1312054 九、發明說明： . 【發明所屬之技術領域】 本發明係有關於一種百葉窗式之太陽追蹤器，尤 指一種可大幅降低太陽追蹤器運作所需之直立高度， 並強化整體結構剛性及強度，以省去地基施工複雜繁 靖之程序。可適用於屋頂及平地架設使用，而達到有 效降低系統安裝之成本。 • 【先前技術】 以在太陽追縱器基座主要係在地基中設置一支 柱，而該支柱係為空心厚壁管狀，並於上方處提供一 固定插管’以插置結合於太陽追蹤器及太陽電池模組 之下方，雖然該太陽追蹤器之基座具有承載結合各式 太陽追蹤器及太陽電池模組之功效，但為了該太陽追 蹤器基座之支柱能夠固定於地基而需要耗費較多時 間、場所及經費於地基之建造設置’且其施工複雜繁 _ 瑣之程序也不適於屋頂架設使用。 故’一般習用者係無法符合使用者於實際使用時 之所需。 【發明内容】 本發明之主要目的係在於，提供承载高效率聚光 型III-V族太陽電池模組以追縱太陽軌跡，使該太陽電 池模組接收更多日照光能，以達成最大之發電量輸出。 1312054 本發明之另一目的係在於，採取方位及仰角驅動 . 模式設計’可大幅降低太陽追蹤器運作所需之直立高 度。 本發明之又一目的係在於，以方位機構、底盤圓 形軌道及支撐輪去強化整體結構剛性及強度，可省去 地基施工複雜繁瑣之程序，以適用於屋頂及平地架設 使用’並能有效降低系統安裝之成本。 • 為達以上之目的’本發明係一種百葉窗式之太陽 追蹤器，至少包含有三太陽電池模組支架組、一仰角 致動器組、三仰角主橫樑組、二平行連桿組、一上部 支撐結構組、一方位馬達減速機及蜗桿組、一方位支 撐作動軸及軸承組及一方位轴承外固定座底盤組，其 中，該太陽電池模組支架組係可承載16個該太陽電池 模組，且3套該太陽電池模組支架組共可承載48個該 太陽電池模組，每個該太陽電池模組發電量約為 110W，故共可產生約52kw發電輸出；該仰角致動器 組之伸長及縮短致動器可使該太陽電池模組支架組之 作動自由度為水平夾角0度〜80度區間；該仰角主橫 樑組係以其兩端軸承連結於太陽追蹤器主結構，以帶 動該太陽電池模組支架組作仰角自由度旋轉 ;該平行 連桿組係分別固^於靠近該仰角主橫樑組支撐抽承之 =側，並透過該仰角致動器組推動其中-套該平行連 才干組’該上部支樓結構組之端點下方係分別有 6個結 6 構之支撐H綠^座錢㈣具有4隻 k伸腳’並向外連結該上部支撑結構組之結構支樓輪 所行走之圓形軌道。 【實施方式】 請參閱『第1圖〜第15圖』所示，係分別為本 發明之立體結構示意圖、本發明之前視結構示意圖、 本發明之俯視結構示意圖、本發明之右視結構示意 圖本發明之上部立體結構示意圖 '本發明之下部立 體結構示意圖、本發明之太陽電池模組支架組示意 圖、本發明之仰角致動器組示意圖、本發明之仰角主 橫樑組示意圖、第9圖中A之細部示意圖、本發明之 平行連桿組示意圖、本發明之上部支撐結構組示意 圖、本發明之方位馬達減速機及堝桿組示意圖、本發 明之方位支撐作動軸及軸承組示意圖及本發明之方位 軸承外固定座底盤組示意圖。如第1圖〜第6圖所 示：本發明係一種百葉窗式之太陽追蹤器，至少包含 有二太％電池模組支架組1 1、一仰角致動器組1 2、三仰角主橫樑組1 3、二平行連桿組1 4、一上 部支撐結構組1 5、一方位馬達減速機及蝸桿組1 6、一方位支撐作動軸及軸承組1 7及一方位軸承外 固定座底盤組1 8,可提供承載高效率聚光型πΐ-ν族 太陽電池模組以追蹤太陽軌跡，使該太陽電池模組接 收更多日照光能，達到最大發電量輸出。 13.12054 • 該太陽電池模組支架組1 1 (請參第7圖），係將 該太陽電池模組固定於其上’且每個該太陽電池模組 支架組1 1係可承載16個該太陽電池模組，故3套該 太陽電池模組支架組1 1子陣列係可承載48個該太 陽電池模組，並且一個該太陽電池模組發電量約為 110W，所以共可產生約5.2kW發電輸出。 該仰角致動器組1 2 (請參第8圖），係藉由伸長 致動器及縮短致動器以推動該太陽電池模組支架組1 1，以達到仰角作動控制之要求，其中，該太陽電池 模組支架組1 1作動自由度係與水平夹角〇度至8〇度 區間。 該仰角主橫樑組1 3 (請參第9圖），係作為支撐 該太陽電池模組支架組1 i之用，且該仰角主橫樑組 13之兩端係由軸承131(請參第1〇囷）連結於 太陽追蹤器主結構，以帶動該太陽電池模組支架組工 籲1作仰角自由度旋轉’其中’該仰角主橫樑組丄3係 具有3套，且個別承载支撐其16個該太陽電池模組及 該太陽電池模組支架組1 1。 該平行連桿組1 4 (請參第i i圖），係連結3套 該太陽電池模組支架組1 i於同一側，而該平行連桿 組1 4係具有2套且分別固定於靠近該仰角主橫標組 1 3支樓該轴承1 3 1之内側，以透過該仰角致動器 組1 2推動其中一套該平行連桿組j 4，使3套該太 8 1312054 陽電池模組支架組1 1同步進行仰角自由度旋轉作動 —致性。 該上部支撐結構組1 5 (請參第1 2圖），係支撐 該太陽電池模組支架組1 1、該仰角致動器組1 2、 該仰角主橫樑1 3及該平行連桿組1 4等荷重，以減 少該太陽電池模組支架組1 1之變形量，且該上部支 撑結構組1 5之端點下方係分別具有6個結構之支撐 輪1 5 1 ’可將該上部支撐結構組1 5之荷重直接由 下方圓形軌道支撐’以強化太陽追蹤器上部結構（請 參第5圖）之剛性及強度’並且利於該太陽電池模組 追蹤太陽直射光線之精確度。 該方位馬逹減速機及蝸桿組1 6 (請參第1 3 圖）’係驅動方位之機構，藉由馬達透過減速機帶動蝸 桿’再由蝸桿傳動蜗輪以達到驅動方位旋轉，使太陽 追蹤器進行方位自由度作動β 該方位支撐作動軸及軸承組17(請參第14 圖），係支撐該上部支撐結構組1 5，且將重量集中於 方位支撐作動軸，並藉由該方位馬達減速機及蝸桿組 1 6之直流馬達及減速機驅動大蜗輪以控制其方位作 動。 該方位轴承外固定座底盤組1 8 (請參第丄5 圖）’係將該方位支撐作動軸及轴承組1 7所支撑該上 部支撐結構組]5之重量傳刭地面或f頂棒板支撐， 9 1312054 且該方位軸承外固定座底盤組1 8係具有4隻延伸 腳，並向外連結該上部支撐結構組i 5之支撐輪工5 1所行走之圓形軌道，以使整個太陽追蹤器重心穩定 且安全運作而不會傾倒。 當本發明於運用時，係將承載該太陽電池模組之 該太陽電池模組支架組1 1區分為三組子陣列，利用 該平行連桿組1 4傳動三組該太陽電池模組支架組工 籲 1進行仰角同步作動，並以該方位馬達減速機及堝桿 組1 6整合直流馬達（DC motor)、減速機及蝸輪組件 以進行驅動，再由該方位軸承外固定座底盤組1 8之 底盤圓形軌道及該支撐輪1 5 1去強化整體結構剛性 及強度，以追蹤太陽軌跡，使該太陽電池模組接收更 多曰照光能’而達成最大之發電量輸出。 綜上所述，本發明係一種百葉窗式之太陽追蹤 器，可有效改善習用之種種缺點，以提供承載高效率 • 聚光型ΙΠ-ν族太陽電池模組追蹤太陽轨跡，並省去地 基施工複雜繁瑣之程序，可適用於屋頂及平地架設使 用，能有效降低系統安裝之成本，進而使本發明之産 生能更進步、更實用、更符合使用者之所須，確已符 合發明專利申請之要件，爰依法提出專利申請。 惟以上所述者，僅為本發明之較佳實施例而已， 當不能以此限定本發明實施之範圍；故，凡依本發明 申請專利範圍及發明說明書内容所作之簡單的等效變 10 1312054 化與修飾，皆應仍屬本發明專利涵蓋之範圍内。 1312054 【圖式簡單說明】 第1圖，係本發明之立體結構示意圖。 第2圖’係本發明之前視結構示意圖。 第3圖，係本發明之俯視結構示意圖。 第4圖，係本發明之右視結構示意圖。 第5圖’係本發明之上部立鱧結構示意圓。 第6圖’係本發明之下部立想結構示意圖。 