WO2016078493A1 - 复合材料太阳能发电支架 - Google Patents

复合材料太阳能发电支架 Download PDF

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Publication number
WO2016078493A1
WO2016078493A1 PCT/CN2015/092068 CN2015092068W WO2016078493A1 WO 2016078493 A1 WO2016078493 A1 WO 2016078493A1 CN 2015092068 W CN2015092068 W CN 2015092068W WO 2016078493 A1 WO2016078493 A1 WO 2016078493A1
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column
disposed
upright column
fixing block
mounting plate
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PCT/CN2015/092068
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English (en)
French (fr)
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顾建
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南通久盛新材料科技有限公司
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Publication of WO2016078493A1 publication Critical patent/WO2016078493A1/zh

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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
    • H02S20/30Supporting structures being movable or adjustable, e.g. for angle adjustment
    • 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
    • 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 invention relates to a composite solar power generation support.
  • the composite material is a mixture. It has played a big role in many fields, replacing many traditional materials.
  • Composite materials are divided into metal and metal composite materials, non-metal and metal composite materials, non-metal and non-metal composite materials according to their composition. According to its structural characteristics, it is further divided into: 1. Fiber reinforced composite material. Various fiber reinforcements are compounded in a matrix material. Such as fiber reinforced plastics, fiber reinforced metals, and the like. 2, sandwich composite material. It is made up of a combination of surface materials and core materials with different properties. Usually the surface material is high and thin; the core material is light and low in strength, but has a certain rigidity and thickness. Divided into solid sandwich and honeycomb sandwich. 3. Fine-grain composite materials.
  • the hard fine particles are uniformly distributed in the matrix, such as a dispersion strengthened alloy, a cermet, or the like.
  • Hybrid composite materials It is composed of two or more kinds of reinforcing phase materials mixed in one matrix phase material. Compared with ordinary single-reinforcing phase composite materials, its impact strength, fatigue strength and fracture toughness are significantly improved, and it has special thermal expansion properties. It is divided into intra-layer hybrid, inter-layer hybrid, sandwich hybrid, intra-layer/inter-layer hybrid and super hybrid composite.
  • fiber reinforced materials are the most widely used and the largest amount. It is characterized by a small specific gravity, a large specific strength and a specific modulus.
  • the specific strength and specific modulus are several times larger than steel and aluminum alloy, but also have excellent chemical stability, anti-friction wear resistance, self-lubricating, heat resistance, fatigue resistance, resistance Creep, noise reduction, electrical insulation and other properties.
  • the graphite fiber is compounded with a resin to obtain a material having a thermal expansion coefficient almost equal to zero.
  • Another feature of fiber reinforced materials is the anisotropy, so the fiber arrangement can be designed according to the strength requirements of different parts of the part.
  • Aluminum-based composites reinforced with carbon fiber and silicon carbide fibers maintain sufficient strength and modulus at 500 °C.
  • Silicon carbide fiber is compounded with titanium, which not only improves the heat resistance of titanium, but also is resistant to wear and can be used as an engine fan blade.
  • Silicon carbide fiber and ceramic composite the use temperature can reach 1500 ° C, than the use temperature of superalloy turbine blades (1100 ° C) Much higher.
  • Carbon fiber reinforced carbon, graphite fiber reinforced carbon or graphite fiber reinforced graphite, which constitute an ablation resistant material has been used in spacecraft, rocket missiles and atomic energy reactors.
  • Non-metallic matrix composites are used in automobiles and airplanes to reduce weight, increase speed and save energy due to their low density.
  • a composite sheet spring made of a mixture of carbon fiber and glass fiber has a stiffness and load carrying capacity comparable to that of a steel sheet spring having a weight more than five times.
  • FRP also known as GFRP
  • GFRP is a fiber reinforced plastic, generally referred to as glass fiber reinforced unsaturated polyester, epoxy resin and phenolic resin matrix.
  • FRP FRP-weight and high strength.
  • the relative density is between 1.5 and 2.0, only 1/4 to 1/5 of carbon steel, but the tensile strength is close to or even higher than that of carbon steel, and the specific strength can be compared with high-grade alloy steel.
  • Some epoxy FRPs have tensile, bending and compressive strengths of more than 400 MPa. preservative.
  • FRP is a good anti-corrosive material with good resistance to atmospheric, water and general concentrations of acids, bases, salts and a variety of oils and solvents.
  • Various structural products can be flexibly designed according to needs to meet the requirements of use, and the products can be well integrated.
  • the material can be fully selected to meet the performance of the product, such as: can be designed to resist corrosion, resistant to transient high temperature, the product has a particularly high strength in a certain direction, good dielectric properties, and so on. Excellent processability.
  • the molding process can be flexibly selected according to the shape, technical requirements, use and quantity of the product. (2) The process is simple, it can be molded at one time, and the economic effect is outstanding, especially for products with a complicated shape and less forming, and the process superiority is more prominent.
