More specifically, the invention concerns the definition of the construction technique of the rotating bodies animated with rotary motion with respect to their longitudinal axis, installed in hydraulic radial turbines operating according to the dynamic effect known as the Magnus effect.

In the text, with the expression radial turbine it is indicated a turbine with an axis of rotation at right angle to the direction of the working fluid.

As is well known, there is a correlation between the spin of a rotating cylinder with respect to its longitudinal axis and the fluid stream which strikes said cylinder in a direction perpendicular to said longitudinal axis. Such a correlation has been described, in 1852 for the first time, by HG Magnus, and for this reason it is called the Magnus effect.

This correlation is highlighted on the lateral skirt of the cylinder with a force, called "lift", in a direction perpendicular to the lines of flow of the fluid stream, and rotated in a clockwise or counterclockwise direction with respect to said stream, depending on the direction of rotation of the cylinder; more in particular it is rotated in a clockwise direction when said cylinder rotates counterclockwise and it is rotated in a counterclockwise direction when said cylinder rotates clockwise.

Quantitatively, the modulus of the lift L (expressed in N/m) , per unit length of the cylinder, is given by the equation of Kutta-Joukowski , and is equal to the product of the density of the fluid p (expressed in kg/m ³ ) , for the asymptotic speed V ₀ of the fluid threads (expressed in m/s) , ie the speed of the fluid threads where the same move undisturbed, and for the circuitry Γ (expressed in m ² /s) .

In formulas, if the cylinder has radius R

(expressed in m) , the lift due to the Magnus effect is determined by the relation:

L = p ·V ₀ = ρ·ν ₀ ·2π·ω·Ι¾ ² = 2n · p -V ₀ · (ω -R ² )

This relation is independent from the shape of the profile, ie it is valid for any profile, by profile being meant the contour of the rotating body along a section plane passing through the rotation axis of the rotating body.

The U.S. patent No. 1,674,169 assigned to the Instituut vor Aero-Hydro-en Dinamiek, inventor Anton Flettner, describes several possible applications of Magnus effect, in particular as "sails" for a boat and as "blades" of a wind generator and presents various alternative embodiments of the rotating bodies, including in particular the cilindric shape (in the patent several boats are shown equipped with a "sail" constituted by a cylindrical rotating body) , the ellipsoidal shape (referred to only in a figure relating to a boat without describing its peculiarities) and a shape consisting of two frustoconical portions mutually connected by a cylindrical portion (also in this case without any description that specifies dimensional relationships between these portions) .

On the basis of this first patent and other subsequent patents, Flettner installed, on a boat with tonnage of 1000 tons, two Magnus effect rotating cylinders, 2.75m in diameter and 15m high, driven by two electric motors of about 40kW, with a spin of 750rounds/min, and made its maiden voyage leaving from Hamburg (March 31, 1926) and arriving in New York (May 09, 1926) (A. Flettner, "Mein Weg zum Rotor" 1926) .

J. Cousteau, in 1985, equips its ocean-going vessel in the same manner as the Flettner rotoship, with a variation due to his own patent.

In 2009, the German Enercon, one of the largest manufacturers of wind turbines, launched a cargo ship, 130m long, 22.5m wide and with 10500 metric tons deadweight (DWT) , equipped with four Magnus effect cylinders 25m high and 4m in diameter, to integrate, with a saving of 40%, the traditional propulsion propellers .

Parallel to the development of devices aiming at exploiting the Magnus effect and based on cylindrical bodies rotating around their axis and arranged in a fixed position relative to the ground and more in general with respect to the power plant to which they belong, turbines using the Magnus effect have been developed with axis of rotation of the turbine being parallel or perpendicular to the direction of the working fluid.

Among these, US patent No. 1744924 describes a radial turbine using the Magnus effect, in which a plurality of rotating cylindrical bodies, with axes of rotation parallel to each other, are housed between two frames, arranged on planes parallel to each other and perpendicular to the axes of said rotating bodies, the lift generated by each rotating body being transmitted to the frames and carrying them in rotation about a common axis of rotation, parallel to the axes of rotation of the rotating bodies.

Similar solutions are shown in French Patent No.608280, as well as in the International PCT application No. WO2009/018524 , which are also related to radial turbines using the Magnus effect, in which the rotating bodies, always of a cylindrical shape, are arranged between two plates mutually parallel and perpendicular to the axis of said rotating bodies.

