The present invention refers to an innovative vertical-axis eolic generator.
Eolic energy is the product of a conversion of the kinetic energy of wind into other forms of energy. To date, such a conversion is carried out by means of eolic generators, which can be horizontal-axis or vertical-axis.
The present invention specifically relates to a vertical-axis eolic generator.
As it is known, for several years now the vertical-axis eolic electric generator has been the subject of studies and implementations for the independence of its operation from wind direction and the simplicity of its implementation, in particular for small installations of a power of the order of some kWs.
Its operation substantially derives from the thrust a wing-type profile is subjected to when impinged upon by a fluid stream, thrust that, opportunely directed by the construction geometry of the machine, produces a torque and therefore the rotary motion of the machine.
In observed embodiments, curved longitudinal-axis vanes are generally utilized which, during their motion, describe a spherical surface or a barrel-like surface or the like, anyhow with the concavity facing the axis of rotation of the machine.
Moreover, it has been observed that the cross section of the vanes is generally configured according to a classic wing-like profile, with the concavity always facing the axis of rotation of the machine, non-symmetrical in the plane of its cross section, whereby it maintains its functionality only in a single zone of its circular path.
It will be appreciated that the above-described known eolic generators entail significant and evident drawbacks, which are listed hereinafter:
Object of the present invention is to solve the abovementioned drawbacks by providing an eolic generator as substantially described in claim 1.
Further features of the process are defined in the corresponding dependent claims thereof.
The present invention, by overcoming the mentioned problems of the known art, entails several evident advantages.
The eolic generator subject-matter of the present invention has the innovative feature of being equipped with vanes having a rectilinear longitudinal axis, entailing a greater simplicity, and therefore lower construction costs. Moreover, the vanes of the eolic generator subject-matter of the present invention have a cross section with a concave profile that is simple and provided with an axis of symmetry.
As will be detailed hereinafter, the area of aerodynamic interaction between vanes and wind can be subdivided, according to a plan view, into four quadrants. The convexity of the profile of the vane of the generator subject-matter of the present invention faces the internal portion of the path of the vane, in a manner such that the vane itself be active (therefore contributing to the production of a useful torque collected at the driving shaft) both when it lies in the first quadrant, when advancing against the wind, and in the first section of the third quadrant when its velocity is concordant with wind velocity.
Even in a starting, low velocity stage, torque is provided by the vane in two distinct path positions, remarkably increasing the performance of the machine under said delicate operation modes.
Along the longitudinal development of each vane, two areas are found which contribute more to torque generation, each one located substantially at respectively a top portion and a bottom portion of the vane. For this reason, at said portions where maximum efficiency for torque production is found, in the generator subject-matter of the present invention additional vanes are advantageously positioned, which contribute to sensibly increase produced torque, especially in the starting stage or under low regimens.
Such additional vanes contribute to generate a remarkable turbulence in the leeside area of the machine, limiting the resisting torque of the vane when it moves in such low-regimen area and enhancing it with the increasing of “ω”, in a manner such as to also offer a system for self-adjusting the machine, in order to prevent it from reaching possibly dangerous critical velocities.
Still further advantages, as well as the features and the operation modes of the present invention, will be made apparent in the following detailed description of a preferred embodiment thereof, given by way of example and not for limitative purposes. Reference will be made to the figures of the annexed drawings, wherein:
Referring to
Referring to
As is amply known to a person skilled in the art, in both cases shown, the force F generated following interaction between fluid stream and wing profile has a numeric value generally proportional to the square of the velocity modulus Va.
In a vertical-axis eolic generator, each section of each vane during a rotary motion of the machine gets to lie, at subsequent instants, in either of the conditions illustrated in
In general, the geometric configuration of the machine tends of course to cause the effects of the condition of
Referring to next
Each vane has a substantially rectilinear longitudinal axis.
The vanes are connected to the driving shaft by a pair of spline elements. In particular, said pair comprises a top spline element 7, placed at a top portion of the driving shaft 2, and a bottom spline element 8, the latter placed at a bottom portion thereof.
The top 7 and bottom 8 spline elements respectively have a plurality of arms, each connected to a respective vane. In particular, since the preferred embodiment described herein comprises four vanes, the top 7 and bottom 8 spline elements each comprise respectively four top arms 71, 72, 73, 74 and four bottom arms 81, 82, 83, 84. Preferably, such top and bottom arms are angularly equispaced thereamong. In other words, all pairs of arms define respective angles equal therebetween.
In the case described herein with four vanes, said arms have a cross-like shape, as each arm forms, with an arm consecutive thereto, a substantially right angle.
Hence, hereinafter in the present treatment of such a preferred embodiment the spline elements 7 and 8 will be referred to as top cross 7 and bottom cross 8.
Always referring to
Considering now by way of example vane 3, yet clearly the principle holds true for each vane of the generator, the former is connected to the top arm 71 at a top part 31 thereof, and is connected to the bottom arm 82 at a bottom part 32 thereof. In particular, the bottom arm 82 is the arm angularly consecutive to the bottom arm 81 opposite to the top arm 71, to which the vane 3 is connected as highlighted above. Therefore, thus the vane 3 assumes a tilt with respect to the driving shaft 2, the latter placed along the vertical axis of the eolic generator.