  • FRP The disadvantage of FRP is that the modulus of elasticity is low.
  • the strength of general-purpose polyester FRP is obviously lower than 50 °C, and it is generally only used below 100 °C; the general-purpose epoxy FRP is above 60 °C, and the strength is obviously decreased.
  • the use of composite materials in solar power generation brackets has also become widespread.
  • the Chinese patent discloses a solar concentrating heat power generation bracket including a torque frame and a cantilever bracket, which is fixed to the torque frame by bolts, and the torque frame is composed of multiple The struts are formed by bolting, and the end of the torque frame is provided with end support rods, and the cantilever bracket is formed by bolting a plurality of struts.
  • the cantilever bracket includes a left bracket and a right bracket, and the left bracket and the right bracket are fixed by the beam. Into a whole.
  • the Chinese patent discloses a solar panel bracket, which belongs to the field of solar power generation.
  • the bracket is disposed under the solar panel, and the joints in the bracket are bolted; in the technical solution of the present invention, the advantages of the prior art welding are replaced.
  • the bolts are easy to disassemble, and the height of the bracket can be adjusted as needed to maximize the efficiency of the solar panel.
  • the object of the present invention is to overcome the above limitations, thereby providing a composite solar power generation bracket with novel structure, convenient transportation, high safety factor, low cost, easy installation and not easy to be damaged.
  • a composite solar power generation bracket comprising a base, the upper surface of the base is provided with a sliding slot, the sliding slot is provided with a plurality of power generating brackets, and the lower end of the power generating bracket is provided
  • the first pulley block has a first I-shaped support on the upper surface of the first pulley block, the first I-shaped support is connected to the first fixed block by bolts, and the first fixed block is connected with the first column
  • the top end of the first column is connected to one end of the mounting plate, and the other end of the mounting plate is connected to the top end of the second column.
  • the surface of the mounting plate is provided with a plurality of mounting brackets, and the first column and the second column are provided with reinforcing ribs on one side.
  • a second fixing block is connected to the lower end of the second column, the second fixing block is connected to the second bracket by bolts, and the second bracket is connected to the second pulley seat, the first pulley seat And the second pulley seat is disposed on the sliding slot, and a support rod is disposed between the upper end of the first pillar and the lower middle end of the second pillar.
  • the first column and the second column are provided with structural gussets.
  • the first post has a length of 924 mm
  • the mounting plate has a length of 1250 mm
  • the second post has a length of 1504 mm.
  • the composite solar power generation bracket of the present invention has the following advantages: novel structure, convenient transportation, high safety factor, low cost, easy installation, and not easy to damage.
  • Figure 1 is a schematic view of the present invention
  • FIG. 2 is a schematic view of a single unit of the power generating bracket of the present invention.
  • a composite solar power generation bracket as shown in FIG. 1 and FIG. 2, includes a base 1.
  • the upper surface of the base 1 is provided with a sliding slot 2, and the sliding slot 2 is provided with a plurality of power generating brackets, and the power generating bracket a first pulley block 3 is disposed at a lower end thereof, and a first I-shaped brace 4 is disposed on an upper surface of the first pulley block 3, and the first I-shaped brace 4 is connected to the first fixing block 5 by bolts, and the first fixing block
  • a first column 6 is connected to the block 5, the top end of the first column 6 is connected to one end of the mounting plate 7, and the other end of the mounting plate 7 is connected to the top end of the second column 8.
  • the mounting plate 7 is provided with a plurality of mounting brackets 15 on the surface thereof.
  • a reinforcing rib 9 is disposed on one side of the first column 6 and the second column 8 , and a second fixing block 10 is connected to the lower end of the second column 6 , and the second fixing block 10 is connected to the second I-shaped struts 11 by bolts.
  • the second I-shaped brace 11 is connected to the second pulley block 12, and the first pulley block 3 and the second pulley block 12 are both disposed on the chute 2, and the upper end of the first upright column 6 and the second upright column
  • a support rod 13 is provided between the lower middle end of the 8th.
  • Structural gussets 14 are provided on the first uprights 6 and the second uprights 8.
  • the first column 6 has a length of 924 mm
  • the mounting plate 7 has a length of 1,250 mm
  • the second column 8 has a length of 1,504 mm.
  • the power generating bracket unit shown in FIG. 2 can be set as needed, that is, the required number and the distance between the individual monomers can be realized by the position adjustment of the unit on the chute 2.
  • the first column 6, the second column 8, the mounting plate 7, and the support rod 13 are mainly made of glass fiber reinforced plastic, that is, a glass reinforced plastic material.
  • the present invention is not limited to the above embodiments, and all the modes in which the present invention is constructed by a similar structure and method of the present invention are within the scope of the present invention.
  • the composite solar power generation bracket of the present invention has the following advantages: novel structure, convenient transportation, high safety factor, low cost, easy installation, and not easy to damage.

