The present invention is a wind turbine designed to transform wind energy into mechanical energy.
The use of turbines designed to transform wind energy into mechanical energy is well known, such devices generally being arranged in arrays comprising a significant number of turbines erected in particularly windy locations.
Generators of known type usually comprise a frame designed to rotatingly support fluid-dynamic means destined to capture the wind, the fluid-dynamic means being connected by a mechanical transmission to a user device, for example a generator of electrical current.
The kinetic energy of the air is generally converted into mechanical energy and subsequently into electrical energy using aerogenerators.
Installations range comprises from mini- and micro-scale wind turbines which give an output of from a few hundred Watts to tens of kW of power, to medium sized installations rendering up to about a hundred kW, and finally to large scale systems which can produce an output measured in MW.
Horizontal axis machines of known type exhibit a rotor axis parallel to the direction of the wind and a rotor which rotates on a plane perpendicular to the direction of the wind.
Such devices can be further sub-categorized according to the characteristics of the rotor.
While numerous variants exist, the typical rotor is normally characterized by a wing shaped radial blades.
The special characteristics of the machine are high rotational speed and high power output as a consequence of the high lift coefficient of the blades.
Also known are vertical axis machines exhibiting a rotor axis that is placed perpendicular to the direction of the wind.
Again these can be sub-categorized on the basis of the rotor type used.
In this specific configuration the turbine exhibits the considerable advantage of not needing to orientate itself relative to the direction of the wind, which can thus be exploited around 360° of rotation without auxiliary movements. In contrast, the rotor of horizontal axis machines must be guided to face the direction of the wind using a vane.
Vertical-axis machines are of limited dimensions and are more suited to urban wind patterns which are normally turbulent, extremely variable in direction and strength, and consequently badly suited to horizontal axis turbines.
Vertical axis turbines are also suitable for use in very remote locations characterized by extreme climactic conditions including the formation of ice and intense, variable wind patterns.
Generators of known type exhibit a number of disadvantages which to date have not been successfully resolved.
A first disadvantage is aesthetic, since in order to provide an acceptable level of power wind turbines must be arranged in arrays or “farms” comprising a considerable number of turbines.
Wind farms must be positioned in windy areas and unavoidably compromise landscape which is often of considerable environmental relevance, and their construction is understandably opposed by local authorities.
Environmental impact is worsened by the fact that the air currents required to turn the fluid-dynamic means of the turbines are generally found at a significant height above ground, making it necessary to construct turbines of a considerable height.
An efficient height is thought to be at least 6 meters above ground level in order to achieve acceptable results.
A second disadvantage, technical in nature, is the limited yield of known fluid-dynamic means which are efficient only if the wind speed is above approximately 6 m/sec., a velocity that is rarely encountered in proximity to urban areas, and consequently any generated electricity is subject to significant transport costs.
Consequently there is an obvious need for a wind turbine, of limited bulk in both the horizontal and vertical profiles, that can operate with wind at a lower speed than that required to drive generators of known type while providing a comparatively higher energy yield.
The aim of the present invention is to provide a wind turbine that satisfies these requirements, is simple in shape, exhibits limited overall dimensions, and produces a high fluid-dynamic yield.
This aim is attained by a generator exhibiting the characteristics recited in the independent claim.
The dependent claims describe characteristics that improve the performance of the invention.
The advantages and constructional and functional characteristics of the invention will better emerge from the detailed description made herein, which in the accompanying figures of the drawings describes a preferred embodiment of the invention, provided by way of non-limiting examples.
The first embodiment of
The brackets 11 support a circular ring 12, on which pairs of idle wheels 13 run, supported by brackets 14 extending from a lower circular edge of a cylindrical casing 15, the casing 15 thus being free to rotate around an axis thereof.
Fitted at the bottom of the casing is a circular rack 16 exhibiting internal teeth enmeshing with a pinion 17 of an electrical motor 18 solidly fitted to the plate 10.
