FIELD OF THE INVENTION The present invention is encompassed in technologies relating to surface assembly and control systems for assembling and controlling surfaces, especially reflective surfaces, made up of different units or facets, such as reflective elements used in solar concentration technologies or other technologies that require high precision for orientating surface elements that form a larger surface. More specifically, the invention relates to canting control systems for heliostats or parabolic troughs installed in solar power plants for power production.

PRIOR ART Since the beginning, techniques of using solar energy have mainly aimed at increasing the intensity of captured solar radiation for later use. Initially, said increase was intuitively brought about by trial and error methods. Nevertheless, this technical problem has later been approached scientifically, leading to systems with higher concentration of incident solar radiation on collection structures, thus allowing thermal conversions of greater efficiency, according to the principles of thermodynamics.

Central tower concentrating solar technologies consist of a solar field, usually made up of structures with several individual mirrors forming a large spherical or parabolic cap, in which focal point a fixed receiver is placed. By means of this distribution, incident solar radiation falling on the reflectors that follow solar movement, known as heliostats, is concentrated and focused on a receiver at the top of the tower. Therefore, the receiver absorbs the received radiation and transfers it, in the form of thermal energy, to a transport fluid called heat transfer fluid to be used directly in the corresponding thermal or thermodynamic process or to be stored as thermal energy that can be used later.

Generally, heliostats forming the solar field or collector subsystem have the capacity of tracking in two axes, known as azimuth or axis of rotation and zenith or axis of inclination with respect to the horizontal. Freedom of movement on both axes therefore ensures that the reflected radiation falls on the suitable area of the receiver, regardless of the position of the sun. On the other hand, the precise aiming of the reflected radiation depends on the relative position of the reflecting surface and the incident radiation, hence the importance of a precise orientation of the facets with each other, in order to a further concentrate the radiation on the receiver. It must be kept in mind that facets are the surface elements that reflect the solar radiation received by the heliostat. In this context, a small angular error in the inclination of the reflective surfaces results in a corresponding deviation of the reflected beam, which depends on the distance to the receiver and on said angular error.

On the other hand, canting is the method whereby surface elements or facets of the solar concentrator are individually oriented or tilted, providing them with a suitable inclination, generally by means of respective angles with respect to the horizontal in perpendicular axes defining a reference plane coinciding with the surface to be leveled. Photovoltaic systems do not require performing this canting operation, these technologies do not concentrate the radiation on any focal point. However, when it comes to heliostats, the main technical purpose is to generate a focal point with the heliostat to further concentrate the reflected energy. Nowadays, for parabolic trough (PT) applications, the canting method, or spatial orientation of the facets, is performed by means of using duly machined molds or jigs on which the facets are deposited and then fixed to the structure that is supported on them. Additionally, this method usually includes a flipping operation, which involves complete rotation of the reflective surface that varies typically between 2 m and 10 m square in commercial designs, with subsequent disruptions due to load variation, time loss and execution risks. Since the canting is performed with the inverted reflective surface, gravity loads must be considered in the previous calculations, and another reflecting surface position measurement or verification station is usually required.

The general prior art related to solar modules discloses several different solutions for positioning the effective surfaces that interact with the solar rays. For positioning these surfaces, stiff supports and an approximate orientation are required, since solar modules tolerate a positioning error very much higher than the one that heliostats can assume, due they do not aim to focus radiation on a focal point. However, heliostats aim to concentrate the reflected solar radiation on a focal point, where is the receiver. This is the case, for example, of the systems described in the applications KR 101427764 B1 (Suntrek Co. Ltd.), EP 2327941 A1 (J. A. Lahora Cruz) and US 2010/236183 A1 (Paul R. Cusson et al.), which refer to three-dimensional (3D) static structures acting as supports where the effective surfaces or solar collectors are arranged at certain orientations or angles towards the sun. In the applications EP 2339262 A2 (Solid Enginyeria SL) and US 2012/125401 A1 (William J. Devillier), several three-dimensional (3D) structures acting as supports are disclosed, where the effective surfaces or solar modules are arranged and can be orientated towards the sun around one and two axes, respectively. One example of heliostat applications is WO 2005/040694 A1 (RAMEM SA et al.), which is a three- dimensional (3D) structure acting as support where the reflective are arranged and can reflect the sun on the receiver. However, all these cases are based on structural supports, either fixed or movable around one or two axes, which are not within the scope of the present invention.

