WO2012091475A2 - Solar tracking apparatus - Google Patents

Solar tracking apparatus Download PDF

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Publication number
WO2012091475A2
WO2012091475A2 PCT/KR2011/010275 KR2011010275W WO2012091475A2 WO 2012091475 A2 WO2012091475 A2 WO 2012091475A2 KR 2011010275 W KR2011010275 W KR 2011010275W WO 2012091475 A2 WO2012091475 A2 WO 2012091475A2
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WO
WIPO (PCT)
Prior art keywords
frame
solar cell
cell unit
solar
central axis
Prior art date
Application number
PCT/KR2011/010275
Other languages
French (fr)
Korean (ko)
Other versions
WO2012091475A3 (en
Inventor
민광식
Original Assignee
Min Kwang Sik
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Min Kwang Sik filed Critical Min Kwang Sik
Priority to CN201180063135.7A priority Critical patent/CN103283035B/en
Publication of WO2012091475A2 publication Critical patent/WO2012091475A2/en
Publication of WO2012091475A3 publication Critical patent/WO2012091475A3/en

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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00Supporting structures for PV modules
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S25/00Arrangement of stationary mountings or supports for solar heat collector modules
    • F24S25/10Arrangement of stationary mountings or supports for solar heat collector modules extending in directions away from a supporting surface
    • F24S25/12Arrangement of stationary mountings or supports for solar heat collector modules extending in directions away from a supporting surface using posts in combination with upper profiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S30/00Arrangements for moving or orienting solar heat collector modules
    • F24S30/40Arrangements for moving or orienting solar heat collector modules for rotary movement
    • F24S30/45Arrangements for moving or orienting solar heat collector modules for rotary movement with two rotation axes
    • F24S30/458Arrangements for moving or orienting solar heat collector modules for rotary movement with two rotation axes with inclined primary axis
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00Supporting structures for PV modules
    • H02S20/30Supporting structures being movable or adjustable, e.g. for angle adjustment
    • H02S20/32Supporting structures being movable or adjustable, e.g. for angle adjustment specially adapted for solar tracking
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S30/00Arrangements for moving or orienting solar heat collector modules
    • F24S2030/10Special components
    • F24S2030/13Transmissions
    • F24S2030/134Transmissions in the form of gearings or rack-and-pinion transmissions
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/47Mountings or tracking
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy

Definitions

  • the present invention relates to a solar tracking device, and more particularly, to a solar tracking device having a simple structure and reducing power for rotation of a solar cell unit.
  • photovoltaic power generation is a technology for converting sunlight into electrical energy, and is a power generation method using a solar cell that generates photovoltaic power by photoelectric effect when light is irradiated.
  • the general configuration of the system consists of a module consisting of solar cells, a battery and a power converter. Examples of solar cells include selenium photovoltaic cells using copper and metal sulfide photovoltaic cells, silicon photovoltaic cells using semiconductor pn junctions, and the like.
  • Such photovoltaic power generation has a merit of self-powered generation to obtain unlimited clean energy, easy maintenance and repair, and unmanned operation.
  • production efficiency is lower than that of fossil fuels such as coal and petroleum, and it is pointed out as a problem that power generation fluctuations are severe depending on solar radiation.
  • tracking devices for moving solar panels in response to changes in the orbit of the sun have been developed.
  • the present invention has been made in view of the above-described problems, and provides a solar tracking device that can accurately track sunlight with less power and simple control by applying a solar tracking device with a simplified structure. There is this.
  • the gravity tracking indicator provides a solar tracking device that can accurately track the altitude of the sun through the relative tilt of the gravity indicator and the tracking device even if the center axis of the solar tracking device is not exactly level with the ground. have.
  • the solar tracking device of the present invention comprises: a first frame for supporting a solar cell unit for condensing sunlight to convert energy; A second frame hinged to rotate the first frame in a east-west direction; A central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, the central axis being hinged to rotate in the north-south direction; First rotation limiting means provided on the second frame and the central axis to limit a north-south rotation radius of the first frame; Second rotation limiting means provided in the first frame and the second frame to limit the east-west rotation radius of the first frame; And a central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, and the solar cell unit is hinged to rotate in the north-south direction. Characterized in that it comprises a.
  • the second frame a gravity direction indicator for displaying the direction of gravity; characterized in that it is further provided.
  • the gravity direction indicator may include a connecting portion formed at a hinge coupling portion between the second frame and the central axis, a rod connected at one end to the connecting portion, and a weight connected to the other end of the rod. It is done.
  • the first rotation limiting means is driven in engagement with the first worm gear and the first gear wheel
  • the second rotation limiting means is driven in engagement with the second worm gear and the second gear wheel.
  • the first gear wheel may be provided in the second frame along a trajectory of the solar cell unit rotating in the north-south direction, and the first worm gear may be rotated by a first motor provided in the central axis. It is characterized by being formed.
  • the second gear wheel may be provided in the first frame along a trajectory of the solar cell unit rotating in the east-west direction, and the second worm gear may be rotated by a second motor provided in the second frame. It is characterized in that it is formed to.
  • a point at which the other end of the central axis and the second frame are coupled is a center of gravity of the solar cell unit and the first frame.
  • the rotating unit for rotating the solar cell unit and a screw jack for supporting the solar cell unit and extending and contracting are not provided separately, and rotate in the east-west direction and the north-south direction by using the center of gravity of the solar cell unit. Therefore, the power to operate the equipment is reduced, and there is an advantage that is easier to control than when driving a complex structure at the same time.
  • since only the rotation angle of the rotating part needs to be controlled there is an advantage in that sunlight can be tracked more precisely than when each screw jack and the rotation angle must be controlled at the same time.
  • FIG. 1 is a perspective view of the solar tracking device of the present invention
  • FIG. 2 is a side view of the solar tracking device of the present invention
  • FIG. 3 is a perspective view of a second frame of the solar tracking device of the present invention
  • FIG. 4 is a side view of a second frame in which the gravity direction indicator of the solar tracking device of the present invention is installed;
  • FIG. 5 is a perspective view of a first frame of the solar tracking device of the present invention
  • Figure 6 is a side view of the first frame of the solar tracking device of the present invention
  • the solar tracking device includes a method of measuring and tracking sunlight with a sensor, a method of rotating according to a predetermined time according to a program, and a method of being manually driven by a user.
  • the rotation method driven to follow the solar light may be divided into a short axis type that rotates in the east-west direction and performs only a round motion, and a biaxial type that simultaneously performs the round motion and playing motion while rotating in the east-west direction and the north-south direction.
  • the solar tracking device 100 of the present invention includes a fixed frame S, a first frame 110, a central axis 120, a second frame 130, and a first rotation limiting means. 140, the second rotation limiting means 150, and the gravity direction indicator 160.