In the years between 1930 and 1950, Marco Todeschini studied and experimented the Magnus effect and finally edited "La Teoria delle Apparenze (Spazio- Dinamica & PsicoBiofisica) " , published by Istituto Italiano d'Arti Grafiche in Bergamo in 1949, as well as "Psico-Biofisica" , Ed. Centro Int. di Psicobiofisica, Bergamo, 1949, setting out an innovative interpretation of Magnus effect based on dynamic considerations and corroborated by experiments made in a ship model basin; determining that the effects of attraction and repulsion which are observed on two cylinders parallel to each other, and due to their rotation about their respective longitudinal axes, are connected to the inertia of the earth: that is, the spin of the Earth.

With the aim to give a more general ustification of this theoretical-experimental thesis, it is possible to imagine that a rotating body reached by a fluid moving in a direction transversal with respect to its axis of rotation is driven by inertial forces activated by the Magnus dynamic process, and, in turn, considered and mathematically explained in the theorem of circuitry of Kutta-Joukowsky, revisited according to a relativistic interpretation.

This may reasonably mean that the one-dimensional theory based on a reference system only coaxial with the longitudinal direction of the flow is not sufficient, since it does not consider the rotational movement of the Earth, ie the "Campo Centro-Mosso" (CCM) , according to the designation used by Todeschini.

So, to grasp the meaning of Magnus effect, and comprehend its implications, it is necessary to move the observation point in a triad of references located outside the terrestrial triad reference system in order to attribute to the coaxial reference system, as it actually is, two movements of the Earth: its revolution around the Sun and its rotation (spin) around its axis.

In short, to the one-dimensional flow theory, which is limited to consider as active only the longitudinal component of the flow, it is necessary to replace a new dynamic situation, where the Earth intervenes with its contribution projected in the flow direction.

As mentioned above, this contribution can be evaluated only if the observation point is placed on a triad of reference outside of the "Campo Centro-Mosso" .

Then, it is possible to say that, between the

Magnus effect machine and the "Campo Centro-Mosso" , ie the Earth, there is a correspondence without exception between the energy produced (action) , and an equal energy (reaction) taken from the "Campo Centro-Mosso" .

Accordingly, following the theoretical- experimental analysis of Todeschini, only a working machine according to the Magnus effect in water, by hypothesis considered in this case incompressible, and in hypercritical dynamic regimes, with the Reynolds number of the order of 10 ⁷ , can transform into useful force the potential of the "Campo Centro-Mosso" , ie that of the Earth.

However, in machines proposed up to now to exploit the Magnus effect, this important contribution has never been taken into consideration, with the result that the capacity of these machines to take advantage of the Magnus effect is not optimal, ie, from a different point of view, the study and design of these machines, with particular reference to the shape of the rotating bodies, has never been optimized in view of the contribution of the Earth's rotation.

In light of the above, it appears evident the need for Magnus effect machines designed taking into account all the components that affect said effect.

In this context it is included the solution according to the present invention, aiming to provide rotating bodies having peculiar profiles, different from those considered in accordance with the prior art.

These rotating bodies are proposed for the construction of wind or hydraulic turbines, operating both in flowing waters and in closed circuits.

In addition to the above justification, by subsequent theoretical and experimental analyses, it is also possible to find more explanations for the generation of energy by the Magnus effect, comparing the theory of inertia with the principles of quantum physics .

Particular importance in this regard have the engineering applications (such as the magnetic levitation train) where it is possible to take advantage of the inhomogeneous magnetic fields and ofthe gradients of magnetic susceptibility, but also the new interpretation of the "quantum vacuum" , considered a supplier of energy and pulses, and, therefore, the connecting element between all bodies in the universe; without forgetting the physics of water.

In particular, according to the present invention, reference is made to the theory of vortex motion in water produced by cylindrical bodies animated by their own spin; this movement being able to generate strong magnetic fields in water, for which the separation surface between the rotating body and the environment a strong pressure gradient is created, resulting in the production of power.

In the range of current technological choices of cylindrical and axial-symmetric rotating shapes, the present invention proposes therefore tp provide significant improvements, both in the field of industrial engineering and as regards the reduction of passive forces, relating to the movement of rotating bodies, thus promoting the increase of power output.

These and other results are obtained according to the present invention suggesting rotating bodies for turbines using the Magnus effect with rotation axis of the turbine at right angle to the direction of the working fluidthe profile of which is obtained by making reference to information deemed sure and reliable, and to the experimental results that give the lift of the cylinder as a function of the relationship between the "spin" of the cylinder and the speed of the undisturbed wind, in order to fit, after processing of fluid dynamic parameters, in a configuration built on the profile of ovoidal bodies with precise ratios of length and width, widely experienced in the aviation industry, as regards the coefficients of lift and drag, and in particular on the profile of the ovoid of Rankine- Fuhrraann, applied in the realization of the airships.