The object of this invention is a system specially designed to position correctly the facets or surface elements of a tracker in the needed relative angle with a high accuracy and saving assembly time, during the assembly process of said tracker. Therefore, the tracker and the canting system are not the same structures, having different functions and being only related in that the canting system is an auxiliary system used during tracker assembly to improve the assembly process and the final tracker performance. For heliostat type solar trackers the common method for canting and orientating the surface elements or facets is carrying out a complex iterative adjustment with the help of external measurement elements. These methods involve the use of equipment with a high cost and high risks of positioning errors or induction of deformation in the facets. With the aim of providing further precision means and in order to reduce errors in concentration systems, the state of the art comprises various designs of heliostats with improved rigidity, as well as suitable systems for assembly and canting, as illustrated by the following references: Patent application US 4502200 (Atlantic Richfield Co.) relates to a heliostat made up of several facets formed by mirrors attached to folded metallic sheets, which provide rigidity to the reflecting surface. These facets are attached to the heliostat structure by means of using threaded rods and sets of spherical nuts and washers. This type of connection allows the anchors to pivot slightly, reducing anchor stresses. However, the mentioned document does not indicate how the canting level is measured, nor does it indicate the attachment positions corresponding to the improvement of solar concentration.

Patent application EP 2410259 (Sener Ingenieria y Sistemas, S.A.) shows a discrete heliostat canting system by means of using grooved washers and a set of threaded rod and nuts. Said canting has to be done manually at each anchoring point of the facets. The main disadvantage of the discrete canting method is the existence of a high minimum canting error, characterized by the minimum thickness of the grooved washers. In fact, the patent application itself sets the adjustable minimum error at 1 mm; a value much higher than necessary in this kind of systems. In addition, vibrations of the structure, whether due to wind or other causes, can reduce the preload of the system, causing complete loosening thereof, the canting level being able change unpredictably or even causing parts, especially the grooved washers, to come off. Another disadvantage of this system is the large amount of time required for a correct canting because it is a trial and error method in which the position of all facets must be measured after each adjustment performing corrections iteratively to get closer to the tolerance.

Patent application WO 201 1/083197 (Urssa Energy, S.L.) proposes a parabolic trough solar collector and a method of assembly thereof, but does not include or propose any positioning system and the subsequent attachment of the reflecting surfaces without changing their correct position, or for verification of the canting performed.

Patent application WO 2012/02441 1 (Sundrop Fuels, Inc.) shows a cable-driven heliostat moving on a ring. The reflecting surface is attached by means of pre-configured brackets and fixed shim kits. Finally, patent application WO 2014/075821 (Termopower, S.L.) proposes a system for measuring the reflective surfaces of heliostats or parabolic troughs by means of using a gantry with measurement sensors which moves over the surface to be measured. The system included in said application has, as analyzed, several technical disadvantages among which the following must be mentioned:

- The canting depends on the manual skills of operators who must be able to attach the facets in the suitable position following the live measurements, for which purpose there is a need to have separate displays for each sensor. This system does not allow the adjustment of all facets of the heliostat at once, which is a waste of operation time. - In case of misalignment of any measuring apparatus, the error will propagate without any means of immediate detection. The only option is the frequent position measurement by means of external precision instruments, which leads to system shutdown while verification is done.

- The canting process needs an additional amount of time spent on moving the measurement gantry from one row of facets to another because in each position only the facets forming the row can be adjusted. - They are complex systems due to the large number of moving parts they possess. This complexity entails higher manufacturing and installation costs.