第7圖’係本發明之太陽電池模組支架組示意圖。 第8圖，係本發明之仰角致動器組示意圖。 第9圖，係本發明之仰角主橫樑組示意圖。 第1 0圖，係第9圖中a之細部示意圖。 第1 1圖，係本發明之平行連桿組示意圖。 第1 2圖，係本發明之上部支撐結構組示意圖。 第1 3圖，係本發明之方位馬達減速機及蜗桿組示意 圖。 第1 4圖’係本發明之方位支撐作動軸及軸承組示意 圖。 第1 5圖’係本發明之方位軸承外固定座底盤組示意 圖。 12 1312054 【主要元件符號說明】 太陽電池模組支架組11 仰角致動器組1 2 仰角主橫樑組13 轴承1 3 1 平行連桿組1 4 上部支撐結構組15 支撐輪151 方位馬達減速機及蜗桿組16 方位支撐作動軸及轴承組17 方位軸承外固定座底盤組1 81312054 IX. Description of the invention: 1. Field of the Invention The present invention relates to a louver type solar tracker, and more particularly to an upright height required to greatly reduce the operation of a solar tracker, and to enhance overall structural rigidity and strength. In order to save the complexity of the foundation construction procedures. It can be used for roof and flat erection, and it can effectively reduce the cost of system installation. • [Prior Art] The main base of the sun chaser is provided with a pillar in the foundation, and the pillar is hollow thick-walled tubular, and a fixed cannula is provided at the top to be inserted and coupled to the sun tracker. And under the solar battery module, although the base of the solar tracker has the function of supporting various solar trackers and solar battery modules, it is necessary to fix the pillars of the solar tracker base to the foundation. More time, place and funding for the construction of the foundation' and its construction is complicated and complicated. The trivial procedure is also not suitable for roof erection. Therefore, the general practitioners cannot meet the needs of the user in actual use. SUMMARY OF THE INVENTION The main object of the present invention is to provide a high-efficiency concentrating type III-V solar cell module to track the solar trajectory, so that the solar cell module receives more sunshine light energy to achieve maximum Power generation output. 1312054 Another object of the present invention is to drive the azimuth and elevation angles. The mode design can greatly reduce the erect height required for the operation of the solar tracker. Another object of the present invention is to enhance the rigidity and strength of the overall structure by the orientation mechanism, the circular circular track of the chassis and the support wheel, thereby eliminating the complicated and cumbersome procedure of foundation construction, and being suitable for roof and flat erection use and effective Reduce the cost of system installation. • For the above purposes, the present invention is a louver-type solar tracker comprising at least three solar cell module support sets, an elevation actuator set, three elevation main beam sets, two parallel link sets, and an upper support. The structural group, the one-direction motor reducer and the worm group, the one-direction supporting actuating shaft and the bearing group, and the one-way bearing outer fixing base plate group, wherein the solar battery module bracket group can carry 16 solar battery modules And 3 sets of the solar battery module bracket group can carry 48 solar battery modules, each of which generates about 110W, so a total of about 52kw power generation output can be generated; the elevation actuator group The elongation and shortening actuators enable the degree of freedom of movement of the solar