In this way it is possible to ensure the reduction of all those terms that subtract power to the axis, such as for example :

- the term due to the friction of the flow on the outer surface of the rotating body;

the term which expresses the losses of the electric motor that generates the rotation of the rotating bodies;

- the term which expresses the friction losses in the transmission and support members: gearwheels and bearings .

It is also possible to ensure:

a standard to be applied in industrial production lines;

- a reduction in the energy dissipated and lost in the power lines due to wake vortex separation.

The purpose of the present invention is therefore to provide rotating bodies for turbines using the Magnus effect with rotation axis of the turbine at right angle to the direction of the working fluidwhich allows to overcome the limits of the solutions of the prior art and to obtain the technical results described above .

Further object of the invention is that said rotating bodies can be manufactured with costs substantially limited, both as regards production costs and as regards the costs of management.

Another object of the invention is to provide rotating bodies for turbines using the Magnus effect with rotation axis of the turbine at right angle to the direction of the working fluidthat is substantially simple, safe and reliable.

It is therefore a specific object of the present invention a rotating body for turbines using the Magnus effect with rotation axis of the turbine at right angle to the direction of the working fluidas defined in claim 1 and a turbine using the Magnus effect with rotation axis of the turbine at right angle to the direction of the working fluidas defined in claim 8.

Further characteristics of the rotating body and turbine according to the present invention are defined in the corresponding dependent claims .

The present invention will be now described, for illustrative but not limitative purposes, according to its preferred embodiments, with particular reference to the figures of the accompanying drawings, in which:

- Figure 1 shows an ovoid of Rankine-Fuhrmann, with its construction lines and the indication of its characteristic measures,

- Figure 2 shows schematically a blade body having a random shape, used to calculate the maximum achievable power;

- Figure 3 shows the profile of the rotating body for turbines using the Magnus effect with rotation axis at right angle to the direction of the working fluidaccording to a first embodiment of the present invention,

- Figure 4 shows the profile of a rotating body for turbines using the Magnus effect with rotation axis at right angle to the direction of the working fluidaccording to a second embodiment of the present invention,

- Figure 5 shows the profile ofa rotating body for turbines using the Magnus effect with rotation axis at right angle to the direction of the working fluidaccording to a third embodiment of the present invention,

- Figure 6 shows a front view of a portion of the rotor of a turbine using Magnus effect with axis of rotation of the turbine at right angle to the direction of the working fluidrealized using a plurality of rotating bodies having the basic profile of figure 5, and

- Figure 7 shows a perspective view of the turbine of Figure 6.

It is known that the kinetic energy per unit of time of a generic flow tube can be transformed into mechanical work, and this, in turn, into electrical energy .

The theory and experiment in recent years (Badr, H.M., Coutanceau, M. , Dennis, S.C.R. and Menard, C. , "Unsteady flow past a rotating circular cylinder at Reynolds numbers 10 ³ and 10 ⁴ " , J. Fluid Mech. (1990), vol. 220, 459-484.; M.H. Chou, "Numerical study of vortex shedding from a rotating cylinder immersed in a uniform flow field" Int. J. Numer. Meth. Fluids (2000), vol. 32, 545-567; Y.T. Chew, M. Cheng, S.C. Luo: "A numerical study of flow past a rotating circular cylinder using a hybrid vortex scheme" J. Fluid Mech. (1995), vol.299, pp.35-71; W. M. Swonson "The Magnus effect: A summary of investigation to date", Trans. ASME, D, (1961), vol. 83. No.3, P. 461-470; N.M. Bychkov "Magnus Wind Turbine. 2. Characteristics of rotating cylinder" Thermophysics and Aeromechanics , vol . 12, No.l, 2005; N.M. Bychkov "Magnus wind turbine. 1 Results of model testing" Thermophysics and Aeromechanics, vol. 11, No.4, pgg. 567-580 (2004); L.S. Pan, Y.T. Chew "A general formula for calculating forces on a 2-d arbitrary body in incompressible flow" J. of Fluids and Structures (2002) 16(1), 71-82; Wind tunnel testing to identify the efficiency of Magnus Effect wind and hydraulic turbines (2008, A. Zasso, Politecnico di Milano, Department of Mechanics) ) have shown that it is possible to improve the performance of a wind turbine using rotating bodies of particular shape and animated by their own spin to take advantage of the dynamic Magnus effect, whose circulatory lift is regulated by the circuitry equation of Kutta-Joukowsky.

