The problems solved by invention, are characterised by the fact that they are referring to the construction, functioning and displacement procedure of a flying saucers with very special performances, processing which can match more technical solutions which leads to a final result characterised by the fact that it’s can create a new kind of transportation vehicles with the same construction, functioning and displacement procedure who seems to be older but modern in the same time: exactly what has been done till now.

To understand the invention, it is known that there is a force named centrifugal force created by the rotation movement of an object around his own axis or around a stabile (fix) point named rotation centre. This force, when used in a certain manner can lead from the reduction to the adulation of gravitation and – not only as I will show later in an example the composition, the description and the function of some flying saucers conform to some cinematic schemes presented in fig.(3):

-A flying saucers according to this invention is made of three functional and inter-dependent main genuine parts which are: the main central non-turning system, a superior turning system and an inferior system inverse-turning as compared to the superior one. Both having the same vertical symmetrical axis (z-z) which are respectively one instant centre of relative rotation for each one and one weight centre located on the same vertical axis of symmetry (z-z) as shown on the cinematically scheme on Fig.(3);
 

- The central discoidal mean - or central domes - is made up of the central circular platform (1) which turning speed around the vertical common symmetrical axis (z-z) is, usually near zero. On this platform solidary with that usually located in the command cabin [cockpit] (2) and the living beings, supports of taking off -landing (3), at the extremity and diametrically opposed a heating chamber on constant pressure - reactively identical with a statoreactor, respectively on the left (4) and on the right (5) sides, excepted goods, the fuel and a part of the used propulsive system which are located on the two others main turning systems on which are fixed turning discs (6) and (7) where are fixed and which are radial and successively inter-combined the blades (8) and (9) of a stepped unically radial centrifugal compressor with double a effect and with the same symmetrical axis (z-z) of the whole system, turbine blades (10) and (11).

- The auxiliary equipment and the liquid stocked oxygen for the displacement in the cosmos etc. are located on the order two discoidal system as a turning-platforms: a superior one (12) and an inferior one (13).

The two heating chambers at a constant pressure -reactive (statoreactors), which are respectively that located on the left (4) and that located on the right (5) are fixed on the extremities of the fixed circular platform (1) which continues towards the exterior through the profiled grill (15) and assures an half (1/2) of the traction force on the horizontal plane (Ft), the heating gases of the chamber (4) assuring concomitantly and leading gases by the movement of the superior turning platform (12).

This phenomenon takes place due to the hitting of the turbine blades on the whole superior disc area of the platform (6) that is forming one piece with the turning superior platform (12) so, (Vt= 3,14.r.n/30) [meters/s] where (Vt) is the tangential speed - (r) the location area of the blades of turbine and - (n) is the revolution in (rot/min) of a turning platform and burning gases leaving the heating chamber at a constant pressure (5) assuring the leading to the unity of the inferior turning disc with the superior one.

The radial slipped unique and centrifugal compressor with a big medium diameter insures a neatly superior relation of result of compression due to the breaking (senssoring) of air at 90 grade which flows at a very big tangential compression separated only by the stationary (15) with uniform holes (16) radially and on 45 grades optimal angle on horizontal plane and profiled.

The stationary circular profiled grill (15) constructively links towards the exterior the whole area of the fixed central platform (1) and has the same symmetrical axis (z-z) with the whole system.

The main advantage of using this type of compressor which is constructively used for this invention is the fact that, due to the high number of blades of each radial step of compression of the compressor which uniformly distributed on a very big area allows long cooling times on a complete rotation; which leads to the thermal reloading of turbine blades (10) and (11) located towards the exterior leads not to constitute an important technical problem as it is the case of the axial turboreactor compressor currently used in aviation.

- The discoidal superior system made up of the superior discoidal turning platform (12), has got the same instant rotation centre relatively located on the vertical symmetrical axis (z-z) of the central platform (1) and approximately the same exterior with the possibility of rotation around the vertical symetrical axis (z-z) and common to the three platforms forming the whole system.

It is also composed the superior flange (17) made of many couples of circular crowns sectors with the possibility of being rotated on bearings (18) located towards the interior and fixed on the superior turning platform (12) made up also of couples of circular crown sectors. At the interior part of the superior flange (17) is located the fix flange (19) welded at the interior of the cylindrical frame(2) of the cockpit.

On the fix flange (19) the compact disc (20) can be rotated by slipping on which is fixed at radial direction and with a radial of liberty [radial shift Fig. (3)] hydraulically amplifiers of force and energy (21) which are made of pistons (22) with vertical symmetrical axis and the piston (23) with the symmetrical axis on the horizontal plane and acted through the bearings systems (24) with a vertical symmetrical turning axis on the interior diameter of the fix static flange (19).

Also solidarilly with the superior turningplatform (12) is fixed the superior exterior frame(25) on which are protected (previewed) admission holes uniformly distributed (26) and the evacuation - admission holes also uniformly distributed (27). At a non working position when the superior turning platform doesn’t rotate the stokes(a) are zero same are the stokes(b).

- The discoidal inferior system made up of the discoidal inferior turning platform (13), which is similarly as description with the superior discoidal platform (18) with the difference that flange (18) is constructively overtaken by the bearings (29) placed this time at the inferior turning platform (13).

flange (30) is identical and fix like the flange (19) and the compact disc (31) is identical with the compact disc (20). On the inferior turning platform (13) the inferior frame(32) is solidarilly fixed which is based on the bearings (33) similarly to the (18) bearings. At the down part of the central cylinder [cockpit] (2) is located the access ramp (34) and on the upper part windows (35).

Because of the stability reasons on the horizontal plane, the inferior turning platform (13) will always have a bigger total weigh (at a stationary position) [the total weight centre of the old functional system always has to be under the weight centre of the central platform (1) to maintain the stability], on the turning direction will always be contrary to the turning direction of the platform, being correlated and permanently controlled by the rotation speed of the discoidal turning platform (12).

Through a controlled dosed of traction forces developed by the two heating chambers at a constant pressure (reactive engines) each one placed diametrically opposed at the stationary central platforms extremities, (1) permanently sustained without any turning movement but with the possibility of changing horizontal plane of the whole system through a suitable dosage of fuel and of diametrically opposed and of the same direction of the forces of traction making possible the brake of the whole system by a controlled rotation of the fix platform (1) [which doesn’t rotate as compared to the other platforms (12) respectively (13)] at an 180 grades angle compared to the initial walking direction.

The fix platform (1) stability against non-controlled rotation being constructively assured due to the controlled dosage of traction forces in the horizontal plane and diametrically opposed to which actions at the extremities of the platform (1) obtained from the burning chambers at a constant pressure (statoreactors) (4) respectively (5) even at a big distances as compared to the turning axis (z-z), the resulting couples of rotation - reciprocally adulating themselves.