battery module bracket group to be between 0 degrees and 80 degrees in a horizontal angle; the main beam assembly of the elevation angle is coupled to the main structure of the sun tracker by the bearings at both ends thereof. Driving the solar battery module bracket group for elevation angle degree rotation; the parallel link group is respectively fixed to the side of the supporting main beam group supporting the pumping belt, and is driven by the elevation angle actuator group The middle-sleeve parallel-connected group 'the lower part of the upper branch structure group has six knots 6 respectively supporting the support H green ^ seat money (four) has 4 k-extension feet ' and externally connects the upper support structure The circular track of the structure of the branch of the building. [Embodiment] Please refer to FIG. 1 to FIG. 15 for a schematic view of a three-dimensional structure of the present invention, a schematic view of a front view of the present invention, a schematic plan view of the present invention, and a schematic diagram of a right-view structure of the present invention. BRIEF DESCRIPTION OF THE EMBODIMENT OF THE INVENTION The schematic diagram of the three-dimensional structure of the lower part of the present invention, the schematic diagram of the solar cell module support set of the present invention, the schematic diagram of the elevation angle actuator set of the present invention, the schematic diagram of the elevation main beam set of the present invention, and the figure A of FIG. Schematic diagram of detail, parallel diagram of parallel linkage set of the present invention, schematic diagram of upper support structure of the present invention, schematic diagram of azimuth motor reducer and mast set of the present invention, schematic diagram of azimuth support actuation shaft and bearing set of the present invention, and the present invention Schematic diagram of the abutment bearing outer fixed base plate set. As shown in FIG. 1 to FIG. 6 , the present invention is a louver type sun tracker, which comprises at least two solar cell module support groups 1 , an elevation actuator group 1 2 , and an elevation angle main beam group. 1 3, two parallel link sets 1 4, an upper support structure group 1 5, an azimuth motor reducer and a worm set 16 , an azimuth support actuating shaft and bearing set 1 7 and an azimuth bearing outer mount chassis set 1 8, can provide high-efficiency concentrating πΐ-ν solar cell module to track the sun's trajectory, so that the solar cell module receives more sunlight energy to achieve maximum power output. 13.12054 • The solar battery module bracket set 1 1 (refer to Fig. 7) is to fix the solar battery module thereon] and each of the solar battery module bracket groups 1 1 can carry 16 such suns The battery module, so the three sets of solar cell module support group 1 1 sub-array can carry 48 solar cell modules, and one solar cell module generates about 110W, so a total of about 5.2kW can be generated. Output. The elevation actuator group 12 (refer to FIG. 8) is configured to elevate the solar battery module bracket group 1 by elongating the actuator and shortening the actuator to achieve the elevation control. The solar cell module