The present invention aims at optimizing the implementation of axial-symmetric rotating bodies, obtained from surfaces of revolution widely experienced in aeronautical engineering, such as the envelope surfaces of airships, and is based in particular on the results of the studies of Todeschini (1949) , and more recent researches (Wind tunnel testing to identify the efficiency of Magnus effect wind and hydraulic turbines (2008, A. Zasso, Politecnico di Milano, Department of Mechanical Engineering) , ie in particular on experiments relating to the lift, the force normal to the direction of motion, as well as the resistance or "drag", longitudinal and transverse, due to the presence of viscous friction of the medium and the effects of the pressure field on the surface of the body, and finally to the ratio of these two forces, called fluid dynamic efficiency "E" .

With regard to the drag, on the reduction of which the present invention is focused, it is possible to distinguish three contributions:

- skin-friction drag, linked to the viscosity of the fluid;

- induced drag, linked to the wingtip vortices; form drag or pressure drag, which depends greatly on the shape of the body, the present invention focusing on this last aspect.

In short, according to the present invention, it is proposed the construction of rotating bodies that, in order to give good results of power are referred, making the relative improvements, to solutions tested and validated with regards to the coefficients of high lift and contained drag, and at the same time to specific aerodynamic and geometric references, accurate and easily reproducible. These requirements have been identified, according to the present invention, in the solid ovoid of Rankine-Fuhrmann, shown with reference to Figure 1, characterized by a ratio between the major axis L _RF and the minor axis D _RF preferably equal or near 10.

The solid of rotation derived from the oval of Rankine-Fuhrmann has been widely used in the aircraft industry, in the construction of large airships, because its shape has a high coefficient of penetration along the longitudinal axis, and a reduced drag coefficient in the transverse direction.

In the present invention, it is also proposed another important datum, that is the ratio between the length of the rotating body L and the maximum diameter D at the end of the rotating body. This ratio, referred to as optimal aspect ratio, referring to consolidated tests on the field respectively of the Flettner roto- ship, the oceanographic ship of Cousteau and the Enercon ship, is made to vary between 5 and 6.

The energy yield of a turbine using the Magnus effect according to the present invention can be further improved by making reference in addition to physical-mathematical studies on aerodynamic forces, pressures and velocities acting on the surface of the rotating body, as well as to specific technological expedients designed to reduce the energy expense of the movement of each rotating body, independently from the others. In particular, the application of these additional design variables allows to guarantee energy yields superior to those obtained by the most modern hydraulic turbines, even in the presence of modest hydrostatic loads, with the contribution of the circuitry of Kutta-Joukowsky, similar to a greater motor hydraulic drop, and of velocity fields of the fluid stream, which, according to the Magnus effect, transform into pressure fields.

According to the present invention, the reference to the theorem of Kutta-Joukowsky is necessary, because because of this it is possible to connect the bearing force acting on a body hit by a fluid stream to the circuitry of the speed along a line that surrounds the body. In short, if the circuitry is null the lift is null, while if the circuitry is different from 0, then the lift is different from 0.

In the following description, the concepts so far anticipated will be treated in detail.

As already mentioned, at the base of the present invention is the choice of a profile of the rotating body shaped on the symmetrical profile of the ovoid of Rankine-Fuhrmann with aspect ratio L/D preferably equal to or close to 10, which in the recent past has been widely used in the construction of airships, as it ensures a low drag coefficient both both the front section that sees the line of flight, and for the cross section while offering a greater area to the lines of side streams.

It is put beforehand that, from the physical point of view, the mechanism which establishes the circulating component of the fluid stream around a profile and gives rise to Magnus effect is due to the action of the viscous force at the limit layer of a real fluid, during the starting phases of motion. Subsequently, once the circulatory movement was created, the stationary motion of the fluid which generates the lift can be studied by means of the description of the incompressible and irrotational streams .

To describe the present invention reference is made to the physical-mathematical modes with which the forms of the bodies are modeled which interact with a fast flowing stream.

The fundamental principle of study used to simulate the dynamic reality of the aerodynamic behavior of a body is the one in which sources and wells interact with a fluid stream animated with uniform motion with asymptotic velocity V∞.

The sources are represented as physical- mathematical point entity, from which a flow springs that spreads in the area crossed by the stream of fluid with uniform motion, while the wells (sinks) are summarized as mathematical-physical point entities where a flow disappears.

In the case in which the stream having uniform velocity V∞ invests only a source of given intensity, it opens upstream of the source, and between the new trajectories of the stream lines the stream line is shown which, starting from a point of stagnation positioned upstream of the source, on an axis z parallel to the stream direction and passing through the source, it is arranged in such a way as to draw an open profile named "semi-infinite ogive of Rankine" .