In an entirely analogous manner, the vane 4 is connected between the top arm 72 and the bottom arm 83, angularly consecutive with respect to the bottom arm 82 opposite to the top arm 72.
Moreover, the eolic generator comprises a third spline element 9, apt to connect the vanes 3, 4, 5 and 6 to the driving shaft 2 at a central portion thereof. It will be appreciated that, in this case as well, the third spline element 9 has the shape of a cross, having central arms 91, 92, 93, 94 angularly equispaced thereamong and forming a substantially right angle thereamong. It will be appreciated that the positioning of such a central cross increases the solidity of the generator 1, as it contributes to decrease any flexural vibrations generated by the vanes during their rotary motion.
Lastly, additional vanes, in the figure denoted by way of example and not for limitative purposes by reference numbers 741 and 742, are advantageously cantilevered on the top and bottom arms. The additional vanes 741 and 742 are cantilevered on the top arm 74 in a manner substantially parallel to the vane 6, connected just with the arm 74.
The generator vanes and the hereto-described additional vanes are connected to the arms of the crosses by preferably reversible mechanical connection means. In particular, each vane is integral, at the top and bottom parts thereof, respectively to a top plate and a bottom plate; said plates are bolted to the respective top and bottom arms. E.g., always referring to
Moreover, the driving shaft has, along its vertical development, a plurality of fins 12, serving as generators of turbulence. The turbulence generated by the fins 12 is such as to produce effects on the vanes lying in a leeside area of the generator, i.e., the area in which the vanes are impinged upon by the fluid stream once it has already gone past the driving shaft 2.
Referring to
Moreover, always in the same figure, the central cross 9 is depicted, which is tilted of 45° with respect to the top cross (and also with respect to the bottom cross not depicted) due to the above-illustrated tilt of the vanes.
Referring now to
Such a surface, also referred to as “skew ruled”, is perfectly known to a person skilled in the art, therefore its properties will not be discussed further.
It will be appreciated that, with the increasing of the number of vanes, the surface described during their motion will be such as to approximate ever better such a geometric figure of hyperbolic paraboloid.
Referring now to
Referring now to
In the case considered, of a four-vane eolic generator, from the top cross to the bottom cross the profile 10 undergoes a rotation of about 90°.
The manufacturing modes for a vane having a twist as described above are amply within the reach of a person skilled in the art and will not be described below. Hereinafter, some aerodynamic analyses of the generator 1 subject-matter of the present invention are described.
Referring to
The vanes/wind interaction area is conventionally divided into four quadrants, to which reference will be made in the following description.
For the above-described particular symmetric profile of the vane, it is obtained the positive thrust (determined by forces P in the Figure) in the first quadrant and in the first section of the third quadrant. In particular, the first quadrant identifies a windward area (i.e., first impinged upon by the fluid stream having a velocity Vr) in which the velocity of the vane V107 is opposite to the velocity of the fluid stream and, in the first section of the third quadrant and wherein the vane has a velocity concordant with wind velocity and with V<r.
Referring now to
Referring to
In general, the eolic generator subject-matter of the present invention, being k1 and k2 coefficients depending on its geometry, has a torque synthetically represented by the simple expression:
Cm=k1S1V2r
whereas a resisting torque likewise assumes the expression:
Cr=k2S2V4r
Hence, the torque available for the electric generator is
C
G
=C
m
−
C
r
=k
1
S
1
V
2
r
−k
2
S
2
V
4
r
An expression reaching its maximum value for
Therefore, the eolic generator subject-matter of the present invention is self-protected from angular velocities harmful to its structure and to electrical apparatuses, as CG cancels out for:
C
G
=k
1
S
1
V
2
r
−k
2
S
2
V
4
r=0
An equation admitting the real and positive solution:
In short, what has been analyzed hereto is highlighted in the diagram of
Referring now to the last
The generator 1′ comprises top 301 and bottom 302 spline elements, which this time comprise each top and bottom arms which are angularly spaced thereamong of an angle equal to about 120°, and therefore have a substantially Y-like shape. The vanes of the generator, for which it is denoted by way of example and not for limitative purposes the vane 400 in figure, have a symmetric crescent-shaped profile, but one which undergoes a rotation of a 120° angle at the various sections of the vane along the longitudinal development thereof.
At most, the eolic generator subject-matter of the present invention could also be implemented with only two vanes. In this case (not depicted) the spline elements will have two arms spaced therebetween of a 180° angle and the vanes will be substantially arranged in an X-like shape with respect to the driving shaft.
The present invention has been hereto described with reference to two preferred embodiments thereof. It is understood that other embodiments might exist, all falling within the concept of the same invention, and all comprised within the protective scope of the claims hereinafter.
Number | Date | Country | Kind |
---|---|---|---|
RM2009A000254 | May 2009 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/IB10/50804 | 2/24/2010 | WO | 00 | 12/6/2011 |