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  • Photovoltaic Devices (AREA)

Abstract

一种复合材料太阳能发电支架,包括底座(1),底座(1)上表面设有滑槽(2),滑槽(2)上设有多个发电支架,发电支架下端设有第一滑轮座(3),第一滑轮座(3)上表面设有第一工字撑(4),第一工字撑(4)通过螺栓连接有第一固定块(5),第一固定块(5)上连接有第一立柱(6),第一立柱(6)顶端连接安装板(7)一端,安装板(7)另一端连接在第二立柱(8)顶端,安装板(7)表面设有多个安装支架(15),第一立柱(6)与第二立柱(8)一侧均设有加强筋(9),第二立柱(8)下端连接有第二固定块(10),第二固定块(10)通过螺栓连接有第二工字撑(11),第二工字撑(11)连接在第二滑轮座(12)上,第一滑轮座(3)和第二滑轮座(12)均设在滑槽(2)上,第一立柱(6)上端与第二立柱(8)中下端之间设有支撑杆(13);其具有以下优点:结构合理,便于运输和安装,安全系数高成本低,不易损坏。

Description

复合材料太阳能发电支架 技术领域
本发明涉及一种复合材料太阳能发电支架。
背景技术
复合材料是一种混合物。在很多领域都发挥了很大的作用,代替了很多传统的材料。复合材料按其组成分为金属与金属复合材料、非金属与金属复合材料、非金属与非金属复合材料。按其结构特点又分为:1、纤维增强复合材料。将各种纤维增强体置于基体材料内复合而成。如纤维增强塑料、纤维增强金属等。2、夹层复合材料。由性质不同的表面材料和芯材组合而成。通常面材强度高、薄;芯材质轻、强度低,但具有一定刚度和厚度。分为实心夹层和蜂窝夹层两种。3、细粒复合材料。将硬质细粒均匀分布于基体中,如弥散强化合金、金属陶瓷等。4、混杂复合材料。由两种或两种以上增强相材料混杂于一种基体相材料中构成。与普通单增强相复合材料比,其冲击强度、疲劳强度和断裂韧性显著提高,并具有特殊的热膨胀性能。分为层内混杂、层间混杂、夹芯混杂、层内/层间混杂和超混杂复合材料。
复合材料中以纤维增强材料应用最广、用量最大。其特点是比重小、比强度和比模量大。例如碳纤维与环氧树脂复合的材料,其比强度和比模量均比钢和铝合金大数倍,还具有优良的化学稳定性、减摩耐磨、自润滑、耐热、耐疲劳、耐蠕变、消声、电绝缘等性能。石墨纤维与树脂复合可得到热膨胀系数几乎等于零的材料。纤维增强材料的另一个特点是各向异性,因此可按制件不同部位的强度要求设计纤维的排列。以碳纤维和碳化硅纤维增强的铝基复合材料,在500℃时仍能保持足够的强度和模量。碳化硅纤维与钛复合,不但钛的耐热性提高,且耐磨损,可用作发动机风扇叶片。碳化硅纤维与陶瓷复合,使用温度可达1500℃,比超合金涡轮叶片的使用温度(1100℃) 高得多。碳纤维增强碳、石墨纤维增强碳或石墨纤维增强石墨,构成耐烧蚀材料,已用于航天器、火箭导弹和原子能反应堆中。非金属基复合材料由于密度小,用于汽车和飞机可减轻重量、提高速度、节约能源。用碳纤维和玻璃纤维混合制成的复合材料片弹簧,其刚度和承载能力与重量大5倍多的钢片弹簧相当。
玻璃钢(FRP)亦称作GFRP,即纤维强化塑料,一般指用玻璃纤维增强不饱和聚脂、环氧树脂与酚醛树脂基体。以玻璃纤维或其制品作增强材料的增强塑料,称谓为玻璃纤维增强塑料,或称谓玻璃钢。由于所使用的树脂品种不同,因此有聚酯玻璃钢、环氧玻璃钢、酚醛玻璃钢之称。质轻而硬,不导电,机械强度高,回收利用少,耐腐蚀。可以代替钢材制造机器零件和汽车、船舶外壳等。
