TR2022000204A2 - SOLAR TRACKING SYSTEM - Google Patents

Abstract

The invention relates to a solar tracking system (1) with one degree of freedom that enables the solar panels (5) to be aligned according to the position of the sun during the day.

Description

DESCRIPTION SOLAR TRACKING SYSTEM Technical Field The invention is generally related to solar energy. More specifically, though not exclusively, It is a solar tracking system that allows photovoltaic panels to be aligned with the sun during the day.

When more than one tracking system acts together in harmony, it depends on the purpose and field structure. Open land that will enable optimization in terms of productivity increase and/or land use, It is a solar tracking system that can be used on flat roofs and floating systems.

Known Status of the Technique The most basic solar tracking systems used today are single-axis ones. These systems, modules a series of solar modules around a fixed axis that provides orientation roughly toward the sun The fixed rotation axis of the mentioned single-axis trackers is vertical, horizontal or inclined. It may be at an angle.

An example design of a single-axis tracker that rotates a series of solar modules around the horizontal axis U58459249 Described in BZ. In this single-axis tracker design, multiple tracker units are mounted on a horizontal rotates in unison around its spin axis.

An example of a single-axis tracker that rotates a series of solar modules at an inclined angle around an axis Its design is described in BZ US7554030. In this fixed-tilt single-axis tracker design, multiple The tracker unit rotates in unison around a rotation axis with a fixed angle of inclination.

In both sample tracking systems, each tracking unit subgroup defines the main rotation axis of each tracking unit. It contains a structure that supports a series of solar modules rotating around two fixed rotation elements that define the solar module.

Actuators and clutches are used to force different subassemblies of monitoring units to rotate together. connects each other.

U58459249 Horizontal single axis tracking systems, an example of which is seen in BZ, are from east to west of the sun. It rotates roughly according to its movement. In this way, it is more efficient than fixed solar modules. But this The systems are installed horizontally on the ground at noon, when the sun's rays carry the most energy. Because of their location, they do not increase efficiency as much as other tracking systems. Additionally, these systems are 45° They function in regions located at angles greater than north and 45° south latitudes. they lose.

U58242424 Vertical single axis tracking systems exemplified in BZ are from east to west of the sun. It rotates roughly according to its movement. In this way, it is more efficient than fixed solar modules. But this Since the systems are positioned at a constant inclination angle, it is expected to increase efficiency at sunrise and They cannot provide sufficient productivity increase during sunset hours. In addition, these systems provide horizontal single-axis tracking They require more land use than other systems.

Inclined angle single axis tracking systems, exemplified in US7554030 BZ, are designed around a fixed horizontal axis. It provides a significant increase in tracking accuracy over rotating prior art single-axis trackers.

However, the kinetic effects of these constant tilt tracers rotating around an axis with an inclined angle movement is significant in self-shading losses between the solar modules of each tracker unit. This results in an increase in the land required for the facility. Also, don't come back Solar modules are not mounted perpendicular to the axis of rotation as this affects the capability. Rotation They must be adjusted in line with the axis. In this case, this type of tracking systems is more effective than others. They stay higher than the ground. This makes these systems more vulnerable to wind, It also makes it difficult to work on these systems.

In addition, with the help of two separate drive systems, called two-axis, the sun is controlled both in azimuth and in azimuth. and solar tracking systems designed to track the altitude movement most accurately. available. However, these systems require more complex mechanical and electronic parts than others. due to the inherent limitations of its movement in its design and the rate of increase in its cost. Accordingly, the productivity increase it provides remains very low. Also, during sunrise or sunset hours They need more space than others to fully absorb the low-energy sunlight.

By eliminating the negative aspects of the sun tracking systems mentioned above, to meet the sun's rays at the most optimized angle, to optimize land use and to It is called 1.5 axis, with the claim that it will be least affected by the wind loads. There is another system available in BZ U510619891. However, this system does not differ from the others given above. Unlike other systems, it works against weight. In the relevant patent, they are called lower and upper drive arms. There are two arms. While these arms change the azimuth angle of the system, they also change the tilt angle.

However, due to the nature of the system, the solar modules rotate on the axis they rotate during the change of their tilt angle. It is not fixed and its center of gravity is not on a fixed axis. As a result, both these arms The loads on both the connections and the relevant drive unit are increasing.

Additionally, in the mentioned 1.5-axis tracking system, the system is placed horizontally on the ground to be protected from wind loads. is being made. However, depending on the type and direction of the wind, this scenario may not provide complete protection. It does not provide. Additionally, where there are no restrictions on land use or 45° In regions located at angles greater than north and 45° south latitudes, this system There is no scenario to which it can be adapted.