- Since the gantry, with the measuring elements, must be moved and positioned in different positions assured by external fixed stops, it is necessary to frequently check that the positioning is correct using external measurement equipment. Each position defines a plane which will be different for each row to be canted with respect to the canting reference plane or midplane, so this method induces an error typical to canting due to the design thereof.

- Only one row of facets can be simultaneously attached and adjusted due to the very nature of the mobile gantry systems, with the influences it has on the canting time for each heliostat. Furthermore, for each row that is adjusted simultaneously, the slowest station determines the cycle time spent on the operation, since the gantry does not move until the entire row is adjusted.

- Gantry systems with active measuring elements have the disadvantage of simultaneously contacting the reflecting surface generating vibration thereof and inducing deformation due to contact force of said elements, this load is additional to the actual gravity load of the heliostat with the subsequent error or inaccuracy in the process. The present invention is presented as a technical solution that improves the known systems and rectifies their associated problems by means of a novel assembly and canting system for assembling and canting solar concentrating reflective surfaces.

BRIEF DESCRIPTION OF THE INVENTION

An object of the present invention is to obtain technical means which allow reducing time and effort, improving angular accuracy, placement and canting of surface elements that form a given surface, such as a solar concentrating reflective surface. For this purpose, the system of the invention consists of a structure, rigid enough to not undergo shape changes during use, covering the entire surface to be assembled. This structure contains a series of preferably adjustable physical stops located at the points of interest to be controlled during assembly or canting.

It is worth recalling that the system of the invention does not refer to the tracker/heliostat structure itself, where the facets are arranged at a given position (as happens with the systems disclosed by the previously mentioned applications KR 101427764 B1 , EP 2339262 A2, US 2010/236183 A1 , EP 2327941 A1 , US 2012/125401 A1 or WO 2005/040694 A1 , which refer to 3D fixed or movable structures where the surfaces are arranged), but to an auxiliary canting structure to be positioned above a heliostat or tracker structure covering it, in order to provide a plurality of external canting reference points over the surface to be canted. These canting reference points define the final orientation and relative angles of the individual facets between themselves, and can be modified in order to define different canting groups (different heliostat configuration depending on the actual heliostat position in the solar field). Therefore, the focal length of the tracker can be changed during its assembly. Once the canting operations have been duly performed, the canting structure of the invention is removed and the heliostat can be installed in the solar plant.

In a main embodiment of the invention, the surface to be canted comprises one or more heliostat facets and, more preferably, the arrangement of canting control nodes coincides with the positions of the vertices of said facets to be canted, if their connecting elements are located at said points. Otherwise, the physical stops will preferably be located as close as possible to the area where the facet anchoring points are located, in order to avoid inducing deformations and to reduce canting errors. In a preferred embodiment of the invention, the system described is used for assembling and canting reflective surfaces of the type forming part of a solar concentrator. More preferably, said system comprises a three-dimensional canting structure configured to be located in a space larger than that of the reflective surface and a plurality of canting control nodes arranged in said three-dimensional canting structure. Advantageously, the control nodes of the system comprise one or more physical canting stops, formed as substantially fixed elements, where the positions of said stops are adjustable for defining canting reference points on the surface to be canted, when the latter is located in a space smaller than that of the three-dimensional canting structure and each canted element is in contact with the physical canting stops defining the desired final position thereof. One benefit of this system is that not all the physical stops contact the reflecting surface simultaneously or apply force thereon, during operation, facets are displaced to the stops without virtually applying any force thereon, which improves the accuracy of the final canting. In another preferred embodiment of the invention, the control nodes are arranged in the intersection of a plurality of bars, of profiles attached by means of welding or of connecting elements threaded or connected by rivets. More preferably, the control nodes are arranged at regular distances in the three-dimensional canting structure to provide uniform canting reference points along the surface to be canted. In another preferred embodiment of the invention, the three-dimensional canting structure is made up of a plurality of substructures to cover the entire surface to be canted.