If the fluid stream with asymptotic velocity V∞ first meets a source of assigned intensity and subsequently a sink of equal and opposite intensity, the source and the sink being lined on the z axis, the stream lines open and then close, ie it is possible to obtain two singular points, called points of stagnation, the first upstream of the source and the second downstream of the sink, and a stream line flowing through both and that before and after these points of stagnation coincides with the z axis.

The closed surface, which is obtained by rotating this stream line through 360° about the z axis defines the shape of a three-dimensional axial symmetric body of predetermined length which, located in the considered stream, reproduces exactly the field of motion outside said stream line. That means that the profile of this body, formed by the revolution of the line of stream generated by the presence of the source and of the sink, if entered into the stream flow, does not alter the flow pattern changed by the flow of the source and the sink. A body with this form is called "solid of Rankine" or "ovoid of Rankine."

If the sink is distributed in an infinite sequence of sinks, called "sheet of sinks," such as to absorb point by point the same flow distributed by an infinite number of sources, called "sheet of sources", the body drawed within this combination "sheet of sources" "sheet of sinks", invested by a plain stream of asymptotic velocity V∞, has a symmetrical profile which is a stream line passing through the points of stagnation. This profile is called "symmetric profile of Rankine-Fuhrmann . "

The general equation of that profile, given its difficulty, is solved by iteration speculating each time a value of the flow rate per unit length distributed by the "sheet of sources" and absorbed by the "sheet of sinks", capable of satisfying the integral equation of the profile. This method was developed by Rankine and then applied in a systematic way by Fuhrmann, who determined the forms corresponding to different distributions. The so-called penetrating solids of Fuhrmann were also identified, and this denomination is due to the low drag coefficient that characterizes these solids, because their profiles accompain the stream gradually and consequently have a very contained trail, unlike a bluff body, such as a cylinder, which presents a very large trail, characterized by the presence of vortices which are detached and subtract energy to penetration of the body in the fluid.

To further improve the lift capacity of the rotating body according to the present invention, it is also possible to corrugate its lateral surface, by covering it with small footprints (dimples) , such as for the golf ball, with the aim of making the boundary layer turbulent and therefore to reduce the drag.

The turbines according to the present invention present a high "integral" surface area, given the choice of the profile of the ovoid of Rankine and Fuhrmann, so the can be considered naval conception machines, that is characterised by low values of L/D (at the relationships already used for the motorboat of Flettner) , and slow spin rotation, between 1500 and 3500 rounds per minute in the models, while in the machines in actual size the spin varies generally between 200 and 650 rounds per minute (in air) or higher (in water) .

The analysis, referring to prototype machines, allows to determine the relationship with which it os possible to predict the maximum extractable power.

This same equation, valid in the conditions of ideal non-viscous fluid, moving from the sums to the integrals, allows to calculate the "power factor" with which making comparisons between different blade bodies .

Obviously, in the case of real viscous fluids, the lift and drag coefficients will have different values from the ideal ones, but it is always possible to use the experimental results .

Finally, the expression of the maximum extractable power must be considered as ideal, since it does not consider the viscous effects and the border effects. But this will not affect the demonstration of the dependence of the blade body on the shape and geometry.

It is known that in the literature many experimental data are present that give the lift of the cylinder in relation to the ratio between the peripheral speed of the rotation of the cylinder and the speed of the wind V _∞ .

In order to generalise the calculation of lift in the case of blades of any shape, it os possible to make approximations according to the following simplifying assumptions :

a) the blade can be represented, and then is divided into (3-6) sectors of cylindrical shape;

b) in view of the fact that the rotational motion is slow, it is possible to approximate the circular motion of the various sectors with a translatory motion whose speed V _h is the one that competes to its center of mass; this speed of the center of mass of the sector must be added to the actual wind speed V~, identifying a fictitious speed V _f with which it will be possible to calculate the lift of each sector;

c) the speed of a peripheric point of the blade is the speed of the spin of the blade .

On the basis of the foregoing, for the h-th sector of the blade which is far from the center of rotation (ie the hub) of the turbine of a distance h is associated an aerodynamic force which is usual to decompose into two components perpendicular and parallel to the fictitious velocity V _f , which are respectively the lift and the drag.

In order to compare the effect of different shapes in the production of power extractable from the turbine it is possible to proceed as follows.

Referring to a single blade body (Figure 2) it os possible to write that:

a) the useful elemental force for the production of power extractable from a generic element dA, in function of the useful component Cu of the force coefficient of the fictitious speed V _f :

dF _u = 1/2 p V _f ² C _u dA; (1)

wherein dA = 2 Rp dh;

C _u = C _L cosO - C _D sinO = C _L (V./V _f ) - C _D (Qh/V _f ) f ² = V» ² + Ω ² h ²

b) the elemental torque of the force dF _u :

d = (dF _u ) h (2) c) the elemental power:

dP = (dFj h Ω (3)

d) the power for the entire blade body:

P„ = 1/2 p Ω f V _f ² C _u dA h (4)

Wherein the integral is extended to the active area of the extremity.

