Thus, by the repeated manoeuvres, 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), electric energy can be obtained (due to that, sometimes electromagnetic fields may appear that can perturb sometimes some electric networks from the sol by the superposition of the frequency,- due to the resonance’s ).

      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 zig-zag can be accelerated and moreover by an supply of kinetic energy liberated by the potential energy of the central platform (1).

      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 (kerosene) used for propulsion in cosmos, the heating being performed at constant presion (turboreactors).

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

      The first possibility consists on the injection of the combustible indirectly through a secondary circular combustion chamber usually composed of two cavities of small volume, separated 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 achieved 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 in the case of feeding with the combustible after air admission at the heating room is closed; that heating room will turn to the regime of constant pression heating, - under the functioning regime of a rocket motor.

-      the symmetrically discoidal construction and robust with aerodynamic form;

-      the detachment from the de earth very easily even in the case of some dimensions and weight very big;

-      comparatively for the same total weight at the taking-off (Gt), this proceeding of propulsion, construction and functioning can dispose constructively by the new system of the propulsion with a traction force of at least ten times bigger than the existing classic solutions and used in the present, the classic flight objects known being considerably surpassed as performance and manageability due to the fact that this invention permit the circulation of some particular and big debit of air in a time unit, respectively directly proportional, - the very big traction forces on the horizontal in the condition in which the lift on the horizontal become null through the elimination of the gravity influence above the flying object;

-      the progressive increase possibility, continue and practically unlimited of the displacement speed and by the successive and continue accelerating due to the possibility of inertial displacement in zigzag, making possible the crossing of some enormous distances in a relative short time at speeds bigger than the light speed.

-      the possibility of remaining in sustentation at fix point, indifferently of the altitude;

-      the possibility of landing and taking-off at a fix point, without special arranged flight strip;

-      the possibility of taking-off and exiting with very big facilities to the cosmic outer space of a flying saucer of very big dimension due to the propulsion of big power, respectively of superior performances and of the propulsion that permits a mixed feeding respectively with oxygen and liquid hydrogen, inclusively the atomic energy, in this way being able to create real flying towns for interplanetary travels.

-      the possibility of creating an artificial gravity in the case of vessel of very big dimensions through the arrangement of some living spaces even in the volumic sectors of which are composed the turning parts in case of the displacement in cosmic outer space. The gravity obtained by this artificial way may be put under control depending on how it is increased or decreasded the turning speed, enabling by this way even very long trips in cosmos.

-      the invention includes the propulsion made by 2 new original type and identical reactive propulsors having a very big power and the building possibility of working according to the needs under 3 different ways respectively, like turbo reactory engines - in atmosphere, like statoreactory engines - at high altitudes, or like rocket engines at high altitude or in cosmos.

-      another great advantage is that the solely combustion chambers of those two universal propulsories are placed outside of the coaxial compressor turbine and are feeded with the air needed by the heating, compressed from a single centrifugal special compressor, having radial steps with double effect, and very big diameter (several metres).

-      the advantage of using a single centrifugal compressor, with radial pression steps and double effect ( pallets frontally interference and in contrary senses ) is that this compressor will be able to ensure very big air flows at very high compression rate and with direct favourable influence over the traction forces (Ft); Example: Ft = η_g.Q/V_H where (η_g) is the global efficiency , (Q) is the heat quantity obtained by heating the mixture of fuels, (V_H) is flight speed at a given altitude. The heat quantity is pending on the air flow Ga=S.V where (S) is the passing section and (V) is the speed of the air flow thru the respective section.

-      the obtaining of some very big specific traction forces because of the lack of building restrictions at the passing sections like in the case of the above mentioned classical turbo reactor engines which are much limited in their performances mainly due to this aspect. Example ;(F_sp) the traction performed by an air flow of (1 kg/sec) defined by the relation F_sp = Ft/Ga [daN.s/kg] where (Ft) is the performed traction force and (Ga) is the air flow passing through the engine, and it is the same result respectively the traction force increases proportionally with air flow (Ga) that passes through the engine within the time unit. Consequently, the passing sections which influence the getting of very big air flows, respectively very big traction forces, are no more restricted in the building field as compared to the classical turbo reactor engines.

-      the possibility of recovering, as mechanic energy, of an important part of the heating gases energy which are released by the turbine pallets after the end of each relaxing phase; those gases have a higher pression than the atmospheric pression and a quite high temperature respectively a kinetic energy which is waisted. Example: by use of the proceeding of this invention this disadvantage is partially put away on basis of the principle of action and reaction of forces. The exit pression (Pe)>(P_athm) that is acting like a specific pression on the whole section, like a surface of gases exit from the heating chamber, generates a supplementary traction force with direct influence over the global efficiency ( ng) respectively also over the fuels consumption according to relation Fsupl=pe.S(kgf), assuring concomitantly both horizontal traction and the rolling in contrary senses of the two rolling platforms respectively involving the feeding compressor.

-      the turbine pallets are no more attacked all simultaneously by the hot teating gases, but only tangentially and only on a single side. By this way, the cooling periods of the turbine pallets after a complete rotation become very big because the number of pallets from the circumference is also much higher, the result being that each turbine palette works at temperatures much lower a enabling the possibility of dissipation of the heat, the turbine pallets taking over them much higher mechanical pressions. It is also notable that the materials used in this proceeding and the output technologies are by far much cheaper.

-      the overcoming of the gravitation and the getting terrestrial orbital place ( at the functioning of the two propulsors of the flying saucer as rocket engines ) can be achieved very easily without using of any supplementary launching rockets, and when entering again the atmosphere, the propulsion can be also used easily to for getting a brake or a total stopping and stationing in sustentation - without being necessary a special termic protection of the exterior carcasses.

-      according to this proceeding, the flying saucers are able to move concomitantly and in zig-zag and with a continuous and progressive speed of the whole functional system, independently of the flow heating gases speed ( which is, however, limited ) through the efuzors.

-      in the economic point of view, in the national plan, the applying in the life of the invention through the standardising in the country of flying saucers inclusively for the exit and the travelling in the outer space, creates the possibility of the massive and immediate attracting of foreign assets (of many billions of dollars) through mixed companies, the immediate activation of some spaces of production from industrial platforms -, the activation and use of the superiorly qualified and available labore of research and design, the creation of a big number of jobs, the increase of the economic power of the country and the increase of the living standard, the establishment and the maintaining of a monopole above a new ultra rapid system of international transport of persons and goods, the increase of the Romanian national prestige all over the world etc.