玻璃钢的优点是:轻质高强。相对密度在1.5~2.0之间,只有碳钢的1/4~1/5,可是拉伸强度却接近,甚至超过碳素钢,而比强度可以与高级合金钢相比。因此,在航空、火箭、宇宙飞行器、高压容器以及在其他需要减轻自重的制品应用中,都具有卓越成效。某些环氧FRP的拉伸、弯曲和压缩强度均能达到400Mpa以上。耐腐蚀。FRP是良好的耐腐材料,对大气、水和一般浓度的酸、碱、盐以及多种油类和溶剂都有较好的抵抗能力。已应用到化工防腐的各个方面,正在取代碳钢、不锈钢、木材、有色金属等。电性能好。是优良的绝缘材料,用来制造绝缘体。高频下仍能保护良好介电性。微波透过性良好,已广泛用于雷达天线罩。热性能良好。FRP热导率低,室温下为1.25~1.67kJ/(m·h·K),只有金属的1/100~1/1000,是优良的绝热材料。在瞬时超高温情况下,是理想的热防护和耐烧蚀材料,能保护宇宙飞行器在2000℃以上承受高速气流的冲刷。可设计性好。(1)可以根据需要,灵活地设计出各种结构产品,来满足使用要求,可以使产品有很好的整体性。(2)可以充分选择材料来满足产品的性能,如:可以设计出耐腐的,耐瞬时高温的、产品某方向上有特别高强度的、介电性好的,等等。工艺性优良。(1) 可以根据产品的形状、技术要求、用途及数量来灵活地选择成型工艺。(2)工艺简单,可以一次成型,经济效果突出,尤其对形状复杂、不易成型的数量少的产品,更突出它的工艺优越性。
玻璃钢的缺点是:弹性模量低。FRP的弹性模量比木材大两倍,但比钢(E=2.1E5)小10倍,因此在产品结构中常感到刚性不足,容易变形。可以做成薄壳结构、夹层结构,也可通过高模量纤维或者做加强筋等形式来弥补。长期耐温性差。一般FRP不能在高温下长期使用,通用聚酯FRP在50℃以上强度就明显下降,一般只在100℃以下使用;通用型环氧FRP在60℃以上,强度有明显下降。但可以选择耐高温树脂,使长期工作温度在200~300℃是可能的。老化现象。老化现象是塑料的共同缺陷,FRP也不例外,在紫外线、风沙雨雪、化学介质、机械应力等作用下容易导致性能下降。剪切强度低。层间剪切强度是靠树脂来承担的,所以很低。可以通过选择工艺、使用偶联剂等方法来提高层间粘结力,最主要的是在产品设计时,尽量避免使层间受剪。玻璃钢的生产方法基本上分两大类,即湿法接触型和干法加压成型。如按工艺特点来分,有手糊成型、层压成型、RTM法、挤拉法、模压成型、缠绕成型等。手糊成型又包括手糊法、袋压法、喷射法、湿糊低压法和无模手糊法。
复合材料在太阳能发电支架中的利用也逐渐广泛,中国专利公开了一种太阳能聚光热发电支架,包括扭矩框和悬臂支架,所述悬臂支架通过螺栓固定在扭矩框上,扭矩框由多个支杆通过螺栓连接形成,扭矩框的边角处设有端部支撑杆,悬臂支架由多个支杆通过螺栓连接形成,悬臂支架包括左支架和右支架,左支架和右支架通过横梁固连成一整体。
中国专利公开了一种太阳能板支架,属于太阳能发电领域,该支架设置在太阳能板下方,所述支架内的连接处为螺栓连接;本发明的技术方案中,取代现有技术的焊接,其优点是螺栓便于拆卸,根据需要可调节支架的高度,使之能够最大效率发挥太阳能板的作用。
发明内容
本发明的目的,在于克服上述局限,从而提供一种结构新颖,便于运输,安全系数高成本低,便于安装,不易损坏的一种复合材料太阳能发电支架。