Replacing in the relation (4) the previous expressions (obtained with reference to Figure 2) , it is possible to get:

P„ = 1/2 p Ω ; (v + Ω ² h ² ) (c _L ν„/ (Ω ² h ² + V„ ² ) -C _D Ωίι/(Ω ² h ² + V„ ² )) h 2 Rp(h) dh (5)

wherein h is integrated between 0 and Rep, radius of the blade body and the lift coefficients CL and the drag coefficient are obtained by integrating the pressure coefficient Cp and friction coefficients Cf on the entire surface of the cylinder, ie the blade body.

In conditions of ideal non viscous fluid results C _f = 0 and integrating C _p derives C _D = 0, from which the coefficient C _L can be expressed as:

C _L = (2πω/ν _£ ) R _p (h)

from which

C _L = (2πω/ν(Ω ² h ² + Vo. ² ) ) Rp(h)

The use of the coefficients C _L and C _D allows to obtain independent values from the surface of the palar blade bodies (and dependent only by the numbers Re, M and Fr) .

The relation (5) is subsequently reduced in the following relation:

P„ = 1/2 p Ω 2πω V. / R _P ² (h) h dh (6) Replacing the integral and identifying with β the multiplicative term:

β = 1/2 p Ω 2πω V„

it can be obtained P„ = β ∑i(R _P ² (h) h Ahi)

where i = 1, N; N is the number of sectors in which the blade body of the turbine is divided, and Ahi is the amplitude of the i-th sector in which the area projected by the blade body is divided (in the case of square sectors it is easy to derive that Ahi=2 R _P (h) .

The ratio Pw/β is called "power factor", and is indicative of the performance of the blade body.

It is evident that the extremity head is the most important element for the generation of power, while the other sectors contribute negligibly.

For this reason, the blade bodies according to the present invention favor the sector that is most distant from the hub, in addition to being on profiles that offer reduced resistance to the sinking fluid.

All the foregoing constitutes the theoretical basis underlying the realization of the rotating bodies for turbines using the Magnus effect with axis of rotation of the turbine at right angle to the direction of the working fluidaccording to the present invention and relative turbines, which will be described in more detail in the following description, with particular reference to the embodiments shown in Figures 3-7.

In particular, with reference to Figure 3 it is shown the profile of a rotating body 10 according to a first embodiment of the present invention, specifically designed for using water as working fluid, Figure 4 shows the profile of a rotating body 10 according to a second embodiment of the present invention, specifically designed for using a dense fluid and Figure 5 shows the profile of a rotating body 10 according to a third embodiment of the present invention, specifically designed for using a super dense fluid as working fluid.

In the present invention, the term dense fluid refers to a fluid with dynamic viscosity comparable to that of water and with a density of between 1 and 5 g/cm ³ and the term super dense fluid refers to a fluid with dynamic viscosity comparable to that of water and with a density greater than 5 g/cm ³ .

Specifically, in the present invention, the design of rotating bodies starts from subdivision of the ovoid of Rankine-Fuhrmann into four sectors, obtained by dividing the major axis L _RF of the same ovoid into four segments of equal length, said segments being indicated in Figure 1 respectively by the reference numbers 1, 2, 3 and 4. In any case, namely in each of the three embodiments which will be described later, the same proportions L _RF /D _RF = 10 are valid for the ovoid of Rankine-Fuhrmann used for the construction of the segments, in order to optimize the coefficients of lift C _L and drag C _D , as well as the form factor L/D = 5 ÷ 6, between the length L of the rotating body and the maximum diameter of the same, proportion that can be found in the Flettner rotoship (1926) , in the oceangoing vessel of Cousteau (1985) , and in the ship of Enercon (2010) .

The height of the rotating body L is then equal to

In fact, repeating the above steps that allow drawing the ovoid of Rankine-Fuhrmann that contains in itself the construction of the three embodiments of the rotating bodies, whatever the length L of the project, we have :

Form Factor of the ovoid of Rankine-Fuhrmann:

LRF/DRF = 10; DR _F = LRF/10; Form Factor of the rotating body:

L/D = 5, D = L/5;

As a datum for the ^" project it is set:

D _RF = D

which allows to exploit at the maximum the ovoid of Rankine-Fuhrmann as a solid of construction of the rotating body, in the sense that the greater diameter D of the rotating body is set equal to the maximum possible given the further dimensions of rotating body.