The rotation of the casing 15 is thus controlled by the motor 18 in a way that will be explained herein below.
The plate 10 is fitted with a central hub 19 (
The shaft 22 supports, above the plate 10, a cage 23 reinforced with plates 230, from which three profiled blades 24 are formed of matching concavity.
In particular each blade 24 is supported by three curved brackets 25 associated to the cage 23.
The lower extremity of the shaft 22 is splined to the rotor, not illustrated, of an electrical generator 26, which can be of synchronous or asynchronous type.
The cylindrical casing 15 exhibits two openings 151 and 152 (
The opening 151 is in communication with a divergent duct 153, while the casing 152 is in communication with another divergent duct 154.
Both the ducts are divergent in the direction they project away from the casing 15.
The space between the two openings 151 and 152 is entirely occupied by at least one of the blades 24, the concavity of which faces towards the opening 151.
A vertically-extending flat vane 27 is supported at the upper end of the casing and is free to rotate about a vertical axis, which vane 27 automatically aligns to the direction of the wind.
The vane 27 rotates freely on a pin 28 solidly associated to the casing 15.
The vane 27 and the casing 15 are connected to reciprocal mobile parts of an encoder device, schematized at 29, of which a reference point, or zero, coincides with the position of the vane 27 orthogonal to the diameter of the casing comprising both the axis of the casing and the axis of the pin 28, i.e. the rotational axis of the vane.
The reference position of the vane coincides with the direction of the wind.
The encoder device controls the motor 18 such as to move the reciprocal positions of the vane 27 and the duct 153 into the reference position.
In this way the duct 153 inlet is always substantially perpendicular to the wind direction.
In the invention the rotor comprised of the blades 24 preferably exhibits an axial dimension of from 2000 mm to 3000 mm, and a diameter of from 2000 mm to 2600 mm; the casing exhibits a diameter and height sufficient to snugly contain the rotor without interference; at the casing 15, the inlet duct 153 is at an angle of about 90° to the casing 15, and also exhibits a flat opening displaced from the casing and at a same height as the casing, with a width of from 1500 mm to 2300 mm, and a length, measured from the diametric plane parallel to the inlet, of from 1500 to 2300 mm; the outlet duct 154 is at an angle of about 90° to the casing 15, and has a flat opening displaced from the casing at a same height as the casing, with a width of from 1000 to 1500 mm, and a length, measured from the diametric plane parallel to the inlet, of from 1500 to 2000 mm.
The invention has been observed to operate with measured wind speeds of around 4 m/sec.
The invention functions as follows.
The encoder located between the vane 27 and the casing 15 activates the motor 18 such as to maintain the inlet opening of the duct 153 always perpendicular to the wind direction.
The wind captured by the duct inlet 153 is conveyed by the duct such that the entire air flow is received by the blade 24 momentarily positioned in front of the opening, causing the rotor to rotate together with the associated generator.
The second embodiment of
The plate 10 is fitted with a central hub 19 (
The shaft 22 supports, above the plate 10, a cylindrical body 220 coaxial with the hub 19, from which three pairs of coplanar arms 250 project radially.
Each pair 250 supports a wing 240 parallel to the external wall of the casing 15, near and substantially parallel thereto.
The cylindrical casing 15 exhibits two openings 151A and 152A (
The opening 151A is in communication with a convergent duct 153A, while the opening 152A is in communication with a divergent duct 154A.
The projection on the diameter of the opening 151A is larger than the radius of the cylindrical casing 15, and the convergent duct 153A is comprised between two convergent walls 153B and 153C having an angle therebetween of 30° to 45°, preferably of 36°.
More precisely the wall 153C is substantially tangent to the cylindrical casing 15, and inclined to the plane 270 of the vane 27, while in its reference position, of an angle α of 7° to 13°, preferably 10.5°. The wall 153B is inclined to the wall 153C of an angle β of 16 to 27, preferably of 25.5°.
