DAMPING SYSTEM OF A SOLAR TRACKER

Abstract

A damping system of a solar tracker is provided, having at least one damper has a rod, an upper tie and a lower tie located at the end of the damper opposite the upper tie; where the upper tie is fixed by an upper support to a rotation shaft of the solar tracker, and where the lower tie is fixed by a lower support to a column of the solar tracker, so that with the rotation of the rotation shaft, the rod of the damper is caused to retract or extend, characterized in that the upper support has a lever comprising at least one end protruding from the rotation shaft with at least two securing points at which the upper tie of the damper is fixed by an upper shaft of the upper tie which is fixed at the at least two securing points of the lever.

Claims

1. A damping system of a solar tracker (1) comprising at least one damper (4) comprising a rod (4.1), an upper tie (4.2) and a lower tie (4.3) located at an end of the at least one damper (4) opposite the upper tie (4.2); wherein the upper tie (4.2) is fixed by means of an upper support (2) to a rotation shaft (1.1) of the solar tracker (1), and wherein the lower tie (4.3) is fixed by means of a lower support (3) to a column (1.2) of the solar tracker (1), so that with the rotation of the rotation shaft (1.1), the rod (4.1) of the at least one damper (4) is caused to retract or extend, wherein the upper support (2) comprises a lever (2.2) comprising at least one end protruding from the rotation shaft (1.1) with at least two securing points at which the upper tie (4.2) of the damper (4) is fixed by means of an upper shaft (2.3) of the upper tie (4.2) which is fixed at the at least two securing points of the lever (2.2).

2. The damping system according to claim 1, wherein the lever (2.2) has an inverted U-shaped profile comprising at least one securing point on each wing of the lever (2.2).

3. The damping system according to claim 1, wherein the upper support (2) comprises an upper clamp (2.1) surrounding the rotation shaft (1.1) and the lever (2.2) is fixed to the upper clamp (2.1).

4. The damping system according to claim 3, wherein the upper clamp (2.1) has an omega-shaped profile on the wings of which the lever (2.2) is fixed.

5. The damping system according to claim 1, further comprising two dampers (4) and the lever (2.2) comprises two ends protruding from the rotation shaft (1.1), in which the upper fastening (4.2) of the respective damper (4) is fixed at each end.

6. The damping system according to claim 1, wherein the lower support (3) comprises a lower clamp (3.1) with an omega-shaped profile surrounding the column (1.2) on the wings of which there is fixed a plate (3.2) in which the lower tie (4.3) of the damper (4) is fixed.

7. The damping system according to claim 1, wherein the lower support (3) comprises a lower clamp (3.1) comprising two sub-clamps (3.1.1) with an L-shaped profile superimposed on one another, being fixed to the column (1.2) and clamping same by means of bolts.

8. The damping system according to claim 7, wherein a plate (3.2) is fixed on the superimposed wings of the sub-clamps (3.1.1) in which the lower tie (4.3) of the damper (4) is fixed.

9. The damping system according to claim 6, wherein the plate (3.2) comprises two fins (3.2.2) projecting outwards, between which there is arranged a sheet (3.2.3) to which at least one end of a lower shaft (3.3) is fixed, the other end of the lower shaft (3.3) being fixed to the plate (3.2) or to the sheet (3.2.3) and where the lower tie (4.3) is fixed to the lower shaft (3.3).

Description

DESCRIPTION OF THE FIGURES

[0030] FIG. 1 shows a perspective image of a preferred exemplary embodiment of the damping system of a solar tracker of the present invention.

[0031] FIG. 2 shows a profile image of the damping system shown in FIG. 1.

[0032] FIG. 3 shows a perspective image of the upper support shown in FIG. 1.

[0033] FIG. 4 shows a perspective image of the upper support from a different view than FIG. 3.

[0034] FIG. 5 shows a schematic image of the interior of the damper.

[0035] FIG. 6 shows a perspective image of the lower support of FIG. 1.

[0036] FIG. 7 shows a perspective image of the lower support from a different view than FIG. 6.

[0037] FIG. 8 shows a perspective image of the plate of the lower support of FIG. 6.

[0038] FIG. 9 shows a perspective image of another exemplary embodiment of the damping system of a solar tracker of the present invention.

[0039] FIG. 10 shows a profile image of the damping system shown in FIG. 9.

[0040] FIG. 11 shows a perspective image of the upper support of FIG. 9.

[0041] FIG. 12 shows a profile image of the upper support of FIG. 11.

[0042] FIGS. 13A and 13B show respective profile images of the damping system shown in FIG. 9 at different moments of the rotational movement of the solar tracker.

[0043] FIG. 14 shows a perspective image of the lower support shown in FIG. 9.

[0044] FIG. 15 shows a perspective image of the lower support from a different view than FIG. 14.