In another preferred embodiment of the invention, each control node comprises a support or plate or system where physical canting stops are installed. The support plates preferably comprise a plurality of housings for said physical canting stops. Likewise, the support plates can contain anchoring points for the control nodes, seats for structural bars, ribs and/or geometric reinforcements to stiffen said support plates.

In another preferred embodiment of the invention, the canting physical stops are attached to the support plates by means of sets of washers, nuts and locknuts located on both surfaces of the support plate or system. More preferably, attachment of physical canting stops to the support plate comprises a preloaded spring the position of which controls the height of canting. This height can be adjusted by means of a fine thread nut, for example, separated from the support plate by a washer or blocked by means of a setscrew, a chemical nut fastener or a locknut system. Alternatively, each physical canting stop can comprise a casing which is attached to a housing on the support plate by means of a setscrew preventing said casing from moving.

In an additional preferred embodiment of the invention, the physical canting stops have a contact control means for marking the canting positions of the reflective surface, said means comprising an inductive pressure or contact sensor or a load cell.

In another preferred embodiment of the invention, the physical canting stops comprise, in its upper region, a cap with one or more surfaces adapted for measurement by external optical verification means. More preferably, the physical canting stops comprise both in the upper cap and on the contact surface with the surface to be canted, receivers suitable for measurement by external optical verification means.

Another object of the present invention relates to an assembly and canting method for assembling and canting a surface made up of a plurality of surface elements, for example of the type forming part of a solar concentrator, which comprises using the system according to any of the embodiments described herein.

Said method preferably comprises the following steps:

- configuring the position of the physical canting stop in the three-dimensional canting structure according of the final surface shape to be obtained;

- positioning the surface to be canted under the three-dimensional canting structure, moving it close enough to the canting control stops ensuring that there is no contact with them in this step. The surface to be canted has been pre-positioned in a previous operation on its support structure, in order to preload the system and so that it adopts deformations the different loads induce on the structure;

- positioning each surface element by manual or automatic means until it contacts all the physical canting stops. This operation can be done simultaneously on all surface elements to be canted;

- verifying that each surface element makes contact with physical canting stops that correspond to it, by means of using optical measuring systems, by direct measurement with any of the described sensors or other sensors existing in the state of the art suitable for this application. This operation can be done simultaneously on all surface elements to be canted;

- finally, separating the canted surface and the three-dimensional structure that contains the physical canting stops by a vertical movement and then the removing heliostat from the canting station.

During the assembly and canting operations, either the support structure of the surface to be canted or the structure of the system of the invention, are movable with respect to one other in order to make the relative positioning to each other easier. Preferably, the structure of the system of the invention is static, whereas the support structure of the surface to be canted is movable. Once the assembly/canting of the surface to be canted is done, they are disengaged again. The system and method of the invention allow verification of the position of each of the physical canting stops, for example, as a step prior to canting the surface elements. The position of the physical stops can be verified either by the upper part of the structure by using bars or rods of known length, which are inside the physical stop and integral with it, that define a plane parallel to that defined by physical canting stops, or alternatively by the lower part, verifying the contact area of the physical stops. Furthermore, the verification process can be done manually or automatically, for example using optical measuring equipment.

Although the present invention is preferably applicable to solar concentrating systems, it can also be applied, with appropriate modifications, to other fields requiring high accuracy in positioning and attaching surface elements, as well as other techniques that require accurate reflection of radiation, such as photovoltaic concentrator (PVC), solar ovens, water treatment, photochemical reactors, steam generators or processes that exploit solar energy for heating materials. DESCRIPTION OF THE DRAWINGS

Figure 1 shows a general perspective view of the canting system of the invention according to a preferred embodiment thereof, applied to heliostat facets.