In the document numbered TR 2016/04750, which is another document in the current technique, three-axis, high A sensitive, easy-to-install solar tracking device is explained. This invention; in solar energy systems, designed for tracking the sun with high precision, easy to install, moving center on the third axis It is a sun tracking device with (8), east (9), west (10), down (11), up (12) light sensors. Third Thanks to the moving middle (8), east (9), west (10), down (11), up (12) light sensors on the axis, it Fast focusing and perfect tracking are its main features. No programming or computers It works without needing a connection. The moving east (9), west (10), controlled by the invention Iogic circuit With the back and forth movement of the lower (11) and upper (12) light sensors in the Z axis (third axis), the solar It works by detecting light at different angles. However, the invention in question has a 3-axis movement logic. It is quite different from our invention. In the invention in question, solar radiation is directly applied on the X, Y and Z axes. The location of the module physically changes location, and in our invention, the height is changed axially. There is no replacement (by moving the entire solar module up/down).

Instead, it rotates around a vertical axis and tilts left/right/down/up in a horizontal plane. There are transactions.

Where restrictions on land use form the main basis and/or due to cost reasons, more Application flexibility for floating systems and roof uses where land use is required cannot be provided in these systems.

Purpose of the Invention The invention aims to solve the above-mentioned drawbacks or to make the use of the mentioned systems convenient. It aims to produce solutions to the situations mentioned where it does not exist. All mentioned systems, As mentioned, they are designed to be applied in certain scenarios. However, solar energy The diversity of uses and related applications of prior art single and dual axis tracking systems An alternative photovoltaic solar tracker that positively addresses the limitations listed above gives rise to the need for the system.

The main purpose of the invention is to increase the movement of the sun, land use and/or productivity during the course of the day. It is adjusted and followed in order to optimize.

Another purpose of the invention is to adjust the solar panels according to the movement of the sun from east to west. To create a solar tracking system that provides guidance and increases efficiency.

Another purpose of the invention is to use it in locations at angles greater than 45° north and 45° south latitudes. The aim is to create a solar tracking system that can be used effectively.

Another purpose of the invention is to increase the movement of the sun, land use and/or productivity during the course of the day. A solar tracking system that optimizes and increases efficiency by taking up less space has been created. is to put.

Another purpose of the invention is to prevent solar panels from causing losses by casting shadows on each other. The aim is to create a solar tracking system that does not give

Another purpose of the invention is to protect and protect against possible wind effects by reducing the distance from the ground. The aim is to create a solar tracking system that is easy to intervene and operate.

Another purpose of the invention is to create a solar tracking system suitable for open land, flat roofs and floating systems. is to put.

Another purpose of the invention is to use it in its position at sunrise and sunset and/or at any desired angle in its position from sunrise to sunset and/or in its position at noon. When it is moved to the possible angular rotation limits, it creates a geometric pattern with the sun's rays. The aim is to present a solar tracking system that is in an orthogonality relationship. For this relationship, the router The length of the arm and/or the support structure of the guiding arm from the point where the support structure connects to the carrier shaft the distance from which it is connected to the structure and/or the point where the carrier structure is connected to the ground, of the guiding arm The distance between the point where it connects to the ground and/or the distance from the ground depending on the bearing structure of the guiding arm. The height is regulated.

Another purpose of the invention is that the length of the directing arm allows the sun rays to be more effective compared to summer and winter months. A solar tracker that has a feature that allows it to be adjusted to receive it at the correct angle. to reveal the system.

Another purpose of the invention is to move more than one solar tracking system in harmony. The aim is to provide drivers with a solar tracking system that has a working drive mechanism.

The structural and characteristic features and all the advantages of the invention are shown in the figures given below and according to these figures. It will be understood more clearly thanks to the detailed explanation written with citations and this Therefore, the evaluation should be made by taking these figures and detailed explanation into consideration. is required.

Figures to Help Understand the Invention Figure 1. is various directional and isometric views of the solar tracking system that is the subject of the invention.

Figure 2A. Various direction, cross-section and isometric features of the support structure of the solar tracking system that are the subject of the invention their views.

Figure ZB. Various direction, cross-section and isometric dimensions of the carrier pole of the solar tracking system subject to the invention their views.

Figure ZC. Various direction, cross-section and isometric features of the carrier structure of the solar tracking system subject to the invention their views.

Figure 3. Various direction, cross-section and isometric views of the guiding arm of the solar tracking system subject to the invention. their views.

Figure 4. The length and/or length of the guiding arm of the solar tracking system of the invention The subject of the invention is the side views of the solar tracking system when its position is changed.

Figure 5A. length and/or length of the guiding arm of the solar tracking system of the invention In an example where the location is adjusted to increase efficiency, the sun tracking device is the subject of the invention. Front and top views of the system.

Figure SB. length and/or length of the guiding arm of the solar tracking system of the invention The subject of the invention is an example where the location is adjusted to reduce land use. Front and top views of the solar tracking system.

Figure 6A. length and/or length of the guiding arm of the solar tracking system of the invention The subject of the invention is an example where the location is adjusted to reduce land use. Front and top views of a group of solar tracking systems.

Figure GB. length and/or length of the guiding arm of the solar tracking system of the invention In an example where the position is adjusted to increase efficiency, a group of Front and top views of the solar tracking system.