DETAILED DESCRIPTION OF THE INVENTION

[0045] The present invention relates to a damping system of a solar tracker (1), as can be seen in the preferred exemplary embodiment of FIGS. 1 and 2, the present damping system comprises at least one upper support (2) fixed to a rotation shaft (1.1) of the solar tracker (1), a lower support (3) fixed to a column (1.2) of the solar tracker (1) and a damper (4) attached at its ends to the upper support (2) and to the lower support (3).

[0046] Normally, the solar tracker (1) comprises an actuator to cause the rotation of the solar tracker (1), preferably located substantially in the middle of the rotation shaft (1.1), for a better distribution of the forces along the rotation shaft (1.1).

[0047] In a non-limiting manner, the present damping system would be installed at least at one end of the rotation shaft (1.1), even more preferably the damping system would be installed at both ends of the rotation shaft (1.1).

[0048] A better distribution of the forces exerted on the rotation shaft (1.1) by the actuator and the damping system is thereby achieved, improving the service life of the rotation shaft (1.1).

[0049] As can be seen in FIGS. 3 and 4, the upper support (2) comprises an omega-shaped upper clamp (2.1) configured to clamp the rotation shaft (1.1).

[0050] As a result of the omega shape of the upper clamp (2.1), the installation of the upper clamp (2.1) on the rotation shaft (1.1) is facilitated, since at the time of installation the operator only has to place the upper clamp (2.1) on an upper face of the rotation shaft (1.1) (the upper face of the rotation shaft (1.1) being understood to mean the face located opposite the ground at the time of installing the present damping system), allowing gravity itself to keep the upper clamp (2.1) clamping the rotation shaft (1.1).

[0051] Likewise, the upper clamp (2.1) comprises two pairs of ribs (2.1.1), each pair of ribs (2.1.1) being fixed to one side and to the wing with which said side is fixed, thereby achieving a better distribution of the efforts to which the upper clamp (2.1) is subjected, increasing the service life thereof.

[0052] In addition, the upper clamp (2.1) comprises two openings in each wing for the passage of attachment means (for example, screws, rivets, etc.) for fixing both wings to the same lever (2.2).

[0053] The rotation shaft (1.1) is thereby compressed by the upper clamp (2.1) and the lever (2.2) when tightening said attachment means, securing the upper support (2) to the rotation shaft (1.1).

[0054] Said lever (2.2) has an inverted U-shaped profile, comprising respective openings on its central surface for the passage of attachment means for fixing the lever (2.2) to the wings of the upper clamp (2.1).

[0055] It should be noted that, although this preferred example mentions that the lever has an inverted U-shaped profile, it is not ruled out that the lever can have a U-shaped, C-shaped, H-shaped, square-shaped, etc., profile.

[0056] In this preferred exemplary embodiment, the lever (2.2) comprises at its end furthest away from the rotation shaft (1.1) a fixing point on each wing of the lever (2.2) for the installation of an upper shaft (2.3), through which the damper (4) is fixed.

[0057] The upper shaft (2.3) is thereby supported at both ends, instead of just one, therefore a better distribution of efforts is obtained, thereby increasing the service life of the damping system. More specifically, the damper (4) comprises at one of its ends an upper tie (4.2), for the attachment between the damper (4) and the upper support (2), and at its other end a lower tie (4.3) for the attachment of the damper (4) to the lower support (3).

[0058] Said upper tie (4.2) comprises an opening for the passage of the upper shaft (2.3), thereby achieving the transmission of the rotational movement of the rotation shaft (1.1) to the damper (4) in a linear manner and achieving that the damper (4) has an angular movement between the damper (4) and the lever (2.2).

[0059] The damper (4) can be a hydraulic cylinder, of the type comprising a rod (4.1) at one end of the damper (4) and where the rod (4.1) extends and contracts in the longitudinal direction of the damper (4).

[0060] As can be seen in FIG. 5, the rod (4.1) comprises at one of its ends (specifically at the end that is located inside the damper (4)) a piston (4.1.1), which separates two chambers (4.1.2) filled with hydraulic oil, both chambers (4.1.2) communicating with one another by means of holes (4.1.3) present in the piston (4.1.1).

[0061] In this way, when the rod (4.1) extends or contracts, it forces the passage of hydraulic fluid between both chambers (4.1.2) through the holes (4.1.3), which only allow a maximum flow of hydraulic fluid.

[0062] Therefore, in the event of a sudden rotation of the rotation shaft (1.1), the flow of hydraulic fluid exceeds this maximum flow of hydraulic fluid, blocking the extension or contraction of the rod (4.1), thus damping the rotation of the rotation shaft (1.1).

[0063] In this preferred exemplary embodiment, the rod (4.1) comprises at its end opposite the piston (4.1.1) the upper tie (4.2), however, it is not ruled out that instead of this, the rod (4.1) comprises at its end opposite the piston (4.1.1) the lower tie (4.3).

[0064] As can be seen in FIGS. 6 and 7, the lower support (3) comprises an omega-shaped lower clamp (3.1) configured to clamp the column (1.2) of the solar tracker (1).