This implies that:

L/5 = L _RF /10;

from which:

From the data available in literature [Gottingen, Swanson, and others (YT Chew, M. Cheng, SC Luo, "A numerical study of flow past a rotating circular cylinder using a hybrid vortex scheme" J. Fluid Mech. , Vol. 229, pp. 35 - 71, 1995)] it is known that the parameter which describes the efficiency of a cylinder and, in general, of any body provided with spin around its longer longitudinal axis reached by a flow with high Reynolds number, is the fluid dynamic efficiency E = C _L /C _D , the relationship between the lift coefficient C _L and the drag coefficient C _D .

In addition, the experimental results [WM Swanson,

"The Magnus effect: A summary of investigation to date", Trans. ASME, D, 1961. Vol.83 No. 3, P.461/470] obtained in the wind tunnel on cylinders with end disks confirm that the dimensionless ratio E = C _L /C _D , when working with high values of Reynolds number, may present higher values than those derived analytically, due to the increase in the real case of the coefficient C _L , while the coefficient C _D is reduced. The lift, instead, is decreasing, as a result of the presence of turbulence which cause the lowering of the pressure difference between the back and the front of the cylinder, where by back it is indicated the part of the cylinder in which the peripheral speed is directed in the opposite direction with respect to the direction of movement of the fluid and by front it is indicated the part of the cylinder in which the peripheral speed is directed in the same direction of the direction of movement of the fluid.

According to the present invention, in the choice of the geometric and functional parameters of rotating bodies, reference is made to the numerical-experimental indications deduced from the study conducted by M Bychkov ["Magnus Wind Turbine.2. Characteristics of rotating cylinder" , Thermophysics and aeromechanics Vol.12, No.l, 2005], on rotating cylinders of an axial wind turbine using the Magnus effect.

The main parameters that govern the analysis of the study of Bychkov are:

- the Reynolds number, referred to the diameter of the cylinder;

- the aspect ratio of the rotating body L/D, ratio of the length of the rotating cylinder and its diameter;

the dimensionless speed a , ratio between the peripheral speed of the rotating body and the velocity of the undisturbed flow;

- the parameter C, ratio between the diameter of the disc at the end of the cylinder and the diameter of the cylinder.

In the diagrams shown in this publication, it is possible to see how the fluid dynamic efficiency E varies and how the lift and drag coefficients vary with respect to a, ie with respect to L/D , and C.

From these analyzes emerges the importance of the parameter C and the aspect ratio L/D in defining the performance of the rotating cylinder turbines, and that in the design of a turbine using the Magnus effect one of the most important problems is to identify the conditions that allow to reduce the drag coefficient of the rotating body.

For this purpose, always from these experimental results, it is shown that it is possible to act on the aspect ratio L/D even if this involves problems from the point of view of construction.

However, when changing the aspect ratio L/D only is not sufficient, it is possible to refer to estimates derived from experimental references, which indicate that it is possible to achieve optimal solutions by making changes to the shape of the rotating bodies.

Starting from this important observation, it is developed the solution according to the present invention wherein in the configurations deduced from the ovoid of Rankine-Fuhrmann with L _RF /D = 10 it is identified the possibility of reduction of the drag coefficients, by reason of the guarantees that are given by the large number of experimental applications in real-world units, such as airships, the forms of which reproduced the profile of the oval of Rankine- Fuhrmann with LR _F /D = 10.

In particular, after having chosen to realize the rotating bodies according to the present invention following the profile of the ovoid of Rankine-Fuhrmann, as well as after dividing this ovoid of construction into four sectors, obtained by subdividing the major axis L _RF into four equal parts, depending on the characteristics of the working fluid the optimum shape of the rotating body is obtained through the following considerations .

With reference to Figure 3, in the case where water is used as working fluid, to take advantage of the maximum useful work surface, the profile of the rotating body 10 is realised following the profile of the second and the third sectors into which the ovoid of construction of Rankine-Fuhrmann has been divided, i.e. the sectors of the ovoid of Rankine-Fuhrmann corresponding to the segments indicated in Figure 1 by the reference numbers 2 and 3, which are those with greater values of diameter.

With reference to Figure 4, in the case where a dense fluid is used as working fluid, to continue to take advantage of the maximum useful surface of work, at the same time limiting the drag of the rotating body in the portion in which the same is the most stressed by the fluid that reaches it, i.e. in correspondence of half of its length, the profile of the rotating body 10 is still realised following the profile of the second and the third sector into which the ovoid of construction of Rankine-Fuhrmann has been divided, in this case by reversing their mutual position so as to form two opposing trapezoids, welded along the minor base, such form being in other words obtained through the combined transposition (permutation) of the third sector to the second sector.