  • a solar cell unit (not shown) is a device that condenses sunlight and converts solar energy into other energy, and it is common to convert solar energy into electrical energy. Therefore, the solar cell unit may be provided with a solar panel for condensing sunlight, a conversion device for converting energy, and an energy storage device for storing the energy, which are the same as in the general case, and thus a detailed description thereof will be omitted.
  • Solar cells convert the energy of sunlight into electrical energy and generate electricity using two types of semiconductors, P-type semiconductors and N-type semiconductors. When light shines on the solar cell, electrons and holes are generated inside. The generated charges move to the P and N poles, and a potential difference (photovoltaic power) is generated between the P pole and the N pole by this phenomenon.
  • Solar cells can be roughly divided into those using a silicon semiconductor as a material and a compound semiconductor as a material.
  • the silicon semiconductor may be classified into a crystal system and an amorphous system (AMOLFASS).
  • the fixed frame (S) is a configuration for fixing the solar cell unit to the solar tracking device of the present invention can be applied to a conventional frame.
  • the fixed frame (S) is a plurality of spaced apart a predetermined distance on the beam.
  • the first frame 110 is a means for supporting the fixed frame (S), the first horizontal frame 111, the first vertical frame 112, the first rotating shaft 113, the first reinforcing rod 114 and And a second gear wheel 153.
  • a plurality of the first horizontal frame 111 is formed spaced apart a predetermined distance on the beam.
  • a plurality of first vertical frames 112 are formed on the beam spaced apart from each other by a predetermined distance, and are coupled to be orthogonal to the first horizontal frames 111.
  • a first rotating shaft 113 is formed at the center of the lower surface of the first vertical frame 112, and both ends of the first rotating shaft 113 are connected to the first rotating shaft 113, and the other end thereof is the first vertical axis.
  • the first reinforcement 114 is connected to the frame 112 is installed.
  • the first rotation shaft 113 and the first reinforcing rod 114 may be formed in each of the first vertical frames 112.
  • the second gear wheel 153 is installed on any one of the first vertical frame 112, a detailed description thereof will be described later in the second rotation limit means (150).
  • the central axis 120 is an axis for supporting the solar tracking device 100 and is extended upward with one end fixed to the bottom surface.
  • the other end of the central axis 120 is coupled to the second frame 130, it is preferable that the hinge coupled to rotate the solar cell unit in the north-south direction.
  • the coupling position of the central axis 120 and the second frame 130 is preferably coupled at the center of gravity of the fixed frame (S) to which the solar cell unit is fixed and the first frame (110).
  • the solar tracking device 100 according to the present invention is provided with only a driving device for rotating the solar cell unit, and there is no auxiliary equipment such as a screw jack.
  • the solar cell unit, the fixed frame (S), the first frame 110 and the second frame 130 are all the central axis 120 that is the coupling point of the second frame 130 and the central axis 120. Is supported by the other end of the
  • the solar cell unit may be at an angle. Even if it rotates, structural stability can be maintained. Since the central axis 120 corresponds to the proximal end supporting the solar tracking device 100, the central axis 120 may be formed of a material having sufficient rigidity.
  • the second frame 130 is coupled to the central axis 120 and includes a first rotation limiting unit 140 and a second rotation limiting unit 150 of the solar cell unit.
  • the radius of rotation can be limited.
  • the inclined frame 133 connecting one end, the lower frame 134 connecting the other end of the rotating frame 135 and the other end of the first gear wheel 143, the rotating frame 135 and the inclined frame 133
  • the vertical frame 131 has a dual structure of the first vertical frame 132a and the second vertical frame 132b, and is fixed to each of the first, second and third parallel frames 132c, 132d, and 132e.
  • the vertical frame 132 is configured in a double structure to ensure the structural strength of the second frame 130.
  • the rotation frame 135 is a second rotation shaft 135a for hinge coupling with the hinge coupling portion 121 formed at one end of the central shaft 120, the main rotation frame hinged to the first rotation shaft 113 135b, an auxiliary rotating frame 135c for reinforcing the structural strength of the rotating frame 135, a second reinforcing frame 135d, and a truss frame 135e.
  • the first rotation limiting unit 140 may be provided in various structures in a range of limiting the radius of rotation of the solar cell unit in the north-south direction. Since the first rotation limiting unit 140 is related to the playing movement of the sun in which the altitude of the sun varies depending on the season, it is preferable to limit the rotation angle to rotate within 60 degrees in consideration of the earth's axis tilt angle. 2 illustrates a case in which the first rotation limiting unit 140 is formed in a worm gear type in which the first worm gear 141 is driven in engagement with the first gear wheel 143 through the first connection gear 142. Is shown.
  • the first gear wheel 142 may be formed in the circumferential direction of the second frame 130 along the rotational trajectory of the solar cell unit rotating in the north-south direction.
  • the acute angle is within 60 degrees by using the coupling point of the central axis 120 and the solar cell unit as the rotation center.
  • the first gear wheel 142 may be formed to be.
  • the first worm gear 141 is preferably formed to rotate by using the first motor (M1) provided in the central shaft 120 as a power.
  • the rotation angle of the worm can be controlled in a precise manner so that the rotation angle can be precisely controlled to accurately follow sunlight.
  • the worm gear system is stable because no reversal phenomenon occurs.
  • the second rotation limiting means 150 may be provided in various structures in a range of limiting the radius of rotation of the solar cell unit in the east-west direction. In the case of the second rotation limiting means 150, only the difference from the first rotation limiting means 140 will be described.
  • the second rotation limiting means 150 limits the east-west rotation radius of the solar cell unit, whereas the first rotation limiting means 140 limits the north-south rotation of the solar cell unit. Therefore, since the second rotation limiting means 150 is related to the circumferential motion of the sun moving from east to west according to the rotation of the earth, the rotation angle is limited to rotate within about 170 degrees in consideration of the east and west horizons. It is preferable.
  • the second rotation limiting means 150 is formed in a worm gear type similarly to the first rotation limiting means 140.
  • the second gear wheel 153 is arranged along the rotation trajectory of the solar cell unit rotating in the east-west direction.
  • the second rotation limiting means 150 is formed in a worm gear type in which the second worm gear 151 is driven in engagement with the second gear wheel 153 through the second connecting gear 152.
  • the sun tracking device of the present invention has the following configuration to accurately track the altitude of the sun irrespective of the inclination of the central axis 120 and the ground.
  • the gravitational direction indicator 160 is installed on the second frame 130 and displays a location on the second gear wheel 143 that is perpendicular to the gravitational direction, that is, the indicator.
  • the gravity direction indicator 160 is composed of a connecting portion 161, rod 162 and weight 163.
  • the connection part 161 is formed on the second rotation axis 135a on the second frame 130.
  • One end of the rod 162 is connected to the connecting portion 161, and any configuration may be applied as long as the connecting portion 161 and the weight 163 can be connected in a straight line.
  • the weight 163 is connected to the other end of the rod 162, a conventional weight configuration can be applied.