Figure 7. In order to increase the space utilization and/or efficiency of the solar tracking system of the invention, These are various views of its suitability for rough terrain installation.

Description of Part References 1. Solar Tracking System . Solar panel . Support Structure 100. Construction 110. Fastener 120. Termination . Carrier Mast 21. First Axis of Rotation 22. Second Axis of Rotation 200. Lower Mile 210. Upper Shaft Bearing 220. Upper Mile 230. Mast . Bearing Structure 300. Support Foot 310. Lower Shaft Bearing 40. Directing Arm 411. First Joint Axis of Rotation 412. Second Joint Axis of Rotation 413. Third Joint Axis of Rotation 414. Fourth Joint Axis of Rotation 415. Fifth Joint Axis of Rotation 400th Arm 420. Upper Joint Set 421. First Joint 422. Second Joint 423. Third Joint 430. Lower Joint Set 431. Fourth Knuckle 432. Fifth Joint Detailed Description of the Invention The invention has been described with reference to various specific and preferred embodiments and techniques.

However, variations and modifications can be made within the nature and scope of the invention. must be understood. This invention, including those shown in the drawings or exemplified in the specification, It is not limited to embodiments which are given by way of example or explanation and are explained without limitation.

The scope of the invention will be limited only by the claims.

The invention is essentially a solar photovoltaic or daylight solar module (2) aligned to the sun during the course of the day. kinetic system, consisting of at least one viewer unit containing the sun's azimuth and tilt angles. It is a structured solar tracking system (1).

The visuals in Figure 1 show the solar module (5) collecting the sun's rays, the sun's rays during the day. It shows the topological structure of the solar tracking system (1), which allows it to be positioned according to its course.

Solar tracking system (1), support structure (10) that allows the said solar module (5) to be mounted Contains.

In a preferred embodiment of the invention, the said support structure (10) has the said solar panel on it. the construction (100) in which the modules (5) are placed and the said solar modules (5) It contains a termination (120) that enables its connection to the construction (10).

This solar tracking system (1) is an adjustable system on which solar modules (5) can be mounted. construction (100), solar panel containing terminations (120) to connect the solar modules to the construction A support structure (10) to which the module (5) will be mounted and a connection to connect this support structure (10). It contains elements (110).

The visuals in Figure 2 show the way the sub-elements of the invention work and the axes on which they will work. shows: The mentioned support structure (10), the beam to be adjusted according to the number of solar modules (5) it will carry, A carrier construction consisting of column, purlin and connecting elements to connect them (100) Said solar modules (5) are placed on the said carrier construction (100), where these solar modules are placed. (5) with ends (120) adjusted to prevent movement in any direction. It is assembled. (Figure 2A) The solar tracking system (1) also carries the said support structure (10) and connects it with the support structure. (10) allows the support structure (10) to move freely around the first rotation axis (21), which is the axis with which it is connected. It contains a carrier pole (20) that allows it to rotate.

This tracking system (1), with a certain arrangement of the invention, is located on the second rotation axis of the carrier pole (20). It can be adjusted to move by rotating around (22).

In a preferred embodiment of the invention, the drive that will give the carrier pole (20) rotational movement is the drive transmission mechanism that enables the transmission and the said drive transmission mechanism to be mounted on There is also a shock absorbing damping system that reduces the wind effect. This structure suddenly It is connected to the drivers in order to control the multi-solar tracking system (1) at the same time from a single center. It may also include a drive mechanism.

In the solar tracking system (1), by connecting the said carrier pole (20) to the ground, the carrier pole (20) freely around a second axis of rotation (22) - preferably perpendicular to the ground and the first axis of rotation (22) There is also a carrier structure (30) that allows it to rotate.

This tracking system (1) is placed on the ground (for example, on a concrete structure) with the said bearing structure (30), using conventional It is fixed by construction methods (embedded in concrete, with the help of dowels or studs, etc.).

In a preferred embodiment of the invention, there is a support column located on the upper part of the mentioned carrier pole (20). The support structure (10) is the carrier pole (20) which provides the connection between the structure (10) and the carrier pole (20). The upper shaft (220), which enables it to rotate around the axis with which it is connected, is the upper shaft of the carrier pole (20). The upper shaft bearing (210), which provides the bearing of the said upper shaft (220), located in the The second support structure (10), located at the bottom of the pole (20), is the axis on which the carrier pole (20) is erected. inside the lower shaft (200) and the carrier pole (20), which enable it to rotate around the rotation axis (22). The post (230) that enables the connection of the said lower shaft (200) with the support structure (10). can be found. In this embodiment, the connection between the said support structure (10) and the upper shaft (220) is The connection elements (110) and the mentioned carrier structure (30) are the parts that enable the lower shaft (200) to be placed. may include lower shaft bearing (310). Additionally, in this embodiment, the said carrier pole (20) and the lower shaft (200) and/or between the said support structure (10) and the upper shaft bearing (210) There may also be a shock absorbing damping system that reduces the impact.