Figure 2 shows a detailed view of figure 1 , in which part of the structure of the canting system has been cut off in order to allow viewing the position of the facets.

Figure 3 is a plan view of the canting system of the invention according to a preferred embodiment thereof, where the arrangement of the nodes and canting stops can be seen. Figures 4, 5 and 6 detail different embodiments of the arrangement of nodes distributed in the structure of the invention including the support plates of physical canting stops.

Figures 7, 8 and 9 show different embodiments of the support plates of the invention made by stamping, machining and injection, respectively.

Figures 10 and 1 1 show two different methods of attaching physical canting stops to support plates as well as the geometric arrangement of the physical canting stops on said plates. Figures 12 and 13 show the detail of two different embodiments of the canting stops of the invention.

REFERENCE NUMBERS OF THE DRAWINGS

(3) Facet or surface element

(4) Canting control node

(5) Physical canting stops

(6) Structural bars

(7) Support plate

(8) Housing for physical canting stop

(9) Anchoring point

(10) Seat for bars of the three-dimensional canting structure

(1 1 ) Geometrical reinforcement of the support plate

(12) Raw support plate

(13) Support plate after manufacturing process

(14) Washer

(15) Nut

(16) Strengthening bushing for housing the physical canting stop

(17) Spring

(18) Nut

(19) Washer

(20) Lower cap

(21 ) Casing

(22) Setscrew

(23) Upper cap

(24) Measurement surface

(25) Upper area of the physical stop

(26) Physical canting stop

(27) Laser radar optical receiver

(28) Washer

(29) Nut

(30) Spring inside the physical canting stop

(31 ) Contact or position sensor

(33) Physical canting stop casing

DETAILED DESCRIPTION OF THE INVENTION

As described in the preceding paragraphs, the present invention is proposed with the of promoting the correct assembly and canting of surface elements that make up a larger area, such as facets of a heliostat or other solar systems such as a parabolic trough or, in general, for the proper arrangement of a plurality of surface elements with respect to a predefined joint surface, that allows saving time and effort in placing surface elements that make up a larger surface, with the corresponding reduction in human and economic costs and positioning error, improving the performances of said surface.

Therefore, the invention is based on the use of a single system for canting all surface elements forming the surface to be canted, such as the surface formed by the facets of a heliostat, in which the canting operation can be developed simultaneously in all surface elements, if desired, in which the canting can be verified in real time, and in which the operators or robots need only to slightly move the surface elements vertically until they contact a plurality of physical stops, proceeding then with the attachment thereof. This way, the proposed canting structure is configured to cover the entire surface to be canted.

In the context of the present invention, the term "covers" shall be interpreted as to be put above, on top of, or in front of the surface to be canted, in order to provide a larger surface which spreads over or on top of said surface, which will allow one or more operators to use the plurality of canting stops, previously set (defining the appropriate canting setup for the heliostat facets), as reference points for canting the surfaces. Therefore, operators just need to push de facet versus the canting stop and fix it, instead of measuring and adjusting iteratively the different facet angles to fit the desired configuration.

These physical stops comprised in the canting system are preferably adjustable in height, in order to allow adjusting the system for different relative positions of the surface elements. The physical stops are preferably located in the vertical of the points of the surface elements to be controlled. For example, for a plurality of facets forming the reflective surface of a heliostat, the physical stops can be located in the vertices of the facets, the latter being an optimum arrangement which entails a smaller positioning error if their attachment points are in those positions. Otherwise, the physical stops will preferably be located as close as possible to the area where the facet anchoring points are located, in order to avoid inducing deformations and to reduce canting error.