The distance between the inlet end of the convergent duct 153A and the axis of the casing 15 is of 1.5 the diameter of the casing to 1.75 the diameter of the casing, preferably the distance is 1.65 the diameter.
The divergent walls 154B and 154C are symmetrically disposed in respect of the shaft 22, each is substantially tangent to the casing and the angle therebetween is of 11° to 15°, preferably of 13°.
The distance between the outlet end of the divergent duct 154A and the axis of the casing 15 is of 1.0 the diameter of the casing to 1.30 the diameter of the casing, preferably the distance is 1.11 the diameter.
The bisecting plane 500 of the walls 153B and 153C of the convergent duct lies between the axis of the casing 15 and the wall 153C.
The space between the two openings 151 and 152, 151A and 152A is always occupied by at least one of the blades 24, or wings 240.
The invention is not limited to the example described above and variants and improvements could be introduced without exiting from the scope of the following claims.
Number | Date | Country | Kind |
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RE2009A0077 | Jul 2009 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2010/051650 | 2/10/2010 | WO | 00 | 4/10/2012 |
Publishing Document | Publishing Date | Country | Kind |
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WO2011/012334 | 2/3/2011 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2746 | Grew | Aug 1842 | A |
14997 | Battey | Jun 1856 | A |
45273 | Reister | Nov 1864 | A |
171962 | Stephens et al. | Jan 1876 | A |
201400 | Everhart | Mar 1878 | A |
264164 | Jackson | Sep 1882 | A |
313646 | Bausman | Mar 1885 | A |
381679 | Devereux | Apr 1888 | A |
993120 | Sterner | May 1911 | A |
1025428 | Stanschus | May 1912 | A |
1225033 | Jackson | May 1917 | A |
1471095 | Bonetto | Oct 1923 | A |
1835018 | Darrieus | Dec 1931 | A |
2942773 | Eck | Jun 1960 | A |
3883261 | Saxmann | May 1975 | A |
3883750 | Uzzell, Jr. | May 1975 | A |
3902072 | Quinn | Aug 1975 | A |
3944840 | Troll | Mar 1976 | A |
4031405 | Asperger | Jun 1977 | A |
4084918 | Pavlecka | Apr 1978 | A |
4164382 | Mysels | Aug 1979 | A |
4174923 | Williamson | Nov 1979 | A |
4260325 | Cymara | Apr 1981 | A |
4279569 | Harloff | Jul 1981 | A |
4295783 | Lebost | Oct 1981 | A |
4834610 | Bond, III | May 1989 | A |
4872804 | Teles De Menezes | Oct 1989 | A |
5009569 | Hector et al. | Apr 1991 | A |
5088884 | Bergstein | Feb 1992 | A |
5332354 | Lamont | Jul 1994 | A |
6191496 | Elder | Feb 2001 | B1 |
6710468 | Marrero O'Shanahan | Mar 2004 | B1 |
6981839 | Fan | Jan 2006 | B2 |
7056082 | Taylor | Jun 2006 | B1 |
7484363 | Reidy et al. | Feb 2009 | B2 |
8154145 | Krauss | Apr 2012 | B2 |
20010004439 | Bolcich et al. | Jun 2001 | A1 |
20030133782 | Holter et al. | Jul 2003 | A1 |
20030133783 | Brock et al. | Jul 2003 | A1 |
20070098542 | Streeman et al. | May 2007 | A1 |
20090045632 | Krauss | Feb 2009 | A1 |
Number | Date | Country |
---|---|---|
202007004034 | May 2007 | DE |
1925819 | May 2008 | EP |
Entry |
---|
Freimund, English Machine Translation of DE202007004034, May 24, 2007, Translated by epacenet Nov. 24, 2014. |
Number | Date | Country | |
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20120189428 A1 | Jul 2012 | US |