This solar tracking system (1), with a certain arrangement of the invention, is located on the second rotation axis of the carrier pole (20). When it is adjusted to move by rotating around (22), the carrier is attached to the pole (20). tracking system by adding a shock absorbing damping system to the upper shaft (200) that will provide rotational movement. (1) can be adjusted to absorb the cyclic loads on it.

In another embodiment of the invention, the shock absorbing damping system consists of a mobile or cyclic loads on the tracking system (1) by adding more than one element Can be adjusted to dampen.

This solar tracking system (1) rotates freely around the first rotation axis (21) mentioned above. the upper shaft bearing (210) on which the rotating upper shaft (200) will be placed, the first rotation axis (21) mentioned The shaft (220), which can rotate freely around it, produces a second rotation perpendicular to the first rotation axis. A carrier containing a pole (230) mounted on the lower shaft (200) so that it can rotate around its axis (22). Contains pole (20).

The said support structure (10) can rotate around the first rotation axis (21) and the carrying pole (20). carrier pole with connection elements (110) to be connected to an upper shaft (220) in order to be mounted on it It is mounted on (20) in a way that it can move. These connection elements (110) are attached to the support structure (10). According to the axes on which it rotates, its centers of gravity can be adjusted so that they coincide with the axes on which it rotates.

(Figure 2A) Said carrier pole (20) has a lower shaft that can rotate around the said second rotation axis (22). It is mounted on the carrier structure in a way that it can move with (220).

In such a way that the said support structure (10) can be mounted on the said carrier pole (20). It is mounted on the pole (230) with shaft bearings (210) on which it is supported by an adjusted upper shaft (220).

In the arrangement shown in the figure, the lower shaft (200) and the post (230) are placed in such a way that there is no movement between them. are mechanically connected. In another embodiment, the lower shaft (200) and the mast are formed in one piece. adjustable. (Figure 25) In a preferred embodiment of the invention, the part of the said carrier structure (30) that is connected to the ground is The carrier leg (300) and more than one carrier leg (300) are fixedly connected to each other. There may be a scissor system that provides

The mentioned carrier structure (30) consists of connections that will be used to fix this tracking system (1) to the ground. throughout the movement of the system with its load-bearing elements that will carry the loads on the system. keeps it stable. In one embodiment, said bearing structure consists of a bearing leg (300).

In another embodiment, a truss with a plurality of legs 300 fixedly adjusted to each other. may consist of the system. (Figure 2C) The shaft bearing where the said carrier pole (20) is connected to this carrier structure with the said lower shaft (200) The rotation axis (310) is the second rotation axis (22). (Figure 2C) The solar tracking system (1), which is the subject of the invention, is connected to the mentioned support structure (10) and the first rotating rotation movements around the axis (21) and the second rotation axis (22) simultaneously. It contains a guiding arm (40) that makes this possible.

This tracking system (1) includes the said support structure (10) and the operatively connected carrier pole (20). to rotate around the first and second rotation axes (21,22) mentioned in the same movement said first and said second rotation axes (21,22) mechanically in a sense. It contains a connecting guiding arm (40).

In the mentioned arrangement, the guiding arm (40) is connected to itself and the connection elements on it. It does not carry any weight other than its weight.

In a preferred embodiment of the invention, sunlight coming from different angles in summer and winter months is arm (400) that enables the length of said guiding arm (40) to be extended and/or shortened accordingly parts may be found.

This tracking system (1), with a certain arrangement of the invention, includes the main elements with mobility. It can rotate with the movement of anyone (support structure (10), carrier pole (20), guiding arm (40)).

The visuals in Figure 3 show how the guiding arm (40) and its sub-elements work and how they will work. shows the axes: The mentioned guiding arm (40), the carrier pole (20), the second rotation axis (22) In an arrangement where the carrier pole (200) is adjusted to move by rotating around itself. The support structure (10) that will follow the azimuth movement of the sun throughout its rotation, the altitude of the sun By rotating around the first rotation axis (21) sensitive to movement, this support structure (10) It directs the angle between it and the ground. The mentioned guiding arm (40) is shown in one piece in the image. has been shown. In a certain arrangement, it can be arranged in an adjustable height.

The images in Figure 4 show the length of the guiding arm (40) in two different configurations of the invention. shows the adjustment of the module at different angles according to its change: Simplifying the description of the invention For this tracking system (1), assuming that the system is installed in a field located in the northern hemisphere has been described systematically, but this tracking system makes a 180-degree turn to the southern hemisphere. It can also be used in the sphere.

Finally, the basic structure of the solar tracking system (1), thanks to the joint points they create, The first rotation axis located in the horizontal plane where the first rotation axis (21) of the support structure (10) is located. an axis other than axis (1) -preferably perpendicular to the first axis of rotation (21) and the second axis of rotation (22) - The said guiding arm (40), which enables it to rotate around, is attached to the support structure (10) from its upper end. the upper joint set (420) connecting it and the said guiding arm (40) from its lower end to the ground or carrier It contains the lower joint set (430) that connects it to the structure (30).