The structure and supports thereof will be designed to allow expansion along both axes to occur without restriction and in a centered and symmetrical manner, thus preventing bending loads that may change the relative position of the physical canting stops. The canting system and canting objects of this invention are describe in detail below according to the embodiments shown in Figures 1-13 of this document: As shown in Figure 1 , the canting system of the invention is preferably based on a three- dimensional canting structure (1 ) the horizontal surface of which is larger than that of the surface to be canted. Said three-dimensional canting structure (1 ) is configured to be located in a space larger than that of the canting surface (for example, it can be located above a heliostat positioned in a horizontal orientation). This three-dimensional canting structure (1 ) is stiff enough so that the shape thereof does not change during use or degrades over time. Typical elements having a modular structure, such as bars, beams, supports and fittings thereof, can be used for manufacturing same. In a preferred embodiment of the invention, this structure is static and has a plurality of supports that allow movement, insertion and removal of the surface to be canted. These supports allow unrestricted, centered and symmetrical expansion of the three-dimensional canting structure (1 ) along the main axes, avoiding deformation of the structure and change in the relative position of the physical canting stops (5) when the environmental temperature changes. Figure 2 shows a heliostat support structure (2) located in the space smaller than the three-dimensional canting structure (1 ), preferred embodiment of the invention. As shown in the drawing, said upper structure (1 ) covers a larger area than the heliostat support structure (2). The latter in turn has a vertical displacement system that allows inserting the support structure (2) together with the facets (3) supported thereon under the three- dimensional canting structure (1 ) without risk. This vertical displacement system can be any one of those existing on the market today, since the heliostat support structure (2) preferably has rest supports at appropriate points of its perimeter or, preferably, at its central point, depending on the heliostat design, thus eliminating the need for precision in the vertical displacement system.

As shown in Figure 3, in a top view of the three-dimensional canting structure (1 ), it also comprises a plurality of canting control nodes (4), preferably regularly arranged along the horizontal surface of the structure (1 ). More preferably, the arrangement of control nodes (4) coincides with the positions of the anchoring systems of the facets or surface elements (3) to be canted. Advantageously (Figures 4-6), the control nodes (4) of the system of the invention comprise one or more physical canting stops (5), formed as substantially static elements, the function of which is to block vertical displacement, i.e., being a physical stop, when making contact with the facets (3), thus marking the canting positions thereof, with the preferred possibility of containing auxiliary elements, which can be pivoting or vertically movable, with the function of detecting contact of the facet against the stop.

Therefore, controlling the relative position of the physical stops (5) allows deriving the canting positions of the facets (3) for subsequent implementation by operators or systems adapted for this purpose.

For installation in the three-dimensional canting structure (1 ) of the invention, it is possible to arrange the control nodes (4) preferably at the intersection of a plurality of structural bars (6), preferably by screw means, in order to simplify the assembly of the three- dimensional canting structure (1 ). However, the system of structural bars (6) is not the only method for building said structure (1 ), also being able to be manufactured, for example, with different profiles connected by means of welding, connecting elements such as screws or rivets, or any other method existing in the state of the art to enable constructing a three-dimensional canting structure (1 ) as described. The control nodes (4) can also be arranged in another location of the three-dimensional canting structure (1 ); although for economic reasons its preferred location is at the intersections of the structure (1 ), as discussed above.

Each control node (4) is in turn preferably provided with a support plate (7) where the physical stops (5) are installed, although use of double nuts or other suitable systems for attaching said physical canting stops (5) is also possible. These support plates (7) can be manufactured in various ways, as desired, such as stamping, machining or injection, for example, as can be seen in Figures 7, 8 and 9, respectively. The proposal of these manufacturing methods does not exclude other possibilities, such as forging or casting.

Figures 7, 8 and 9 show the different main elements that are defined in the support plates (7) in terms of the different manufacturing methods. Said elements can be used, individually or in combination, in different preferred embodiments of the invention, and preferably comprise housings (8) for the physical canting stops (5), anchoring points (9) for the control nodes (4), seats (10) for structural bars (6), ribs or geometric reinforcements (1 1 ) to stiffen the support plate (7). Regarding the shape of the support plate (7) itself, it is shown in Figures 8 and 9 both as a machined support plate (12) and as injection molded plate (13).