With reference to Figure 5, in the case where a super dense fluid is used as working fluid, it becomes essential to further reduce the drag of the rotating body in the portion in which the same is the most stressed by the fluid that reaches it, i.e. in correspondence of half of its length, the profile of the rotating body 10 is realised following the profile of the first and fourth sectors in which the ovoid of construction of Rankine-Fuhrmann has been divided, i.e. the sectors corresponding to the segments indicated in Figure 1 by the reference numbers 1 and 4, reversing their reciprocal position so as to form an hourglass, thus formed by the combined transposition (permutation) of the last sector to the first sector and welded together at the point of maximum curvature, where they are connected by means of sections of prolated spheroid, i.e. with surfaces of quadrics of rotation with one flap. It is evident that, according to this embodiment, the space available to the passage of the fluid is greater, in this way being avoided that the fluid itself can subject the rotating body to overstressing .

With reference to Figures 6 and 7, by way of non limitative example it is shown the portion of the rotor of a radial turbine using the Magnus effect provided with a plurality of rotating bodies according to the embodiment of the present invention shown in Figure 5 and specifically proposed for use with a super dense working fluid. This does not exclude that the same configuration can be applied also with rotating bodies 10 made according to the embodiments shown in Figures 3 and 4.

In particular, in Figures 6 and 7, the upper 11 and lower 12 bases of each of the rotating bodies 10, preferably equal in number to eight, which form the portion of the rotor of a turbine using the Magnus effect according to the present invention, are carefully secured to two respective connecting rings 13, 14 which have, in their interior, seats designed and equipped to allow the various rotation speed schemes around its own axis .

All rotating bodies 10, due to the Magnus effect, are solicited by a force that moves the connecting rings 13, 14, determining a motor torque on the central axis of the rings themselves, in turn connected with a drive of electrical power, or an alternator (not shown) .

To ensure that all the rotating bodies 10 are moved by a thrust which transfers to the central axis a torque that is added positively with that derived from the other rotating bodies, the same must be invested by the fluid vein in a radial direction with respect to the central axis, i.e. guided and regulated by the presence of a suitable distributor (not shown) .

To enable continuity in the operation and limitation of energy expenditure due to the movements, in spite of this entails greater constructive difficulties, it is also convenient to equip each rotating body with its own motor member of rotation around its own axis, at variable speed to cover the range of work and in perfect synchronism with the others, by means of individual multipolar motors with variable number of revolutions .

The scheme of spin chosen, i.e. the speed of rotation of the rotating bodies around their axis is governed by process considerations on energy, the analytical relations of which contain the geometrical- functional parameters that govern the realization phase of the executive project.

Moreover, referring to Figures 6 and 7, the rotating body 10 is completed by two end disks 14, with a diameter greater than the diameter of the rotating body, equipped, on their side directed towards the outside, with a series of blades 15, shaped so as to capture energy from the flow generating a thrust through which they participates to the movement of the spin of the rotating body 10, thus reducing the energy expense of the engines dedicated to the rotation of the same rotating bodies .

The end plate 14 and the winglets 15 are an adaptation of improvement compared to the previous embodiments of the ends (Flettner rotoship; N.M. Bychkov "Magnus Wind Turbine. 2. Characteristics of rotating cylinder" Thermophysics and Aeromechanics, vol. 12, No.l, 2005). In particular, the end plate has the task to increase the lift of the rotating body, reducing the vorticity of the fluid threads of the extremities, and its diameter is equal to k-D, where k depends on the ratio between the spin velocity of the rotating body and the resultant velocity V _R incident on the rotating body, vector sum of the undisturbed velocity V∞ of the fluid interacting and the peripheral velocity of the peripheral end of the turbine-wheel: VR ² = V∞ ² + Q ² - R ² . In particular, k is preferably comprised between 1,25 and 1,3, and more preferably itis equal to 1,3.

It is important to repeat two aspects of the decisive stage of movement of the rotating bodies.

The first aspect is that the expense of spin is invariant with respect to the speed of the fluid that invests the rotating ovoids, as it is apparent from repeated experimental cycles .

The second aspect concerns the fact that, in order to allow continuity in the operation and limitation in energy expense due to the movements, it is convenient to equip each rotating body of a motor member of its own rotation around its own axis, at variable speed to cover the working range, despite it involves more difficult construction.

The present invention has been described for illustrative but non limitative purposes, according to its preferred embodiments, but it is to be understood that variations and/or modifications can be apport by those skilled in the art without departing from the relevant scope of protection, as defined by the appended claims.