This guiding arm (40) operates on the supporting structure (10) of the guiding arm (40) with a certain arrangement. 3 rotary joints (421, 2 rotary joints whose rotation axes are set perpendicular to each other to enable the connection It can be set to include (431, 432).

In another embodiment, said rotation axes are adjusted to be perpendicular to each other. The number of joints can be set to 2 or 3 so that they are not the same as each other. For example, The rotation axes that will operatively connect the guiding arm (40) to the support structure (10) are perpendicular to each other. If 2 rotary joints adjusted to According to (30), the rotation axes will be perpendicular to each other to ensure a stable and operable connection. It can be adjusted to use 3 swivel joints adjusted accordingly.

While this guiding arm (40) is connected to the support structure (10) at the top with a certain arrangement, the support The first joint (421) to be connected to the structure (10) is placed from the ground-facing surface of the support structure (10) to the sun. having a first joint rotation axis (411) in the direction of the facing surface adjustable. In this arrangement, the first joint (421) connected to the support structure (10) is connected to the arm (400). The second joint (422), which will connect it to the third joint (423), will rotate on the first arm rotation axis (411). It is connected as follows. In this arrangement, the said joint (422) is perpendicular to the first joint rotation axis (411). A second joint is connected to the third joint (423) on the rotation axis (412), which will operatively connect it to the arm (400). connects. In this arrangement, the arm (400) is connected to the third joint (423) on the first joint's rotation axis. (411) and a third joint rotation axis that will be perpendicular to the second joint rotation axis (412). (413) is connected so that it can rotate and work.

While this guiding arm (400) is connected to the ground below with a certain arrangement, the arm (400) is connected to the guiding arm (400). The fourth joint (431) that will connect the arm (40) to the fifth joint (432) and the fourth The joint is connected operatively on the rotation axis (414).

The fifth joint (432) that will fix the guiding arm (40) to the ground and the fifth joint that will connect it to the arm (400) (431) operate on a fifth arm rotation axis (415) perpendicular to each other and the fourth arm rotation axis (414). It is connected as follows. In this arrangement, the third arm rotation axis (413) and the fourth arm rotation axis (414) are set to be parallel to each other. In another embodiment, the upper joint assembly 420 is rotated There may or may not be a correlation.

The fifth joint (432), which will fix the guiding arm (400) to the ground, is attached to the ground with a certain arrangement. It can also be fixed on the fixed carrier structure (30).

In another embodiment, currently available joint assemblies with three-dimensional movement capability It can also be connected with . For example, a ball joint can be connected to the lower and upper ends of the guiding arm (40).

In a preferred embodiment of the invention, the said upper joint set (420) and/or lower joint set (430) is the ball joint.

In a preferred embodiment of the invention, said upper joint set (420) The third joint (423), which enables the movement received from the arm (40) to be transferred, comes from the said third joint. (423) transfers the movement it receives to a second joint rotation axis (412) perpendicular to the third joint rotation axis (413). the second joint (422) that rotates and the movement it receives from the said second joint (422) to the support structure (10). to a first joint rotation axis (411) perpendicular to the second joint rotation axis (412) that ensures the transfer of If we include the first rotating joint (421), the said lower joint set (430) the fourth joint (431) which enables the transfer of the movement received from the arm (40) and the said fourth The movement it receives from the joint (431) is transferred to a fifth joint rotation perpendicular to the fourth joint rotation axis (414). It contains the fifth joint (432) that rotates it to the axis (415).

In another preferred embodiment of the invention, the said upper joint set (430) the fourth joint (431) that enables the transfer of the movement received from the guiding arm (40) and the mentioned It transfers the movement it receives from the fourth joint (431) to a fifth joint perpendicular to the fourth joint's rotation axis (414). While it contains the fifth joint (432) that turns the joint to the rotation axis (415), the said lower joint set (420), the third joint (423), which ensures the transfer of the movement received from the said guiding arm (40), It transfers the movement it receives from the said third joint (423) to a second joint perpendicular to the rotation axis (413) of the third joint. the second joint (422) that turns the joint to the rotation axis (412) and the The second joint, which enables the movement to be transferred to the support structure (10), is a first joint perpendicular to the rotation axis (412). It contains a first joint (421) that rotates the joint to the rotation axis (411).