  • the gravity direction indicator is displayed on the second gear wheel 143 by measuring the point perpendicular to the ground through the gravity direction indicator 160. It is possible to accurately track the altitude of the sun through the relative inclination between the 160 and the second gear wheel 143.

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Abstract

The present invention relates to a solar tracking apparatus, and more particularly, to a solar tracking apparatus which can save power when rotating a solar cell unit and which has a simple structure. In detail, the solar tracking apparatus according to one embodiment of the present invention comprises: a solar cell unit that collects solar light and coverts the solar light into energy; a center shaft, one end of which is fixed onto a floor and extends upwardly, and the other end of which is coupled to the solar cell unit, wherein the center shaft is hinged onto the solar cell unit such that the solar cell unit rotates in the north and south directions; and a frame which is coupled to the center shaft, and which includes first rotation-limiting means for limiting the radius of rotation of the solar cell unit in the north and south directions, and second rotation-limiting means for limiting the radius of rotation of the solar cell unit in the east and west directions.

Description

태양광 추적 장치Solar tracking device
본 발명은 태양광 추적 장치에 관한 것으로, 특히 태양 전지 유닛의 회전을 위한 동력을 절감하고 단순한 구조를 갖는 태양광 추적 장치에 관한 것이다.TECHNICAL FIELD The present invention relates to a solar tracking device, and more particularly, to a solar tracking device having a simple structure and reducing power for rotation of a solar cell unit.
일반적으로 태양광 발전은 태양광을 전기 에너지로 변환하는 기술로, 빛이 조사(照射)되면 광전 효과에 의해 광기전력이 발생되도록 하는 태양 전지(solar cell)를 이용한 발전 방식이다. 그 시스템의 일반적인 구성은 태양 전지로 구성된 모듈과 축전지 및 전력 변환장치로 구성된다. 또한, 태양 전지의 종류로는 금속과 반도체의 접촉을 이용한 셀렌 광전지 및 아황산구리 광전지, 반도체 pn접합을 사용한 실리콘 광전지 등이 있다.In general, photovoltaic power generation is a technology for converting sunlight into electrical energy, and is a power generation method using a solar cell that generates photovoltaic power by photoelectric effect when light is irradiated. The general configuration of the system consists of a module consisting of solar cells, a battery and a power converter. Examples of solar cells include selenium photovoltaic cells using copper and metal sulfide photovoltaic cells, silicon photovoltaic cells using semiconductor pn junctions, and the like.
이러한 태양광 발전은 청정에너지를 무제한으로 얻을 수 있는 자가 발전 방식이고, 유지 및 보수가 용이하며 무인화가 가능하다는 장점을 갖고 있다. 그러나 석탄 및 석유와 같은 화석 연료를 이용한 화력 발전보다 생산 효율이 낮으며, 일사량에 따라 전력 생산량의 발전 편차가 심한 점이 문제점으로 지적되고 있다. 이를 해결하기 위해 태양의 궤도 변화에 따라 태양 전지판이 움직이는 추적 장치가 개발되어 왔다.Such photovoltaic power generation has a merit of self-powered generation to obtain unlimited clean energy, easy maintenance and repair, and unmanned operation. However, production efficiency is lower than that of fossil fuels such as coal and petroleum, and it is pointed out as a problem that power generation fluctuations are severe depending on solar radiation. In order to solve this problem, tracking devices for moving solar panels in response to changes in the orbit of the sun have been developed.
종래의 태양광 추적 장치의 경우 회전부와 태양 전지판을 연결하는 스크루 잭이 구비되어, 이들 구조물이 총체적으로 유동하며 태양광을 추적하게 된다. 따라서 구조가 복잡하고 회전하는 중심축과 각각의 스크루 잭을 모두 동시에 움직여야 하므로 많은 동력을 요하게 된다. 뿐만 아니라, 태양광을 추적하기 위해 회전하는 중심축의 회전각과 각각의 스크루 잭의 인장 및 수축 정도가 동시에 제어되어야 하므로, 제어가 어렵고 정밀한 추적이 어려운 문제점이 있다.Conventional solar tracking device is provided with a screw jack for connecting the rotating unit and the solar panel, these structures flow in total and track the sunlight. Therefore, the structure is complicated and requires a lot of power because the rotating central axis and each screw jack must be moved simultaneously. In addition, since the rotation angle of the rotating central axis and the tension and shrinkage of each screw jack must be simultaneously controlled in order to track sunlight, it is difficult to control and precise tracking is difficult.
또한 사계절의 태양 고도 데이터에 따라 태양광 추적 장치의 기울기를 정확하게 세팅 한다 할지라도 태양광 추적 장치 중심축 기울기에 따른 오차가 발생해 태양의 정확한 추적이 어려운 문제점이 추가로 발생한다.In addition, even if the slope of the solar tracking device is accurately set according to the solar altitude data of the four seasons, an error occurs due to the tilt of the central axis of the solar tracking device, which makes it difficult to accurately track the sun.
따라서 태양광을 추적하는 추적 장치의 구조를 단순화하여 적은 동력과 간단한 제어만으로도 태양광을 정확하게 추적할 수 있는 태양광 추적 장치의 개발이 요구된다.Therefore, there is a need for the development of a solar tracking device that can accurately track sunlight with little power and simple control by simplifying the structure of the tracking device that tracks sunlight.
본 발명은 상술한 바와 같은 문제점을 감안하여 안출된 것으로, 구조가 단순화된 태양광 추적 장치를 적용하여 보다 적은 동력과 간단한 제어만으로도 태양광을 정확하게 추적할 수 있는 태양광 추적 장치를 제공하는데 그 목적이 있다.SUMMARY OF THE INVENTION The present invention has been made in view of the above-described problems, and provides a solar tracking device that can accurately track sunlight with less power and simple control by applying a solar tracking device with a simplified structure. There is this.
또한, 중력방향 표시기를 통해 태양광 추적 장치의 중심축이 지면과 정확하게 수평을 유지하지 않아도 중력방향 표시기와 추적 장치의 상대 기울기를 통해 태양의 고도를 정확하게 추적할 수 있는 태양광 추적 장치를 제공함에 있다.In addition, the gravity tracking indicator provides a solar tracking device that can accurately track the altitude of the sun through the relative tilt of the gravity indicator and the tracking device even if the center axis of the solar tracking device is not exactly level with the ground. have.