support group 1 1 has a degree of freedom of freedom and a horizontal angle to a range of 8 degrees. The elevation main beam group 13 (refer to FIG. 9) is used for supporting the solar battery module bracket group 1 i, and the two ends of the elevation main beam group 13 are supported by bearings 131 (please refer to the first section)囷) is connected to the main structure of the solar tracker to drive the solar battery module bracket assembly to make an elevation angle of freedom rotation. [The elevation angle of the main beam group 丄3 series has 3 sets, and the individual load supports 16 of them. The solar battery module and the solar battery module bracket set 1 1 . The parallel link set 14 (refer to FIG. ii) is connected to three sets of the solar battery module bracket group 1 i on the same side, and the parallel link set 14 has two sets and is respectively fixed to the same The elevation angle main group 1 3 is the inner side of the bearing 1 3 1 , and the set of the parallel link group j 4 is pushed through the elevation actuator group 1 2 to make 3 sets of the 8 1312054 positive battery module bracket Group 1 1 synchronizes the elevation angle of freedom rotation actuation. The upper support structure group 15 (refer to FIG. 12) supports the solar battery module bracket group 1 1 , the elevation angle actuator group 1 2 , the elevation main beam 13 and the parallel link group 1 4 load, so as to reduce the deformation of the solar battery module bracket group 1 1 , and the lower end of the upper support structure group 15 has 6 structural support wheels 1 5 1 ' can be the upper support structure The load of Group 1 5 is directly supported by the circular track below to enhance the rigidity and strength of the solar tracker's upper structure (see Figure 5) and to facilitate the solar cell module to track the accuracy of direct sunlight. The azimuth gear reducer and the worm group 16 (refer to Fig. 1 3) 'the mechanism for driving the azimuth, the motor drives the worm through the reducer', and then the worm drive worm wheel to achieve the driving azimuth rotation, so that the sun tracker Performing azimuth degree of freedom actuation β The azimuth supporting the actuating shaft and bearing set 17 (see Figure 14) supports the upper support structure set 15 and concentrates the weight on the azimuth support actuating axis and is decelerated by the azimuth motor The DC motor and reducer of the machine and the worm group 16 drive the large worm gear to control its azimuth operation. The azimuth bearing outer fixing base plate group 1 8 (refer to FIG. 5) is the weight of the abutting support actuating shaft and the bearing group 17 supported by the upper supporting structure group 5 Support, 9 1312054 and the azimuth bearing outer mount chassis set 8 8 has 4 extension legs, and connects outwardly to the circular support of the upper support structure group i 5 supporting the wheeler 5 1 to make the whole sun The tracker's center of gravity is stable and safe to operate without dumping. When the present invention is applied, the solar battery module bracket group 1 1 carrying the solar battery module is divided into three sub-arrays, and the parallel rod group 14 is used to drive three sets of the solar