本发明的目的通过以下技术方案来实现:一种复合材料太阳能发电支架,包括底座,所述底座上表面设有滑槽,所述滑槽上设有多个发电支架,所述发电支架下端设有第一滑轮座,所述第一滑轮座上表面设有第一工字撑,所述第一工字撑通过螺栓连接有第一固定块,所述第一固定块上连接有第一立柱,所述第一立柱顶端连接安装板一端,安装板另一端连接在第二立柱顶端,所述安装板表面设有多个安装支架,第一立柱与第二立柱一侧均设有加强筋,所述第二立柱下端连接有第二固定块,所述第二固定块通过螺栓连接有第二工字撑,所述第二工字撑连接在第二滑轮座上,所述第一滑轮座和第二滑轮座均设在滑槽上,所述第一立柱上端与第二立柱中下端之间设有支撑杆。
优选的是,第一立柱与第二立柱上设有结构角撑。
优选的是,第一立柱长度为924毫米,安装板长度为1250毫米,第二立柱长度为1504毫米。
综上所述,本发明的一种复合材料太阳能发电支架具有以下优点:结构新颖,便于运输,安全系数高成本低,便于安装,不易损坏。
附图说明
图1是本发明的示意图;
图2是本发明发电支架单体示意图;
图中标号:1-底座、2-滑槽、3-第一滑轮座、4-第一工字撑、5-第一固定块、6-第一立柱、7-安装板、8-第二立柱、9-加强筋、10-第二固定块、11-第二工字撑、12-第二滑轮座、13-支撑杆、14-结构角撑、15-安装支架。
具体实施方式
为了加深对本发明的理解,下面将结合实施例和附图对本发明作进一步详述,该实施例仅用于解释本发明,并不构成对本发明保护范围的限定。
如图1和图2所示的一种复合材料太阳能发电支架,包括底座1,所述底座1上表面设有滑槽2,所述滑槽2上设有多个发电支架,所述发电支架下端设有第一滑轮座3,所述第一滑轮座3上表面设有第一工字撑4,所述第一工字撑4通过螺栓连接有第一固定块5,所述第一固定块5上连接有第一立柱6,所述第一立柱6顶端连接安装板7一端,安装板7另一端连接在第二立柱8顶端,所述安装板7表面设有多个安装支架15,第一立柱6与第二立柱8一侧均设有加强筋9,所述第二立柱6下端连接有第二固定块10,所述第二固定块10通过螺栓连接有第二工字撑11,所述第二工字撑11连接在第二滑轮座12上,所述第一滑轮座3和第二滑轮座12均设在滑槽2上,所述第一立柱6上端与第二立柱8中下端之间设有支撑杆13。
第一立柱6与第二立柱8上设有结构角撑14。
第一立柱6长度为924毫米,安装板7长度为1250毫米,第二立柱8长度为1504毫米。
如图2所示的发电支架单体可以根据需要设置,即需要的数量以及各个单体之间的距离可以通过单体在滑槽2上的位置调节来实现。
第一立柱6、第二立柱8、安装板7和支撑杆13主要采用玻璃纤维增强塑料,即为玻璃钢材料。
申请人又一声明,本发明通过上述实施例来说明本发明的实现方法及装置结构,但本发明并不局限于上述实施方式,即不意味着本发明必须依赖上述方法及结构才能实施。所属技术领域的技术人员应该明了,对本发明的任何改进,对本发明所选用实现方法等效替换及步骤的添加、具体方式的选择等,均落在本发明的保护范围和公开的范围之内。
本发明并不限于上述实施方式,凡采用和本发明相似结构及其方法来实现本发明目的的所有方式,均在本发明的保护范围之内。
综上所述,本发明的一种复合材料太阳能发电支架具有以下优点:结构新颖,便于运输,安全系数高成本低,便于安装,不易损坏。