본 발명의 태양광 추적 장치는 태양광을 집광하여 에너지를 변환하는 태양 전지 유닛을 지지하는 제1 프레임; 상기 제1 프레임이 동서 방향으로 회전하도록 힌지 결합되는 제2 프레임; 일단이 바닥면에 고정된 채 상방으로 연장되고 타단이 제2 프레임과 결합되되, 상기 태양 전지 유닛이 남북 방향으로 회전하도록 힌지 결합되는 중심축; 상기 제2 프레임 및 중심축에 구비되며, 상기 제1 프레임의 남북 방향 회전 반경을 제한하는 제1 회전 제한수단; 상기 제1 프레임 및 제2 프레임에 구비되며, 상기 제1 프레임의 동서 방향 회전 반경을 제한하는 제2 회전 제한수단; 및 일단이 바닥면에 고정된 채 상방으로 연장되고 타단이 제2 프레임과 결합되되, 상기 태양 전지 유닛이 남북 방향으로 회전하도록 힌지 결합되는 중심축; 을 포함하는 것을 특징으로 한다.The solar tracking device of the present invention comprises: a first frame for supporting a solar cell unit for condensing sunlight to convert energy; A second frame hinged to rotate the first frame in a east-west direction; A central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, the central axis being hinged to rotate in the north-south direction; First rotation limiting means provided on the second frame and the central axis to limit a north-south rotation radius of the first frame; Second rotation limiting means provided in the first frame and the second frame to limit the east-west rotation radius of the first frame; And a central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, and the solar cell unit is hinged to rotate in the north-south direction. Characterized in that it comprises a.
이때, 상기 제2 프레임에는, 중력방향을 표시하기 위한 중력방향 표시기;가 더 구비되는 것을 특징으로 한다.At this time, the second frame, a gravity direction indicator for displaying the direction of gravity; characterized in that it is further provided.
또한, 상기 중력방향 표시기는, 상기 제2 프레임과 중심축과의 힌지결합부에 형성되는 연결부와, 일단이 상기 연결부에 연결되는 로드와, 상기 로드의 타단에 연결되는 무게추로 구성되는 것을 특징으로 한다.The gravity direction indicator may include a connecting portion formed at a hinge coupling portion between the second frame and the central axis, a rod connected at one end to the connecting portion, and a weight connected to the other end of the rod. It is done.
여기서, 상기 제1 회전 제한수단은 제1 웜기어와 제1 기어휠이 맞물려 구동되며, 상기 제2 회전 제한수단은 제2 웜 기어와 제2 기어 휠이 맞물려 구동되는 것을 특징으로 한다.Here, the first rotation limiting means is driven in engagement with the first worm gear and the first gear wheel, the second rotation limiting means is driven in engagement with the second worm gear and the second gear wheel.
또한, 상기 제1 기어 휠은 남북 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 궤적을 따라 상기 제 2프레임에 구비되고, 상기 제1 웜 기어는 상기 중심축에 구비되는 제1 모터에 의해 회전하도록 형성되는 것을 특징으로 한다.The first gear wheel may be provided in the second frame along a trajectory of the solar cell unit rotating in the north-south direction, and the first worm gear may be rotated by a first motor provided in the central axis. It is characterized by being formed.
또한, 상기 제2 기어 휠은 동서 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 궤적을 따라 상기 제1 프레임에 구비되고, 상기 제2 웜 기어는 상기 제2 프레임에 구비되는 제2 모터에 의해 회전하도록 형성되는 것을 특징으로 한다.The second gear wheel may be provided in the first frame along a trajectory of the solar cell unit rotating in the east-west direction, and the second worm gear may be rotated by a second motor provided in the second frame. It is characterized in that it is formed to.
아울러, 상기 중심축의 타단과 상기 제2 프레임이 결합되는 지점은 상기 태양 전지 유닛 및 상기 제1 프레임의 무게 중심점인 것을 특징으로 한다.In addition, a point at which the other end of the central axis and the second frame are coupled is a center of gravity of the solar cell unit and the first frame.
본 발명의 일실시예에 따른 태양광 추적 장치는,Solar tracking device according to an embodiment of the present invention,
첫째, 태양 전지 유닛을 회전시키는 회전부와 태양 전지 유닛을 지지하며 인장 및 수축되는 스크루 잭이 별도로 구비되지 않고, 태양 전지 유닛의 무게 중심을 이용하여 동서 방향과 남북 방향으로 회전시키므로 단순한 구조를 갖는다. 따라서 장비를 운용하는 동력이 절감되며 복잡한 구조를 동시에 구동하는 경우보다 제어가 쉬운 장점이 있다. 또한 회전부의 회전각만을 제어하면 되므로, 각각의 스크루 잭과 회전각을 모두 동시에 제어해야 되는 경우에 비해 보다 정밀하게 태양광을 추적할 수 있는 장점이 있다.First, the rotating unit for rotating the solar cell unit and a screw jack for supporting the solar cell unit and extending and contracting are not provided separately, and rotate in the east-west direction and the north-south direction by using the center of gravity of the solar cell unit. Therefore, the power to operate the equipment is reduced, and there is an advantage that is easier to control than when driving a complex structure at the same time. In addition, since only the rotation angle of the rotating part needs to be controlled, there is an advantage in that sunlight can be tracked more precisely than when each screw jack and the rotation angle must be controlled at the same time.
둘째, 태양 전지 유닛을 동서 방향 및 남북 방향으로 회전 시키는 제 1, 제 2 회전 제한수단을 웜 기어 방식에 의하는 경우, 웜의 회전수를 조절함에 따라 정밀한 제어가 가능하고 역전 현상이 발생하지 않는다. 따라서 태양광 추적 장치가 설치되는 현장의 기상 조건에 영향이 적으며 안정적으로 정밀한 태양광 추적이 가능하다.Second, when the first and second rotation limiting means for rotating the solar cell unit in the east-west direction and the north-south direction by the worm gear system, precise control is possible and the reversal phenomenon does not occur by adjusting the rotation speed of the worm. . Therefore, it is possible to reliably and precisely track solar light with little influence on weather conditions at the site where the solar tracking device is installed.
셋째, 태양광 추적 장치의 중심축이 지면과 직교하지 않아도 중력방향 표시기를 통해 상대 기울기를 적용하여 태양의 고도를 정확하게 추적할 수 있게 되는 효과가 있다.Third, even if the central axis of the solar tracking device is not orthogonal to the ground, it is possible to accurately track the altitude of the sun by applying a relative slope through the gravity direction indicator.
도 1은 본 발명의 태양광 추적 장치 사시도1 is a perspective view of the solar tracking device of the present invention
도 2는 본 발명의 태양광 추적 장치 측면도Figure 2 is a side view of the solar tracking device of the present invention
도 3은 본 발명의 태양광 추적 장치의 제2 프레임 사시도3 is a perspective view of a second frame of the solar tracking device of the present invention
도 4는 본 발명의 태양광 추적 장치의 중력방향 표시기가 설치된 제2 프레임 측면도4 is a side view of a second frame in which the gravity direction indicator of the solar tracking device of the present invention is installed;
도 5는 본 발명의 태양광 추적 장치의 제1 프레임 사시도5 is a perspective view of a first frame of the solar tracking device of the present invention
도 6은 본 발명의 태양광 추적 장치의 제1 프레임 측면도Figure 6 is a side view of the first frame of the solar tracking device of the present invention
일반적으로 태양광 추적 장치는 태양광을 센서로 측정하여 추종하는 방식, 프로그램에 따라 미리 입력된 시간에 맞추어 회전하는 방식, 사용자에 의해 수동으로 구동되는 방식 등이 있다. 상술한 바와 같이 태양광 발전의 효율을 높이기 위해서는 일조량에 따라 태양 전지 패널이 추종하여 회전하는 것이 중요하기 때문이다. 또한, 태양광을 추종하도록 구동되는 회동 방식은 동서 방향으로 회동하며 일주 운동만을 하는 단축식과, 동서 방향 및 남북 방향으로 회동하면서 일주 운동과 연주 운동을 동시에 하는 양축식으로 구분되기도 한다.In general, the solar tracking device includes a method of measuring and tracking sunlight with a sensor, a method of rotating according to a predetermined time according to a program, and a method of being manually driven by a user. As described above, in order to increase the efficiency of photovoltaic power generation, it is important that the solar cell panel follow and rotate according to the amount of sunshine. In addition, the rotation method driven to follow the solar light may be divided into a short axis type that rotates in the east-west direction and performs only a round motion, and a biaxial type that simultaneously performs the round motion and playing motion while rotating in the east-west direction and the north-south direction.
