole functional system.

So, supposing that the exterior diameter of the superior frames 12 meters then 1200 cm an the internal diameter in 2 m then 200 cm, thus, the specifically depression is (-0,01) ) [kg.f/cm²] it will result a frame active surface superior (25) of around 1.099.000 cm² , multiplied with 0,01 it results an ascensional force which reduce the total weight at the taking off with around 10.990 kg, which is not small because at the taking off, all the genuine parts are solicitated in the maximum.

Another new element of that invention is the regime of flight in the atmosphere at a high speed seems necessary and constructively favourable. The opportunity of alimentation of the reactive burning chambers (4) respectively forced admission of air which is naturally compressed in front of exterior frames (35) respectively (32).

So, the natural and caught compressed air at the surface of admission relatively very big (similar to a convergent piece approximately rectangular or square but divergent due to the curved cylindrical surfaces) get in towards the statoreactors through the holes (27) uniformly distributed on the circumference superseding the compressor by the controlled of the opening or the closing of the inelar diaphragm (36).

That technical combined solution of feeding permanently the necessary an sufficient quantity of air for combustion as far as it is known at very high altitudes the air density necessary for the combustion considerably decrease, anyway, due to the possibility of the admission and the obtention of the air from big surfaces, and constructively profiled, some big debits respectively big quantities of air can be provided due to the natural compression.

Comparatively, the classic turboreactors and statoreactors currently used in the aircraft industry do not benefit of that big constructive advantage because of the relatively reduced surface of the admission filters which are severely restricted constructively because of their reduced diameter.

Also as a big advantage and at the same time favoured and also as an innovating aspect of that invention is the fact that turning of the superior(12), and inferior (13) frame in the contrary direction, and the displacement at the superior speeds (greater than de 1000 m/sec). The natural air compressor located in front of the direction of the promotion can be optimised and increased by a radial shaping of the extremity in zone of the orifice of admission (27) - in relief – and adequate to those two rotating carcass, the naturally compressed air from the front of the displacement direction being in this way obtained, directed and captated toward the centre from the horizontal plan of the entire system where the natural compression of the air has the maximal value.

The big tangential speed (Vt) necessary of the ranged in steps blades of the centrifugal compressor unique in steps that are constructively interpenetrated, are very easy to perform practical and of of the revolution particularly reduced of the rotating of the disks (6) and inferior (7) solitary each of them with the rotating platform (12) respectively (13) according to the relation (Vt)=3,14.D.n/60)[meters/sec] where (Vt) is the tangential speed of the rotating platform, (n) is a rotating platform revolution in [rot/min], and (D) is the average diameter of the blades location, so by example if the revolution (n)=200[rot/min] and (D)=15[meter] it results; (Vt)=3,14.15.200/60 = 157 [meter/sec] but as the two turning disks blades (6) respectively (7) have contrary rotating direction it results Vt=314(meter/sec) entering already in the supersonic regime.

That supersonic speed obtained at a only 200 [revolutions/min] revolution is sufficient to perform comparatively, relations of compression favourable, practical – according to the desire, being able to perform very easily the aimed scope due to the tangential speed. They can be lightly increased and – with no constructive restriction – by enlarging the circumference or by the light increase of the rotating platform revolution.

The most important innovation of this invention is characterised by the fact that by this proceeding of construction of the hole functional system, after the taking off, the flying saucer can still be propelled and by <crossing> also named inertial displacement in zigzag, the displacement observed quite frequently to some UFO-s, that displacement having as consequence an acceleration more and more big reaching some unimaginable speeds because by that principle the light speed does no more represents the speed limit. Practically that principle of displacement concomitantly superposes to the proceeding previously described by the following supplementary successive commands like this:

- Commute the rotation centre of the turning superior platform (12) – at the extremity of the latter, this thing being possible practically by the temporary coupling and of the a very short duration of the superior platform (12) with the stationary platform (1) at the same point from the extremity located at the distance (d) by the sabots (S1) respectively (S2) for the inferior platform (13) having as the immediate result the obtention of one force that pull all the system towards.

That force is made evident by the Theorem of Steiner from the physics, the theorem that is applied to the movement of a body that is moving rotatively like this: knowing the value of the inertia moment that passes through the centre or of the mass noted with (I) we will have; (I)=1/2.M(R.+r.),

where:

• (M) is the mass of the body as a cylindrical ring,
• but (R) and (r) are the exterior radius and the interior radius of the platform,

the moment of inertia can be calculated  respectively calculating similarly the kinetic energy u where (w) is the angular speed, it results that at another instantaneous centre of rotation located on the axis of rotation (z1-z1) parallel, the moment of inertia (I1) is much bigger comparatively with the moment of inertia (I) conserved at the kinetic moment respectively in the kinetic energy (Ec) accumulated and conserved by the training in the rotation of the two turning platforms, the kinetic available energy having a very big value and being able to liberate hardly instantaneously and is in a mechanical working (LM)=(Ftsupl.D).