Claims (3)

  1. 一种复合材料太阳能发电支架,其特征在于:包括底座(1),所述底座(1)上表面设有滑槽(2),所述滑槽(2)上设有多个发电支架,所述发电支架下端设有第一滑轮座(3),所述第一滑轮座(3)上表面设有第一工字撑(4),所述第一工字撑(4)通过螺栓连接有第一固定块(5),所述第一固定块(5)上连接有第一立柱(6),所述第一立柱(6)顶端连接安装板(7)一端,安装板(7)另一端连接在第二立柱(8)顶端,所述安装板(7)表面设有多个安装支架(15),第一立柱(6)与第二立柱(8)一侧均设有加强筋(9),所述第二立柱(6)下端连接有第二固定块(10),所述第二固定块(10)通过螺栓连接有第二工字撑(11),所述第二工字撑(11)连接在第二滑轮座(12)上,所述第一滑轮座(3)和第二滑轮座(12)均设在滑槽(2)上,所述第一立柱(6)上端与第二立柱(8)中下端之间设有支撑杆(13)。
  2. 根据权利要求1所述的一种复合材料太阳能发电支架,其特征在于:所述第一立柱(6)与第二立柱(8)上设有结构角撑(14)。
  3. 根据权利要求1所述的一种复合材料太阳能发电支架,其特征在于:所述第一立柱(6)长度为924毫米,安装板(7)长度为1250毫米,第二立柱(8)长度为1504毫米。
PCT/CN2015/092068 2014-11-18 2015-10-16 复合材料太阳能发电支架 WO2016078493A1 (zh)

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