이하에서는 도면을 참조하여 본 발명의 일실시예에 따른 태양광 추적 장치에 대하여 상세히 설명하기로 한다.Hereinafter, with reference to the drawings will be described in detail with respect to the solar tracking device according to an embodiment of the present invention.
도 1 및 도 2를 참조하면 본 발명의 태양광 추적 장치(100)는 고정프레임(S), 제1 프레임(110), 중심축(120), 제2 프레임(130), 제1 회전 제한수단(140), 제2 회전 제한수단(150) 및 중력방향 표시기(160)를 포함하여 이루어진다.1 and 2, the solar tracking device 100 of the present invention includes a fixed frame S, a first frame 110, a central axis 120, a second frame 130, and a first rotation limiting means. 140, the second rotation limiting means 150, and the gravity direction indicator 160.
태양 전지 유닛(미도시)은 태양광을 집광하여 태양 에너지를 다른 에너지로 변환시키는 장치이며 전기 에너지로 변환시키는 것이 일반적이나 설계에 따라 직접 열에너지로 변환하는 경우도 있다. 따라서 상기 태양 전지 유닛은 태양광을 집광하는 태양 전지 판과 에너지를 변환하는 변환 장치 및 저장하는 에너지 저장 장치 등으로 구비될 수 있으며, 이는 일반적인 경우와 동일하므로 자세한 설명은 생략하기로 한다. 태양전지는 태양빛의 에너지를 전기에너지로 바꾸는 것으로 P형 반도체와 N형 반도체라고 하는 2종류의 반도체를 사용해 전기를 생성한다. 태양전지에 빛을 비추면 내부에서 전자와 정공이 발생하는데 발생된 전하들은 P, N극으로 이동하며 이 현상에 의해 P극과 N극 사이에 전위차(광기전력)가 발생하며 이때, 태양전지에 부하를 연결하면 전류가 흐르게 되는데 이를 광전 효과라 한다. 태양전지는 실리콘 반도체를 재료로 사용하는 것과 화합물 반도체를 재료로 하는 것으로 크게 나눌 수 있다. 다시 실리콘 반도체에 의한 것은 결정계와 비결정계(AMOLFASS)로 분류될 수 있다.A solar cell unit (not shown) is a device that condenses sunlight and converts solar energy into other energy, and it is common to convert solar energy into electrical energy. Therefore, the solar cell unit may be provided with a solar panel for condensing sunlight, a conversion device for converting energy, and an energy storage device for storing the energy, which are the same as in the general case, and thus a detailed description thereof will be omitted. Solar cells convert the energy of sunlight into electrical energy and generate electricity using two types of semiconductors, P-type semiconductors and N-type semiconductors. When light shines on the solar cell, electrons and holes are generated inside. The generated charges move to the P and N poles, and a potential difference (photovoltaic power) is generated between the P pole and the N pole by this phenomenon. Connecting a load causes current to flow, which is called the photoelectric effect. Solar cells can be roughly divided into those using a silicon semiconductor as a material and a compound semiconductor as a material. In addition, the silicon semiconductor may be classified into a crystal system and an amorphous system (AMOLFASS).
상기 고정프레임(S)은 상기 태양 전지 유닛을 본 발명의 태양광 추적 장치에 고정시키기 위한 구성으로 통상의 프레임이 적용될 수 있다. 상기 고정프레임(S)은 빔 상으로 다수 개가 일정거리 이격 형성된다.The fixed frame (S) is a configuration for fixing the solar cell unit to the solar tracking device of the present invention can be applied to a conventional frame. The fixed frame (S) is a plurality of spaced apart a predetermined distance on the beam.
상기 제1 프레임(110)은 상기 고정프레임(S)을 지지하기 위한 수단으로 제1 가로프레임(111), 제1 세로프레임(112), 제1 회전축(113), 제1 보강대(114) 및 제2 기어 휠(153)을 포함한다.The first frame 110 is a means for supporting the fixed frame (S), the first horizontal frame 111, the first vertical frame 112, the first rotating shaft 113, the first reinforcing rod 114 and And a second gear wheel 153.
상기 제1 가로프레임(111)은 빔 상으로 다수 개가 일정거리 이격 형성된다. 상기 제1 세로프레임(112)은 빔 상으로 다수 개가 일정거리 이격 형성되되, 상기 제1 가로프레임(111)과 직교하도록 결합된다. 상기 제1 세로프레임(112)에는 하면 중심에 제1 회전축(113)이 형성되고, 상기 제1 회전축(113)의 양단에는 일단이 상기 제1 회전축(113)에 연결되고 타단이 상기 제1 세로프레임(112)에 연결되는 제1 보강대(114)가 설치된다. 상기 제1 회전축(113) 및 제1 보강대(114)는 상기 제1 세로프레임(112) 각각에 형성될 수 있다. 상기 제2 기어 휠(153)은 상기 제1 세로프레임(112) 중 어느 하나에 설치되며, 이에 대한 상세 설명은 제2 회전 제한수단(150)에서 후술하기로 한다.A plurality of the first horizontal frame 111 is formed spaced apart a predetermined distance on the beam. A plurality of first vertical frames 112 are formed on the beam spaced apart from each other by a predetermined distance, and are coupled to be orthogonal to the first horizontal frames 111. A first rotating shaft 113 is formed at the center of the lower surface of the first vertical frame 112, and both ends of the first rotating shaft 113 are connected to the first rotating shaft 113, and the other end thereof is the first vertical axis. The first reinforcement 114 is connected to the frame 112 is installed. The first rotation shaft 113 and the first reinforcing rod 114 may be formed in each of the first vertical frames 112. The second gear wheel 153 is installed on any one of the first vertical frame 112, a detailed description thereof will be described later in the second rotation limit means (150).