The presence of seats (10) for the threaded rods (6) prevents rotation or displacement of the support plate (7), thus increasing the stability of the canting system over time.

Figures 10 and 1 1 of this document show the vertical geometric arrangement of the physical canting stops (5), while Figures 12 and 13 show in more detail different possible configurations thereof. More specifically, Figures 10 and 13 show a set of physical canting stops (5) the attachment system of which for attachment to the support plate (7) is based on the use of sets of washers (14) and nuts (15) on both surfaces of the bushing (16) of the support plate (7) serving as a housing (8) for the physical canting stops (5). In this embodiment, changing the canting groups or relative distances between reference points of the same facet (3) is performed by means of adjusting and tightening both sets of connections from both sides of the bushing (16) of the support plate (7).

Figures 1 1 and 12 in turn show a system using a physical canting stop (5) the attachment system of which for attachment to the support plate (7) is based on the use of a duly preloaded spring (17) between a washer (19) and a nut (18) and the housing (8) of the physical canting stop (5) in the support plate (7). The height of canting can be adjusted by means of a nut (29), preferably with fine thread, separated from the housing (8) of the support plate by a washer (28) or blocked by means of a setscrew, a chemical nut fastener or a locknut system, for example, as desired. If necessary, the spring (17) can be compressed or decompressed by means of using the nut (18) and washer (19), configured for this purpose. In any case, the spring (17) must lift the physical canting stop (5), a movement that is blocked and controlled by the adjusting nut (29).

As described above, the mode of operation and usefulness of physical canting stops (5), irrespective of its attachment system, is to provide a physical stop system against which the surface to be canted moves (for example, the facets (3) of a heliostat). In a preferred embodiment of the invention (Figure 12), said physical canting stops (5) have contact control means (31 ) integrated with or incorporated to the physical stop, such as an inductive pressure or contact sensor; a load cell or any other related system that serves to alert the operator that he has reached the desired physical canting stop. Each physical canting stop (5) preferably comprises a casing (21 ) fixed to its housing (8) in the support plate (7) by means of a setscrew (22) which ensures, together with the adjusting nut (29), that said casing (21 ) is not displaced. The physical stop will therefore act when the lower cap (20) is pushed and vertically displaced by the surface element or facet (3) until it contacts the casing (21 ), at this moment, its rigidity will prevent the facet (3) from displacing further, ensuring its correct position, and the detector (31 ) will signal that contact is occurring. In a preferred embodiment of the invention, the physical canting stops (5) contain therein a spring (30), or functionally similar system, to ensure that when the facet (3) does not push the cap (20) of the physical stop (5) against the casing (21 ), the cap (20) is separated from said casing (21 ) and correct positioning signal will be interrupted. As an alternative, the detector is a measurement device that provides an actual measurement of the distance between the cap (20) of the physical stop (5) and the casing (21 ), allowing the operator to arrange the surface element, avoiding impacts between the surface element (3) and the physical stop (5).

Additionally, the canting system of the invention presents the possibility of accurately verifying the position of the physical canting stops (5) by external optical means, which are not affected by the unlikely deformations of the three-dimensional canting structure (1 ), and which allow verification before, during and after canting process, as desired. Verification systems that are preferred are photogrammetry, laser radar, laser tracker, measurement laser systems, or any other suitable optical measuring means from those commonly used in the state of the art.