But as D (Ec)=(LM) the supplementary force of traction value can be established (Ftsupl) resultant as effect of the coupling of the sabots (S1) and analogous for the inferior platform by the coupling of the sabots (S2).

Like this, by the repeated manoeuvre, commanded and controlled from the binnacle, the whole functional system displace inertially <<advancing>> in zigzag increasing like this progressively the speed of the displacement and with the great advantage that in case of using the electromagnetic braking by the help of the two coupling sabots (S1) respectively (S2) the electric energy can be obtained (also the forming the electromagnetic field of force that can perturb sometimes some electric networks from the sol by the superposition of the frequency).

Due to the fact that the kinetic energy gathers up and conserves itself in the two turning platforms independently to the linear speed reached on the trajectory at given moment and can be liberated in the form of mechanical activity respectively the traction force, displacement by the inertial going in zigzag, can lead by this proceeding to a continuous increase of the displacement speed of the whole system independently from the combustion gas speed value that leave combustion chambers at the constant pressure (4) respectively (5).

But as the combustion gas the letting out speed of which are limited, in the exchange, the transmitted energy by the former and the reason why they can be used permanently to the training in the rotation movement of the two turning platforms (12) and (13).

In this way this proceeding of inertial displacement in zigzag on the outer space permits to achive some linear and progressive speeds on the trajectory bigger and bigger, respectively impossible to imagine because the light speed does no more represents the upper limit.

Related to this proceeding of displacement in zigzag that superposes concomitantly above the basic proceeding increasing like this the performances and the manageability of the whole system, during the displacement in the terrestrial field of gravity, another innovation appears characterised by the fact that the inertial displacement in zigzag can be accelerated and moreover by an supply of kinetic energy liberate by the potential energy of the central platform (1).

Those energy can communicate between them through the amplifiers of forces and energy (21) commanded and hydraulically connected between them, but of course with rapid loose in height but above all when certain purposes are deliberately desired and other purposes, - this thing (the displacement in zigzag and in very rapid dive), the trajectory and the displacement by those proceedings superposed simultaneous being particularly difficult to establish and to locate as possible purpose when they are desired by somebody because of the very big degree of manageability of the entire system during the flight.

Another innovation of this invention is the fact that for the displacements in the outer extra-terrestrial space there exist sufficient volumes in the turning sectors that constitute the two turning platforms (12) respectively (13) where sufficient liquid oxygen can be deposit and liquid hydrogen and with the advantage that those one can be especially used at very high altitudes and in the outer space, apart from this in the atmosphere saving by the way the oxygen as liquid hydrogen or any other combustible mixture used for the propulsion in the outer space.

Another innovation of the invention is characterised by the fact that the feeding and dosing system of the combustible is specialised and constructively adapted to this invention due to the existence of two possibility.

The first possibility consists on the injection of the combustible indirect through a secondary circular combustion chamber usually composed of two cavities of small volume, separate by the de grating (15), practised in the disks (6) respectively (7), [to make air-tight by labyrinth] and communicates by the ceramic tubes of link with the two principle fix combustion chamber (4) respectively (5) mounted to the extremity of the fix platform (1).

In this case the injection of the stored combustibles in the volumic turning sectors that composes the turning platforms (12) respectively (13) can be achieve through some injectors and valves of dosing mounted on the turning disks (6) respectively (7) and act by telemechanical remotes from the binnacle (2).

The second possibility of feeding the two combustion chamber is simpler and consists in the bringing of the combustible by the link mobile pipe which start from each volumic sector of circular crown where the combustible is stored to the two central fix collecting pipes on the central platform (l), respectively one above for the collecting from the circular crown sectors that compose, by the assembling with a degree of radial liberty, the superior turning platform (12) that rotates in the contrary direction.

The collection of the combustible becomes possible due to the fact that the fix collecting pipes are located on the rotation axis (z-z) above and below the binnacle (2), the hydraulically link being achieved through the two hydraulic extremities constructively similar with the hydraulic extremities of the injection turning pumps used in diesel engine.

Let us mention that in case of the displacement in the outer space the feeding with the oxygen necessary to the combustion and that can be stored in some of the volumic turning sectors can be achieved similarly as the feeding with the combustible.