도 1 및 도 2를 참조하면 상기 중심축(120)은 상기 태양광 추적 장치(100)를 지지하는 축으로 일단이 바닥면에 고정된 채 상방으로 연장되어 있다. 상기 중심축(120)의 타단은 상기 제2 프레임(130)과 결합되되, 상기 태양 전지 유닛이 남북 방향으로 회전하도록 힌지 결합되는 것이 바람직하다. 상기 중심축(120)과 상기 제2 프레임(130)의 결합 위치는 상기 태양 전지 유닛이 고정되는 고정프레임(S)과 제1 프레임(110)의 무게 중심점에서 결합되는 것이 바람직하다. 종래의 구조와 달리 본 발명에 따른 태양광 추적 장치(100)의 경우 상기 태양 전지 유닛을 회전시키는 구동 장치만 구비되었을 뿐, 스크루 잭과 같은 보조 장비가 없다. 따라서 상기 태양 전지 유닛, 고정프레임(S), 제1 프레임(110) 및 제2 프레임(130)이 모두 상기 제2 프레임(130)과 상기 중심축(120)의 결합 지점인 상기 중심축(120)의 타단 단부에 의해 지지된다. 상기 중심축(120)과 상기 제2 프레임(130)이 결합되는 위치를 상기 태양 전지 유닛, 고정프레임(S) 및 제1 프레임(110)의 무게 중심점으로 선택하면, 상기 태양 전지 유닛이 어떠한 각도로 회전하더라도 구조적 안정성을 유지할 수 있다. 상기 중심축(120)은 상기 태양광 추적 장치(100)를 지지하는 기단부에 해당하므로 충분한 강성을 지닌 재질로 형성되는 것이 좋다.1 and 2, the central axis 120 is an axis for supporting the solar tracking device 100 and is extended upward with one end fixed to the bottom surface. The other end of the central axis 120 is coupled to the second frame 130, it is preferable that the hinge coupled to rotate the solar cell unit in the north-south direction. The coupling position of the central axis 120 and the second frame 130 is preferably coupled at the center of gravity of the fixed frame (S) to which the solar cell unit is fixed and the first frame (110). Unlike the conventional structure, the solar tracking device 100 according to the present invention is provided with only a driving device for rotating the solar cell unit, and there is no auxiliary equipment such as a screw jack. Therefore, the solar cell unit, the fixed frame (S), the first frame 110 and the second frame 130 are all the central axis 120 that is the coupling point of the second frame 130 and the central axis 120. Is supported by the other end of the When the position where the central axis 120 and the second frame 130 are coupled is selected as the center of gravity of the solar cell unit, the fixed frame S, and the first frame 110, the solar cell unit may be at an angle. Even if it rotates, structural stability can be maintained. Since the central axis 120 corresponds to the proximal end supporting the solar tracking device 100, the central axis 120 may be formed of a material having sufficient rigidity.
도 3 및 도 4를 참조하면 상기 제2 프레임(130)은 상기 중심축(120)에 결합되고 제1 회전 제한수단(140) 및 제2 회전 제한수단(150)을 구비하여 상기 태양 전지 유닛의 회전 반경을 제한할 수 있다.3 and 4, the second frame 130 is coupled to the central axis 120 and includes a first rotation limiting unit 140 and a second rotation limiting unit 150 of the solar cell unit. The radius of rotation can be limited.
상기 제2 프레임(130)은 상기 제1 회전축(113)에 힌지 결합되는 회전프레임(135), 제1 기어 휠(143), 상기 회전프레임(135)의 일단과 제1 기어 휠(143)의 일단을 연결하는 경사프레임(133), 상기 회전프레임(135)의 타단과 제1 기어 휠(143)의 타단을 연결하는 하부프레임(134), 상기 회전프레임(135)과 경사프레임(133)을 연결하며, 제1 회전 제한수단(140)이 설치되는 수평프레임(131) 및 상기 경사프레임(133)과 하부프레임(134)을 연결하는 수직프레임(132)을 포함하여 이루어진다. 상기 수직프레임(131)은 제1 수직프레임(132a)과 제2 수직프레임(132b)의 이중구조로 이루어지며, 각 제1, 제2 및 제3 병렬프레임(132c, 132d, 132e)에 고정된다. 상기 수직프레임(132)을 이중 구조로 구성하여 상기 제2 프레임(130)의 구조적 강도를 보장하게 된다.The second frame 130 of the rotary frame 135, the first gear wheel 143, one end of the rotary frame 135 and the first gear wheel 143 hinged to the first rotation shaft 113 The inclined frame 133 connecting one end, the lower frame 134 connecting the other end of the rotating frame 135 and the other end of the first gear wheel 143, the rotating frame 135 and the inclined frame 133 And a horizontal frame 131 on which the first rotation limiting unit 140 is installed, and a vertical frame 132 connecting the inclined frame 133 and the lower frame 134. The vertical frame 131 has a dual structure of the first vertical frame 132a and the second vertical frame 132b, and is fixed to each of the first, second and third parallel frames 132c, 132d, and 132e. . The vertical frame 132 is configured in a double structure to ensure the structural strength of the second frame 130.
상기 회전프레임(135)은 상기 중심축(120)의 일단에 형성되는 힌지 결합부(121)와 힌지 결합되기 위한 제2 회전축(135a), 상기 제1 회전축(113)에 힌지 결합되는 메인회전프레임(135b), 상기 회전프레임(135)의 구조적 강도를 보강하기 위한 보조 회전프레임(135c), 제 2보강프레임(135d), 트러스프레임(135e)으로 구성된다.The rotation frame 135 is a second rotation shaft 135a for hinge coupling with the hinge coupling portion 121 formed at one end of the central shaft 120, the main rotation frame hinged to the first rotation shaft 113 135b, an auxiliary rotating frame 135c for reinforcing the structural strength of the rotating frame 135, a second reinforcing frame 135d, and a truss frame 135e.