For the use of these optical systems, the three-dimensional canting structure (1 ) preferably has numerous gaps and openings, sufficient to ensure the physical canting stops (5) are visible from the upper and lower parts of the structure and directly from many points of the perimeter. Therefore, depending on the desired verification system, the position of the physical canting stops (5) can be verified from a single external point or from several points, as appropriate. To make this possible, the physical canting stops (5) are easily adaptable in their configuration. As an example of the mentioned embodiment, Figure 12 shows a physical canting stop (5) fixed by a spring system (17) and adjusting nut (29). The rigid body has an inner rod connecting the cap (20) of the physical canting stop (5), going through the casing (21 ) of said stop (5) to its upper part, with the upper part of the system, which has a cap (23) with, for example, a surface (24) adapted for photogrammetric measurement. The actual position of the controlled canting points could therefore be determined by photogrammetry technique, from the upper part of the system, by means of measuring a plane parallel vertically translated the corresponding length of the inner rod of the physical canting stop (5) and defined by a plurality of reference photogrammetric surfaces (24). These surfaces may also be located on the lower cap (20) for verification from the lower part of the system, with the peculiarity that it would not be a suitable system for verifying the position of the canting points while canting facets (3), whereas the other embodiments do not present this disadvantage. If control by means of a laser tracker or laser pointer is desired, for example, a device such as that shown in Figure 13 can be mounted. In this device, both the upper part (25) of the rod and the contact surface (26) for contact with the surface to be canted have receivers (27) suitable for use with said laser tracker.

The canting method by means of using the system object of the invention is described below according to a preferred embodiment of said method for canting a heliostat.

Once assembled the heliostat structure (2), which supports the facets (3), is positioned horizontally. Subsequently, all facets (3) to be supported thereon are deposited on the structure, the structure (2) bends as correspond as it is subjected to the load induced by the weight of said facets (3).

Next, the heliostat structure with the facets (3) supported thereon, is inserted below the canting system of the invention, under the three-dimensional canting structure (1 ). In this step, the support structure (2) of the facets (3), belonging to the heliostat, will be in its lowest position.

Once the heliostat structure (2) in held in the correct position under the three-dimensional canting structure (1 ) of the canting system object of the invention, said structure (2) is placed in a canting position, preferably supported on a central support or, alternatively, a plurality of perimetric supports. This measurement position requires lifting said support structure (2) to a predetermined distance with respect to the three-dimensional canting structure (1 ), in which no facet makes contact with the physical stop (5) but are at a suitable distance for proper canting.

At this time, operators or automatic systems can access the area smaller than the facets (3), below both structures; the three-dimensional canting structure (1 ) and the heliostat structure (2).

Then, each facet (3) is raised, pushing until contacting with the physical canting stops (5), or until the auxiliary sensor (31 ) (if one is used, for example, inductive means) actives a light signal or a warning sound to finally fix the canting in said position using the anchoring elements for facet (3). In a preferred embodiment of the invention, the sensors (31 ) existing in the physical canting stops (5) report the presence of contact between the physical canting stop (5) and the surface element or facet (3), ensuring that if all signals are activated at the end the attachment of the facet (3), all them will be located in the desired canting position. All facets (3) can be simultaneously canted and/or verified with the system object of the invention. Once the full heliostat is canted and the positions are verified, with the aid of auxiliary sensors, if any, the heliostat support structure (2) with the already canted facets (3) is lowered so that there is a sufficient distance with respect to the three-dimensional canting structure (1 ) to avoid collisions. Then the heliostat is removed, and the system is now available to be used again.

Prior to the introduction of the heliostat structure with the facets (3), after removing the latter, i.e., either between canting methods or during the performance thereof, the correct position of the physical canting stops (5) will be verified using suitable means according to the chosen system configuration. It is worth noting that, once the physical canting stops (5) are adjusted for the desired canting, the stops (5) keep their relative position constant, since neither the stops nor the support structure thereof move, so the canting obtained during canting operation will be very repeatable.

Some verification means, without excluding others, include photogrammetry, laser radar, laser tracker or measurement lasers used from the perimeter of the three-dimensional canting structure (1 ) or from the lower or upper part, as a means for verifying the position of the laser receivers (27) or the measurement surfaces (26). As already mentioned, the physical canting stops (5) may be provided with an electronic proximity switch, or, in a preferred design of the invention, an inductive measurement system. These auxiliary sensors can be integrally attached to the physical stop (5) or be an integral part of its design.