battery module bracket group. The machine 1 performs the synchronous operation of the elevation angle, and the DC motor, the reducer and the worm gear assembly are integrated by the azimuth motor reducer and the mast group 16 to drive, and then the abutment bearing outer fixed chassis group 1 8 The circular circular track of the chassis and the support wheel 1 5 1 enhance the rigidity and strength of the overall structure to track the solar trajectory, so that the solar cell module receives more illuminating light energy to achieve the maximum power output. In summary, the present invention is a louver type sun tracker, which can effectively improve various disadvantages of the conventional use to provide high efficiency of carrying. • The concentrating type ΙΠ-ν solar cell module tracks the solar trajectory and saves the foundation. The complicated and cumbersome procedure can be applied to roof and flat erection, which can effectively reduce the cost of system installation, and thus make the invention more progressive, more practical and more suitable for users. It has indeed met the invention patent application. The key requirements are to file a patent application in accordance with the law. However, the above is only the preferred embodiment of the present invention, and the scope of the present invention is not limited thereto; therefore, the simple equivalent of the invention and the content of the invention is 10 1312054 Both modifications and modifications are still within the scope of the invention. 1312054 BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic perspective view of the present invention. Fig. 2 is a schematic view showing the structure of the present invention. Figure 3 is a schematic plan view of the present invention. Fig. 4 is a schematic view showing the right side structure of the present invention. Fig. 5 is a schematic circle of the upper vertical structure of the present invention. Fig. 6 is a schematic view showing the structure of the lower part of the present invention. Figure 7 is a schematic view of a solar battery module bracket set of the present invention. Figure 8 is a schematic view of an elevation actuator group of the present invention. Figure 9 is a schematic view of the elevation main beam set of the present invention. Figure 10 is a detailed view of a in Figure 9. Figure 11 is a schematic view of a parallel link set of the present invention. Figure 12 is a schematic view of the upper support structure of the present invention. Fig. 1 is a schematic view of the azimuth motor reducer and the worm set of the present invention. Figure 14 is a schematic view of the azimuth support actuation shaft and bearing assembly of the present invention. Fig. 15 is a schematic view of the abutment bearing outer mount chassis of the present invention. 12 1312054 [Description of main component symbols] Solar battery module bracket group 11 Elevation actuator group 1 2 Elevation main beam group 13 Bearing 1 3 1 Parallel link group 1 4 Upper support structure group 15 Support wheel 151 Azimuth motor reducer and Worm set 16 Azimuth support actuating shaft and bearing set 17 Azimuth bearing outer mount base plate set 1 8
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