상기 제1 회전 제한수단(140)은 상기 태양 전지 유닛의 남북 방향의 회전 반경을 제한하는 범위에서 다양한 구조로 구비될 수 있다. 상기 제1 회전 제한수단(140)은 계절별로 태양의 고도가 달라지는 태양의 연주 운동과 관련되므로, 지구의 지축 경사각을 고려하여 60도 이내로 회전하도록 회전각을 제한하는 것이 바람직하다. 도 2에서는 상기 제1 회전 제한수단(140)이 제1 웜 기어(141)가 제1 연결기어(142)를 통해 제1 기어 휠(143)과 맞물려 구동되는 웜 기어 방식으로 형성되는 경우를 예시하여 도시하고 있다. 이러한 웜 기어 방식의 경우 상기 제1 기어 휠(142)은 남북 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 회전 궤적을 따라 상기 제2 프레임(130)에서 원주 방향으로 형성되도록 구비되는 것이 좋다. 또한 제1 회전 제한수단(140)에서는 상술한 바와 같이 60도 이내의 회전각을 갖도록 하면 충분하므로, 상기 중심축(120)과 상기 태양 전지 유닛의 결합 점을 회전 중심으로 하여 예각이 60도 이내가 되도록 상기 제1 기어 휠(142)이 형성될 수 있다. 상기 제1 웜 기어(141)는 상기 중심축(120)에 구비되는 제1 모터(M1)를 동력으로 하여 회전하도록 형성되는 것이 바람직하다. 이와 같이 상기 제1 회전 제한수단(140)이 웜 기어 방식으로 구비되는 경우 웜의 회전수를 조절하는 방식으로, 회전각을 정밀하게 제어할 수 있어 태양광을 정확하게 추종하기 쉬운 장점이 있다. 또한, 웜 기어 방식은 역전 현상이 발생하지 않으므로 안정적이다.The first rotation limiting unit 140 may be provided in various structures in a range of limiting the radius of rotation of the solar cell unit in the north-south direction. Since the first rotation limiting unit 140 is related to the playing movement of the sun in which the altitude of the sun varies depending on the season, it is preferable to limit the rotation angle to rotate within 60 degrees in consideration of the earth's axis tilt angle. 2 illustrates a case in which the first rotation limiting unit 140 is formed in a worm gear type in which the first worm gear 141 is driven in engagement with the first gear wheel 143 through the first connection gear 142. Is shown. In the case of the worm gear system, the first gear wheel 142 may be formed in the circumferential direction of the second frame 130 along the rotational trajectory of the solar cell unit rotating in the north-south direction. In addition, in the first rotation limiting means 140, as described above, it is sufficient to have a rotation angle within 60 degrees. Thus, the acute angle is within 60 degrees by using the coupling point of the central axis 120 and the solar cell unit as the rotation center. The first gear wheel 142 may be formed to be. The first worm gear 141 is preferably formed to rotate by using the first motor (M1) provided in the central shaft 120 as a power. As such, when the first rotation limiting unit 140 is provided in a worm gear type, the rotation angle of the worm can be controlled in a precise manner so that the rotation angle can be precisely controlled to accurately follow sunlight. In addition, the worm gear system is stable because no reversal phenomenon occurs.
상기 제2 회전 제한수단(150)은 상기 태양 전지 유닛의 동서 방향의 회전 반경을 제한하는 범위에서 다양한 구조로 구비될 수 있다. 상기 제2 회전 제한수단(150)의 경우 상기 제1 회전 제한수단(140)과 차이점만을 중심으로 설명하기로 한다. 상기 제1 회전 제한수단(140)이 상기 태양 전지 유닛의 남북 방향 회전을 제한함에 비해, 상기 제2 회전 제한수단(150)은 상기 태양 전지 유닛의 동서 방향 회전 반경을 제한한다. 따라서 상기 제2 회전 제한수단(150)은 지구의 자전에 따라 태양이 동쪽에서 서쪽으로 움직이는 태양의 일주 운동과 관련이 있으므로, 동쪽과 서쪽의 지평선을 고려하여 약 170도 이내로 회전하도록 회전각을 제한하는 것이 바람직하다. 도 2에서는 상기 제1 회전 제한수단(140)과 마찬가지로 상기 제2 회전 제한수단(150)이 웜 기어 방식으로 형성되는 경우를 예시하여 도시하고 있다. 이와 같이 웜 기어 방식으로 상기 제2 회전 제한수단(150)이 형성되는 경우, 상기 제2 기어 휠(153)은 동서 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 회전 궤적을 따라 배치되도록 상기 제1 프레임(110)에 위치된다. 따라서 상기 제 1 기어 휠(143)이 상기 제2 프레임(130)에 수평하도록 구비되는 것과 달리, 상기 제2 기어 휠(153)은 상기 제2 프레임(130)에 수직하도록 제1 프레임(110)에 구비될 수 있다. 상기 제2 회전 제한수단(150)은 제2 웜 기어(151)가 제2 연결기어(152)를 통해 제2 기어 휠(153)과 맞물려 구동되는 웜 기어 방식으로 형성된다. 상기 제2 프레임(130)에 구비된 제2 모터(M2)를 동력으로 제2 웜 기어(151)가 회전하면 상기 제2 기어 휠(153)은 상기 제1 프레임(110)과 일체로 동서 방향으로 회전하게 된다.The second rotation limiting means 150 may be provided in various structures in a range of limiting the radius of rotation of the solar cell unit in the east-west direction. In the case of the second rotation limiting means 150, only the difference from the first rotation limiting means 140 will be described. The second rotation limiting means 150 limits the east-west rotation radius of the solar cell unit, whereas the first rotation limiting means 140 limits the north-south rotation of the solar cell unit. Therefore, since the second rotation limiting means 150 is related to the circumferential motion of the sun moving from east to west according to the rotation of the earth, the rotation angle is limited to rotate within about 170 degrees in consideration of the east and west horizons. It is preferable. FIG. 2 exemplarily illustrates a case in which the second rotation limiting means 150 is formed in a worm gear type similarly to the first rotation limiting means 140. As described above, when the second rotation limiting means 150 is formed by the worm gear method, the second gear wheel 153 is arranged along the rotation trajectory of the solar cell unit rotating in the east-west direction. Located in frame 110. Therefore, unlike the first gear wheel 143 is provided to be horizontal to the second frame 130, the second gear wheel 153 is perpendicular to the second frame 130, the first frame 110 It may be provided in. The second rotation limiting means 150 is formed in a worm gear type in which the second worm gear 151 is driven in engagement with the second gear wheel 153 through the second connecting gear 152. When the second worm gear 151 is rotated by the power of the second motor M2 provided in the second frame 130, the second gear wheel 153 is integral with the first frame 110 in the east-west direction. Will rotate.
이때, 본 발명의 태양 추적 장치는 중심축(120)과 지면과의 기울기에 관계 없이 태양의 고도를 정확하게 추적하기 위해 다음과 같은 구성을 갖게 된다.At this time, the sun tracking device of the present invention has the following configuration to accurately track the altitude of the sun irrespective of the inclination of the central axis 120 and the ground.
도 4를 참조하면, 상기 중력방향 표시기(160)는 상기 제2 프레임(130) 상에 설치되며, 중력방향 즉 지표와 직교하는 위치를 제2 기어 휠(143)상에 표시하게 된다. 상기 중력방향 표시기(160)는 연결부(161), 로드(162) 및 무게추(163)로 구성된다. 상기 연결부(161)는 상기 제2 프레임(130) 상의 제2 회전축(135a)에 형성된다. 상기 로드(162)는 일단이 상기 연결부(161)에 연결되며, 상기 연결부(161)와 상기 무게추(163)를 일직선으로 연결시킬 수 있는 구성이면 어떠한 구성도 적용이 가능하다. 상기 무게추(163)는 상기 로드(162)의 타단에 연결되며, 통상의 무게추 구성이 적용될 수 있다. Referring to FIG. 4, the gravitational direction indicator 160 is installed on the second frame 130 and displays a location on the second gear wheel 143 that is perpendicular to the gravitational direction, that is, the indicator. The gravity direction indicator 160 is composed of a connecting portion 161, rod 162 and weight 163. The connection part 161 is formed on the second rotation axis 135a on the second frame 130. One end of the rod 162 is connected to the connecting portion 161, and any configuration may be applied as long as the connecting portion 161 and the weight 163 can be connected in a straight line. The weight 163 is connected to the other end of the rod 162, a conventional weight configuration can be applied.