[0065] Said lower clamp (3.1) comprises at its ends openings for the passage of the attachment means (which can be screws, rivets, etc.) for the fixing thereof with a plate (3.2), although it is not ruled out that the lower clamp (3.1) is fixed to the plate (3.2) by welding.

[0066] The column (1.2) is thereby compressed by the lower clamp (3.1) and the plate (3.2) when tightening said attachment means, securing the lower support (3) to the column (1.2).

[0067] As can be inferred from FIG. 8, the plate (3.2) comprises a flat surface (3.2.1) from which there protrude at least two fins (3.2.2) transversally to the flat surface (3.2.1) and in the opposite direction with respect to the column (1.2), both fins (3.2.2) being parallel to one another. A sheet (3.2.3) is fixed between said fins (3.2.2), the sheet (3.2.3) being U-shaped in this preferred exemplary embodiment.

[0068] The sheet (3.2.3) comprises at each end an opening for the installation of a lower shaft (3.3), through which the lower tie (4.3) of the damper (4) is fixed.

[0069] For this purpose, the lower tie (4.3) comprises an opening for the passage of the lower shaft (3.3), thereby achieving that the damper (4) can have angular movement between the damper (4) and the column (1.2).

[0070] With all this, once the rotation shaft (1.1) performs a rotational movement, such movement is transmitted longitudinally to the damper (4), which in the event that the rotational movement is normal, the damper (4) does not prevent said movement, but in the event that said rotational movement is sudden, the damper (4) blocks the rotational movement of the rotation shaft (1.1) of the solar tracker (1).

[0071] FIGS. 9 and 10 show another exemplary embodiment of the present invention, in which the damping system comprises two dampers (4).

[0072] Both dampers (4) are attached by their respective upper ties (4.2) to the lever (2.2) of the upper support (2) and by their respective lower ties (4.3) to the plate (3.2) of the lower support (3).

[0073] As can be seen in FIGS. 11 and 12, the lever (2.2) of the upper support (2) comprises two ends protruding from the rotation shaft (1.1) and where an upper shaft (2.3) is fixed at each end.

[0074] Likewise, it can be seen in said figures that the two ends of the lever (2.2) protrude equidistantly on both sides of the rotation shaft (1.1), although it is not ruled out that said ends protrude non-equidistantly on both sides of the rotation shaft (1.1).

[0075] As in the previous exemplary embodiment, each upper shaft (2.3) is fixed at each end to a different wing of the lever (2.2), preventing the upper shaft (2.3) from being supported at only one end, therefore a better distribution of efforts is obtained, thereby increasing the service life of the damping system.

[0076] As can be seen in FIGS. 13A and 13B, during the rotation of the rotation shaft (1.1) while the rod (4.1) of one of the dampers (4) extends, the rod (4.1) of the other damper (4) contracts, thereby doubling the ability to block the rotational movement of the rotation shaft (1.1) in the event of a sudden rotation.

[0077] In this exemplary embodiment, the lower support (3) comprises a lower clamp (3.1) which in turn comprises two sub-clamps (3.1.1) with an L-shaped profile superimposed on one another, being fixed to the column (1.2) and clamping same by means of tightening means (3.1.2) (for example, bolts), as can be inferred from FIGS. 14 and 15.

[0078] The column (1.2) is thereby compressed by the sub-clamps (3.1.1) when tightening said tightening means (3.1.2), without the need for a plate (3.2) to tie the lower support (3) to the column (1.2).

[0079] This also allows the lower clamp (3.1) to clamp columns (1.2) of different shapes (for example, H- or U-shaped) or sizes, which in turn increases the flexibility of the installation of the damping system.

[0080] Likewise, it is not ruled out that the lower shaft (3.3) is fixed to the superimposed wings of the sub-clamps (3.1.1), the lower tie (4.3) being fixed to the lower shaft (3.3).

[0081] Preferably, on the superimposed wings of the sub-clamps (3.1.1) there is fixed a plate (3.2) (for example, by means of screwing, welding, etc.), in which the lower tie (4.3) of the damper (4) is fixed.

[0082] As can be inferred from FIGS. 14 and 15, the plate (3.2) comprises a flat surface (3.2.1) from which there protrude at least two fins (3.2.2) transversely to the flat surface (3.2.1) and in the opposite direction with respect to the column (1.2), both fins (3.2.2) being parallel to one another.

[0083] A sheet (3.2.3) is fixed between said fins (3.2.2), the sheet (3.2.3) having a flat surface in this preferred exemplary embodiment.

[0084] The sheet (3.2.3) comprises two openings for the installation of respective lower shafts (3.3), where the lower shafts (3.3) are fixed at one end to the sheet (3.2.3) and at the other end to the plate (3.2), each lower tie (4.3) of both dampers (4) being fixed to the respective lower shafts (3.3).

[0085] Both lower shafts (3.3) are thereby prevented from being supported at only one end, therefore a better distribution of efforts is obtained, thereby increasing the service life of the damping system.