In a preferred embodiment of the invention, said carrier structure (30) is fixed to the ground, said The carrier pole (20) is attached to the carrier structure (30) in a way that it rotates around the second rotation axis (22). The guiding arm (40) is placed on the ground with the lower joint set (430), the said guiding arm (40) is placed on the upper joint. The guiding arm (40) and the said support structure (10) will rotate around the first rotation axis (21). It is connected to the carrier pole (20) mentioned in the figure and has one degree of freedom. This In the embodiment, the carrier arm (40) is connected to the ground through the lower joint set (430). The direction to the structure (30) is north-south. Also, when not connected to a drive system When released, the center position is on said lower joint set of said guiding arm (40). The direction from both upper joint sets (420) mentioned with (430) to the carrier structure (30) is north- is in the south direction. The centers of gravity in this embodiment are on the first mentioned first section of the support structure (10). perpendicular to the rotation axis (21) and to the said first rotation axis (21) of said support structure (10). The upper joint set (420) of the said guiding arm (40) and the said support It is on the first rotation axis of the central axis of the weight distribution in the direction of its connection to the structure (30). (21). However, from the ground-facing surface of the support structure (10) to the sun-facing surface The central axis of the weight distribution in the direction of the first rotation axis (21) and the support structure (10) the second rotation of the central axis of the weight distribution in the direction of the first rotation axis It is on the axis. (22).

This tracking system (1), in one embodiment, is perpendicular to the first rotation axis (21) of the support structure (10) and from the point where the said support structure (10) is connected to the said first rotation axis (21). The said guiding arm (40) is connected to the said support structure (10) with the upper joint set (420). The center of the weight distribution in the direction is on the first rotation axis (21), with the support structure (10) facing the ground. The central axis of the weight distribution in the direction from the surface to the surface facing the sun is the first rotation axis (21), the center of the weight distribution in the direction of the first rotation axis of the support structure axis can be adjusted to be on the second rotation axis (22).

In one embodiment, the support structure (10) enables 3-axis rotation movement (vertical, east-west direction). horizontally and horizontally in the north-south direction) in each of the support structure (10) and the bearing pole (20). The center of gravity in all three directions is on the axis on which it rotates In a preferred embodiment of the invention, the said carrier structure (30) connects the carrier to the pole (20) and the floor, the said guiding arm (40), the lower joint set (430) and the upper joint set (420), the said upper joint set (420) and the support structure (10) and the said lower joint set (430) There are connection elements that enable the connection of the supporting structure (30) or the ground.

In a preferred embodiment of the invention, the said upper joint set (420) and the support structure (10) There is also a shock absorbing damping system that reduces the wind effect by being placed between can be found.

This solar tracking system (1) consists of a mechanical element that will drive the carrier pole (20). (not shown) with an electronic motor (not shown) to provide the torque to give rotational movement. An electronic component (e.g. driver not shown) that will control this motor must be installed properly. Can be controlled by programming.

This solar tracking system (1), with a certain arrangement of the invention, allows multiple tracking systems to be driven by a single drive. Can be adjusted to be moved.

The angles of inclination that the modules (5) should have will vary in different latitudes. adaptation to the length of the guiding arm (40) and/or the support structure (10) of this guiding arm distance of the connection point to the first rotation axis (21) and/or the distance of this guiding arm to the ground the distance of the connection point to the second rotation axis (22) and/or the length of the carrier pole (20). It is achieved by changing the . Thanks to the changes mentioned, the modules (5) have The maximum and minimum values of the inclination angles can be adjusted.

When the guiding arm (40) is fixed to the ground in the southward direction from the carrying structure (30), this tracking system will have the smallest slope angle in the south. In this arrangement, throughout the course of the day, From sunrise to noon the slope angle will decrease and from noon to sunset the slope angle will The angle will increase. In this arrangement, the slope angle will be greatest at sunrise and sunset.

When the guiding arm (40) is fixed to the ground in the northward direction from the carrying structure (30), this tracking system, It will have the largest slope angle in the south. In this arrangement, throughout the course of the day, From sunrise to noon, the slope angle will increase, and from noon to sunset, the slope angle will It will decrease. In this arrangement, the angle of inclination will be smallest at sunrise and sunset. a certain With regulation, this angle can be adjusted parallel to the ground.

The images in Figure 5 show the tilt according to the change in azimuth angles in two different configurations of the invention. It shows the change in angle: The largest and/or smallest azimuth that this tracking system (1) can reach angle and/or the largest and/or smallest inclination angles are determined by the length of the guiding arm (40) and/or this The distance of the point where the guiding arm is connected to the support structure (10) to the first rotation axis (21) and/or the distance of the point where this guiding arm is connected to the ground to the second rotation axis (22) and/or it is adjusted by changing the length of the carrier pole (20).

In regions with different wind conditions, the wind loads that will fall on the tracking system The guiding arm (40) moves northward from the carrier structure (30) so that its impact on the direction (Figure 5A) and/or the guiding arm (40) moves southwards from the carrier structure (30). direction (Figure SB) and/or these two configurations are used in common adjustable.