상기와 같은 구성을 통해 중심축(120)이 지면과 직교하지 않더라도 중력방향 표시기(160)를 통해 지면과 수직인 점을 가늠하여 제2 기어 휠(143)상에 표시하기 때문에 상기 중력방향 표시기(160)와 제2 기어 휠(143)과의 상대 기울기를 통하여 태양의 고도를 정확하게 추적할 수 있게 된다.Although the central axis 120 is not orthogonal to the ground through the configuration as described above, the gravity direction indicator is displayed on the second gear wheel 143 by measuring the point perpendicular to the ground through the gravity direction indicator 160. It is possible to accurately track the altitude of the sun through the relative inclination between the 160 and the second gear wheel 143.
본 발명의 상기한 실시 예에 한정하여 기술적 사상을 해석해서는 안된다. 적용범위가 다양함은 물론이고, 청구범위에서 청구하는 본 발명의 요지를 벗어남이 없이 당업자의 수준에서 다양한 변형 실시가 가능하다. 따라서 이러한 개량 및 변경은 당업자에게 자명한 것인 한 본 발명의 보호범위에 속하게 된다.The technical spirit should not be interpreted as being limited to the above embodiments of the present invention. Various modifications may be made at the level of those skilled in the art without departing from the spirit of the invention as claimed in the claims. Therefore, such improvements and modifications fall within the protection scope of the present invention as long as it will be apparent to those skilled in the art.

Claims (7)

  1. 태양광을 집광하여 에너지를 변환하는 태양 전지 유닛을 지지하는 제1 프레임;A first frame that supports a solar cell unit that condenses sunlight to convert energy;
    상기 제1 프레임이 동서 방향으로 회전하도록 힌지 결합되는 제2 프레임;A second frame hinged to rotate the first frame in a east-west direction;
    일단이 바닥면에 고정된 채 상방으로 연장되고 타단이 제2 프레임과 결합되되, 상기 태양 전지 유닛이 남북 방향으로 회전하도록 힌지 결합되는 중심축;A central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, the central axis being hinged to rotate in the north-south direction;
    상기 제2 프레임 및 중심축에 구비되며, 상기 제1 프레임의 남북 방향 회전 반경을 제한하는 제1 회전 제한수단;First rotation limiting means provided on the second frame and the central axis to limit a north-south rotation radius of the first frame;
    상기 제1 프레임 및 제2 프레임에 구비되며, 상기 제1 프레임의 동서 방향 회전 반경을 제한하는 제2 회전 제한수단; 및Second rotation limiting means provided in the first frame and the second frame to limit the east-west rotation radius of the first frame; And
    일단이 바닥면에 고정된 채 상방으로 연장되고 타단이 제2 프레임과 결합되되, 상기 태양 전지 유닛이 남북 방향으로 회전하도록 힌지 결합되는 중심축;A central axis of which one end is extended upward while the other end is fixed to the bottom surface and the other end is coupled to the second frame, the central axis being hinged to rotate in the north-south direction;
    을 포함하는 것을 특징으로 하는 태양광 추적 장치.Photovoltaic tracking device comprising a.
  2. 제 1항에 있어서,The method of claim 1,
    상기 제2 프레임에는,In the second frame,
    중력방향을 표시하기 위한 중력방향 표시기;가 더 구비되는 것을 특징으로 하는 태양광 추적 장치.And a gravity direction indicator for displaying the gravity direction.
  3. 제 2항에 있어서,The method of claim 2,
    상기 중력방향 표시기는,The gravity direction indicator,
    상기 제2 프레임과 중심축과의 힌지결합부에 형성되는 연결부와, 일단이 상기 연결부에 연결되는 로드와, 상기 로드의 타단에 연결되는 무게추로 구성되는 것을 특징으로 하는 태양광 추적 장치.And a connecting portion formed at the hinge coupling portion between the second frame and the central axis, a rod connected at one end to the connecting portion, and a weight connected to the other end of the rod.
  4. 제 1항에 있어서,The method of claim 1,
    상기 제1 회전 제한수단은 제1 웜기어와 제1 기어휠이 맞물려 구동되며, 상기 제2 회전 제한수단은 제2 웜 기어와 제2 기어 휠이 맞물려 구동되는 것을 특징으로 하는 태양광 추적 장치.The first rotation limiting means is driven by meshing the first worm gear and the first gear wheel, the second rotation limiting means is a solar tracking device characterized in that the second worm gear and the second gear wheel is driven in engagement.
  5. 제 4항에 있어서,The method of claim 4, wherein
    상기 제1 기어 휠은 남북 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 궤적을 따라 상기 제 2프레임에 구비되고,The first gear wheel is provided in the second frame along the trajectory of the solar cell unit rotating in the north-south direction,
    상기 제1 웜 기어는 상기 중심축에 구비되는 제1 모터에 의해 회전하도록 형성되는 것을 특징으로 하는 태양광 추적 장치.The first worm gear is a solar tracking device, characterized in that formed to rotate by a first motor provided on the central axis.
  6. 제 4항에 있어서,The method of claim 4, wherein
    상기 제2 기어 휠은 동서 방향으로 회전하는 상기 태양 전지 유닛이 이동하는 궤적을 따라 상기 제1 프레임에 구비되고,The second gear wheel is provided in the first frame along the trajectory of the solar cell unit rotating in the east-west direction,
    상기 제2 웜 기어는 상기 제2 프레임에 구비되는 제2 모터에 의해 회전하도록 형성되는 것을 특징으로 하는 태양광 추적 장치.The second worm gear is a solar tracking device, characterized in that formed to rotate by a second motor provided in the second frame.
  7. 제 1 항에 있어서,The method of claim 1,
    상기 중심축의 타단과 상기 제2 프레임이 결합되는 지점은 상기 태양 전지 유닛 및 상기 제1 프레임의 무게 중심점인 것을 특징으로 하는 태양광 추적 장치.The point at which the other end of the central axis and the second frame are coupled is a center of gravity of the solar cell unit and the first frame.
PCT/KR2011/010275 2010-12-29 2011-12-29 Solar tracking apparatus WO2012091475A2 (en)

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KR20100066065A (en) * 2008-12-09 2010-06-17 미래에너지기술(주) Sun location tracking type solar generation apparatus
KR20100102402A (en) * 2009-03-11 2010-09-24 윤정식 Sunlight-tracking apparatus for solar cell module panel
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KR20100102402A (en) * 2009-03-11 2010-09-24 윤정식 Sunlight-tracking apparatus for solar cell module panel

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