The present invention falls within the field of solar trackers and more specifically, within the field of T-shaped solar trackers, comprising either a cylindrical or parallelepiped pedestal, to which a supporting structure or structural support is attached by its upper extremity, said supporting structure or structural support being made of mirrors or photovoltaic modules, rotating on two axes, namely azimuthal and lifting axles.
Many supporting and rotating mechanisms in supporting structures in solar panels are currently known, understanding by solar panels, both, solar collectors and photovoltaic cells.
These known azimuthal rotation systems are problematic in that, during their daily following of the sun, their initial angular position changes, day after day (in some cases, the difference between the initial position of one day and the next, exceeding 40°). When a large daily angular trajectory (for example 330°) is necessary in order to adopt the initial position the following day, they must be capable of travelling the 330° daily trajectory plus the 40° which separate them from the new initial position, in other words a total of 370°. Nevertheless, when the state of the art trackers surpass a total revolution of 360° and end their travel length at this point, it becomes necessary for them to backtrack, that is to say to rotate in the opposite direction to that of the daily trajectory, in order to position themselves in the new initial position corresponding to the next day. This results in a loss of time, that could be spent reflecting solar rays to the tower and subsequently, in a loss of energy and production time as the solar tracker repositions itself. Furthermore, it creates the risk of the rays moving randomly, thus losing energy and production time since they are not reflected on the tower when the solar tracker is repositioning itself.
Of the azimuthal rotation mechanisms known, U.S. Pat. No. 6,123,067 stands out, disclosing an azimuthal rotation mechanism of solar tracker supporting structures by means of two hydraulic cylinders, which are capable of rotating without the need to backtrack. This mechanism achieves said effect by means of a complex and expensive system, comprising a large scale rotating frame, which rotates around the pedestal, driven by two cylinders, which comprise a first extremity attached to one corner of the frame and a second extremity attached to a rotating axle, the rotating axle of each extremity of each cylinder being different and close, attached to a piece fixed to the pedestal by means of a cylinder, both of which are screwed to the pedestal. This mechanism presents the problem of having large backlashes and runs the risk of the frame rubbing against the pedestal and thus creating friction.
The invention refers to a solar tracker comprising either a cylindrical or parallelepiped pedestal, to which a supporting structure or structural support made of mirrors or photovoltaic modules is attached by its upper extremity, with an azimuthal rotating mechanism comprising:
the ends of the pistons of the first and second cylinders being arranged in the interior of the bearing cap, one on top of the other and connected by the same, fixed rotating axle, perpendicular to the cylinders, attached to the hollow cylinder on the fixed base of the mechanism by a connecting piece, upon which the bearing cap with the supporting structure it supports rotates, driven by the cylinders to which the bearing cap is attached.
The two hydraulic cylinders are at different heights and levels, that is to say, one on top of the other, enabling them to cross whilst preventing them from bumping into one another.
The advantage of this azimuthal rotating mechanism for supporting structures of solar trackers arranged on a pedestal, is that it enables a rotation of 360° or more along one sole axle, without the need to backtrack in order to continue the rotation on the following complete day and without the interposition of any element.
Below, a series of drawings which facilitate a better understanding of the invention will be briefly described, these drawings relating specifically to one embodiment of said invention and presented as a non-limiting example thereof.
1.—pedestal
2.—supporting structure or structural support
3.—bearing cap
4.—upper lid
5.—lower lid
6.—hydraulic cylinder
7.—vertical rotation axle
8.—element attaching the axle to the hollow cylinder
9.—lateral opening of the bearing cap
10.—fixed base
11.—supporting plate
12.—supporting rib
13.—hollow cylinder
14.—clamp
15.—upper attachment extension of the cylinder
16.—lower attachment extension of the cylinder
17.—rotating mechanical element
18.—fixed internal hoop
19.—rotating external hoop
20.—cylindrical piece with a diameter equal to that of the pedestal
21.—join
With this arrangement, when the pistons in the cylinders 6, 6′ start to move, they cause the bearing cap 3, to which the supporting structure 2 is attached, to rotate. The cylinders are attached by means of the clamps 14, 14′ to the upper extensions 15, 15′ and lower extensions 16, 16′ of the bearing cap. The cylinders 6, 6′ rotate relative to the same axle 7, which in turn is attached to the hollow cylinder 13 of the base 10. In this way, the bearing cap 3 rotates along with the supporting structure 2 in an azimuthal fashion on the fixed pedestal 1.
As already mentioned, the hydraulic cylinders 6, 6′ are connected by the extremity corresponding to their piston by means of the same fixed vertical rotating axle 7, perpendicular to the cylinders, attached to the hollow cylinder 13 by means of an attachment element 8. This enables a rotation of more than 360° without any form of impediment, in such a way that the solar tracker does not have to backtrack in order to position itself at the start of each travel length.
The ends of the pistons are arranged one on top of the other, preventing one from impeding the rotational movement of the other, in such a way that each cylinder 6, 6′ is at a different height, crossing a first and second opening 9, 9′ on the lateral surface of the bearing cap 3.
Each of the cylinders 6, 6′ are attached to the bearing cap by means of a clamp 14, 14′, in such a way that when the cylinders 6, 6′ begin to move, their pistons rotate relative to the fixed rotating vertical axle 7 and cause the bearing cap upon which the supporting structure 2 is secured, to rotate.
This tracking system is specifically designed for its use in solar trackers but the possibility of extending its use to other fields within the industry requiring similar azimuthal tracking is not discarded.
Number | Date | Country | Kind |
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P201230809 | May 2012 | ES | national |
Filing Document | Filing Date | Country | Kind |
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PCT/ES2013/070327 | 5/23/2013 | WO | 00 |