The images in Figure 6 show the movements of the invention in two different configurations during the day. As a result, when more than one tracking system (1) acts together in harmony, no The area in which they are located is positioned so that the tracking system is not shadowed by another shows its usage: The guiding arm (40) moves from the carrier structure (30) to the ground in a northward direction. When more than one tracking system (1) acts together in harmony, a certain In the arrangement, space usage can be adjusted to be minimum for this topological structure. (Figure 6A) When the guiding arm (40) is fixed to the ground in the southward direction from the carrying structure (30), more than one When the tracking system (1) acts together in harmony, the increase in efficiency in a certain arrangement is It can be adjusted to the maximum for the topological structure. (Figure GB) When both the guiding arm (40) is fixed to the ground in the northward direction from the carrying structure (30) and When the guiding arm (40) is fixed to the ground in the southward direction from the carrying structure (30), and/or these two When the configuration is used in common, space utilization and/or efficiency increases are optimized in a particular arrangement. can be done.

In regions with different wind conditions, the wind loads that will fall on the tracking system (1) The guiding arm (40) moves northward from the carrier structure (30) so that its impact on the direction is fixed to the ground and/or the guiding arm (40) moves southward from the carrier structure (30). It can be set to be fixed to the floor and/or these two configurations can be used jointly.

The systems that will act together in harmony with more than one tracking system (1) are different from each other. having different largest and/or smallest azimuths and/or largest and/or smallest inclination angles They may be.

The visuals in Figure 7 show that this tracking system (1) is used in situations where the area where it will be installed is rugged. Indicates suitability for installation: This tracking system (1) has a certain shape on which it stands on one leg. In this arrangement, the system will have the ability to be installed independently of the topography of the land.

In cases where the field is rough, the invention can be used in multiple different configurations depending on the topography. and when arranged in dimensions and moving together in harmony, a tracking system (1) is formed, thus The maximum efficiency increase for this topological structure will not be overshadowed by the other and/or appropriate for the purpose. and/or space usage in a way that is minimal for this topological structure and efficiency increase can be optimized for the purpose when used together.

Claims (8)

1. It is a solar tracking system (1) that allows at least one solar module (5) that collects the sun's rays to be positioned according to the course of the sun during the day, and its feature is; At least one support structure (10), which enables the said solar module (5) to be mounted, supports the support structure (10) around the first rotation axis (21), which carries the said support structure (10) and is the axis with which the support structure (10) is connected. ) at least one carrier pole (20) that allows it to rotate freely, connecting said carrier pole (20) to the ground, allowing the carrier pole (20) to rotate freely around a second axis of rotation (22) - preferably perpendicular to the ground and the first axis of rotation (22). - at least one guiding arm (40) that enables the rotation movements around the first rotation axis (21) and the second rotation axis (22) to be carried out simultaneously by connecting to the said support structure (10), o Thanks to the joint points they form, they enable the support structure (10) to rotate around an axis other than the first rotation axis (21) in the horizontal plane where the first rotation axis (21) is located - preferably perpendicular to the first rotation axis (21) and the second rotation axis (22). , at least one upper joint set (420) connecting said guiding arm (40) to the support structure (10) from its upper end, and at least one lower joint set (430) connecting said guiding arm (40) to the ground or carrier structure (30) from its lower end. , it contains. 2. It is a solar tracking system (1) in accordance with claim 1, and its feature is; The said upper joint set (420) and/or lower joint set (430) is a spherical joint. 3. It is a solar tracking system (1) in accordance with claim 1, and its feature is; o at least one third joint (423) that ensures the transfer of the movement received by the said upper joint set (420) from the said guiding arm (40), o transfers the movement received from the said third joint (423) to a second joint rotation perpendicular to the third joint rotation axis (413). at least one second joint (422) that turns it to the axis (412), and at least one that turns it to a first joint rotation axis (411) perpendicular to the second joint rotation axis (412), which ensures that the movement received from that second joint (422) is transferred to the support structure (10). The first joint (421) includes the said lower joint set (430). At least one fourth joint (431), which enables the transfer of the movement received from the said guiding arm (40), and at least one fifth joint (431), which converts the movement received from the said fourth joint (431) into a fifth joint rotation axis (415) perpendicular to the fourth joint rotation axis (414). 432), 4. It is a solar tracking system (1) in accordance with claim 1, and its feature is; o at least one fourth joint (431), which enables the transfer of the movement received by the said upper joint set (430) from the said guiding arm (40), and transfers the movement received from the said fourth joint (431) to a fifth joint rotation axis perpendicular to the fourth joint rotation axis (414). The said lower joint set (420) includes at least one fifth joint (432) that rotates (415). At least one third joint (423) that ensures the transfer of the movement received from the said guiding arm (40), and at least one second joint (423) that converts the movement received from the said third joint (423) into a second joint rotation axis (412) perpendicular to the third joint rotation axis (413). 422), at least one first joint (421), which converts the movement received from the said second joint (422) into a first joint rotation axis (411) perpendicular to the second joint rotation axis (412), which ensures its transfer to the support structure (10), 5. It is a tracking system (1) in accordance with claim 1, and its feature is; - the said bearing structure (30) fixedly to the ground, that said bearing pole (20) to the bearing structure (30) rotating around the second rotation axis (22), that said guiding arm (40) to the ground with the lower joint set (430), - the said guiding arm (40) connects the upper joint set (420) to the support structure (10), - the said support structure (10) connects the upper joint set (420) to the guiding arm (40), that and the said support structure (10), It has a degree of freedom connected to the said carrier pole (20) in such a way that it rotates around the first rotation axis (21). 6. It is a solar tracking system (1) in accordance with any of the above claims, and its feature is; The said support structure (10) contains at least one construction (100) on which the said solar modules (5) are placed, and at least one termination (120) that enables the connection of the said solar modules (5) to the construction (10). 7. It is a solar tracking system (1) in accordance with any of the above claims and its feature is; o the said bearing structure (30) and the carrier pole (20) and the ground, o the said guiding arm (40) and the lower joint set (430) and the upper joint set (420), 1› the said upper joint set (420) and the support structure (10) contains connection elements that enable the connection of the said lower joint set (430) with the carrier structure (30) or the ground. 8. It is a solar tracking system (1) in accordance with any of the above claims and its feature is; The said carrier pole (20) has at least one column on the upper part of that carrier pole (20), which enables the connection of the support structure (10) with the carrier pole (20) and enables the support structure (10) to rotate around the axis where it is connected to the carrier pole (20). an upper shaft (220), at least one upper shaft bearing (210) located on the upper part of the 1st carrier pole (20), providing the bearing of said upper shaft (220), and supporting structure (10) located on the lower part of that carrier pole (20). ), at least one lower shaft (200) that enables the carrier pole (20) to rotate around the second rotation axis (22), which is the axis on which it is erected, and the said lower shaft (200) located inside that carrier pole (20) is connected to the support structure (10). It contains at least one pole (230) that provides It is a solar tracking system (1) in accordance with any of the above claims and its feature is; It contains at least one arm (400) component that allows the length of the said guiding arm (40) to be extended and/or shortened according to the sunlight coming at different angles in summer and winter months. It is a solar tracking system (1) in accordance with any of the above claims and its feature is; It contains at least one drive transmission mechanism that provides the transmission of the drive that will give the rotational movement to the carrier pole (20). It is a solar tracking system (1) in accordance with any of the above claims and its feature is; It contains at least one drive transmission mechanism that provides the transmission of the drive that will give the rotational movement to the guiding arm (40). It is a solar tracking system (1) in accordance with any of the above claims and its feature is; The said bearing structure (30) contains at least one bearing leg (300), which is the part that is connected to the ground. It is a solar tracking system (1) in accordance with any of the above claims and its feature is; It contains at least one shock absorbing damping system that reduces the wind effect by placing it between the said upper joint set (420) and the support structure (10). It is a tracking system (1) in accordance with claim 5, and its feature is; The direction of the said guiding arm (40) from the lower joint set (430) to the carrier structure (30) to which it is connected to the ground is in the north-south direction. It is a solar tracking system (1) in accordance with Claim 8, and its feature is; It contains connection elements (110) that enable the connection of the said support structure (10) and the upper shaft (220). It is a solar tracking system (1) in accordance with claim 8, and its feature is; The said carrier structure (30) contains at least one lower shaft bearing (310) that allows the lower shaft (200) to be placed. It is a solar tracking system (1) in accordance with Claim 8, and its feature is; It contains at least one shock absorbing damping system that reduces the wind effect by placing it between the said carrier pole (20) and the lower shaft (200) and/or, o between the said support structure (10) and the upper shaft bearing (210). . It is a solar tracking system (1) in accordance with claim 10, and its feature is; It contains at least one shock absorbing damping system that reduces the wind effect on the said drive transmission mechanism. It is a solar tracking system (1) in accordance with Claim 10 or Claim 11, and its feature is; It contains at least one drive mechanism connected to the drivers in order to control multiple solar tracking systems (1) simultaneously from a single center. It is a solar tracking system (1) in accordance with claim 12, and its feature is; It contains at least one scissor system that allows multiple carrier legs (300) to be connected to each other in a stable manner. It is a tracking system (1) in accordance with claim 14, and its feature is; When it is released while not connected to a drive system, the center position of the said guiding arm (40) is that the direction from both the said lower joint set (430) and the said upper joint set (420) to the carrier structure (30) is in the north-south direction. It is a tracking system (1) in accordance with claim 14, and its feature is; perpendicular to the said first rotation axis (21) of the support structure (10) and in the direction where the said guiding arm (40) is connected to the said support structure (30) with the upper joint set (420) from the point where the said support structure (10) is connected to the said first rotation axis (21). The central axis of the weight distribution is on the first rotation axis (21). It is a tracking system (1) in accordance with claim 14, and its feature is; The central axis of the weight distribution in the direction from the ground-facing surface of the support structure (10) to the sun-facing surface is in the first rotation axis (21). It is a tracking system in accordance with claim 14, and its feature is; The central axis of the weight distribution of the support structure (10) in the direction of the first rotation axis is in the second rotation axis (22).