CN111834211A - Pretreatment method of silicon wafer and preparation method of stitched solar module - Google Patents
Pretreatment method of silicon wafer and preparation method of stitched solar module Download PDFInfo
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Abstract
Description
技术领域technical field
本发明属于光伏技术领域,特别涉及一种硅片的预处理方法及叠焊太阳能组件的制备方法。The invention belongs to the field of photovoltaic technology, and particularly relates to a method for pretreatment of silicon wafers and a method for preparing stitched solar modules.
背景技术Background technique
作为一种新的电池焊接工艺,叠焊技术在传统焊带焊接工艺的基础上实现电池片的叠加,缩小电池片间距,最大化利用面积,从而实现高能量密度。As a new battery welding process, stitch welding technology realizes the superposition of battery cells on the basis of the traditional ribbon welding process, reduces the spacing between cells, maximizes the utilization area, and achieves high energy density.
在叠焊太阳能组件的制备过程中,硅片分选结束后需要对硅片进行切割预处理,然后使用柔性焊带及定制工装,基于焊接技术,将硅片相互搭接焊接。其中,传统的硅片切割方式是:利用具有高能量密度的脉冲激光在硅片上划出一条沟槽,随后用机械方式将其掰开。对采用传统方式切割的硅片断面采用扫描电子显微镜观察,发现断面极不均匀,呈明显的波浪状,具有较多毛刺与裂纹,这是因为激光热度使电池切割截面产生了化学变化,出现了熔融现象,对硅片造成了严重的切割损伤。由于激光切割与机械掰片的交接点有应力,而硅片切割部位又位于焊带压延位置,因此切割过程中造成的硅片损伤最终影响到叠焊太阳能组件的质量,叠焊太阳能组件在层压后出现较多纹路隐裂。During the preparation of stitch-bonded solar modules, after the silicon wafers are sorted, the silicon wafers need to be cut and pretreated, and then the silicon wafers are lapped and welded based on the welding technology using flexible welding tapes and custom tooling. Among them, the traditional silicon wafer cutting method is to use a pulsed laser with high energy density to draw a groove on the silicon wafer, and then mechanically break it apart. The section of the silicon wafer cut by the traditional method was observed by scanning electron microscope, and it was found that the section was extremely uneven, with obvious wavy shape and many burrs and cracks. This is because the laser heat caused chemical changes in the cut section of the battery, and the The melting phenomenon caused serious cutting damage to the silicon wafer. Due to the stress at the junction point of laser cutting and mechanical breaking, and the cutting part of the silicon wafer is located at the calendering position of the welding tape, the damage of the silicon wafer caused by the cutting process will ultimately affect the quality of the stitched solar modules. After pressing, more lines and cracks appear.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于针对上述现有技术的不足,提供一种硅片的预处理方法及叠焊太阳能组件的制备方法。The purpose of the present invention is to provide a method for pretreatment of silicon wafers and a method for preparing stitched solar modules in view of the above-mentioned deficiencies of the prior art.
为解决上述技术问题,本发明的第一方面提供了一种硅片的预处理方法,依次包括:采用激光束对硅片待裂片部位的内部快速加热,以使所述硅片待裂片部位的内部膨胀形成压应力;采用流体束对硅片待裂片部位的表面快速冷却,以使所述硅片待裂片部位的表面收缩形成拉应力;所述硅片在所述压应力和所述拉应力的作用下发生裂片;将硅片的至少一部分表面暴露于等离子体中,对所述硅片的至少一部分表面进行等离子体刻蚀,其中,所述硅片的至少一部分表面包括硅片发生裂片部位的表面。In order to solve the above-mentioned technical problems, a first aspect of the present invention provides a method for preprocessing a silicon wafer, which sequentially includes: using a laser beam to rapidly heat the interior of the portion of the silicon wafer to be split, so that the portion of the silicon wafer to be split is rapidly heated. The internal expansion forms compressive stress; the surface of the part to be split of the silicon wafer is rapidly cooled by the fluid beam, so that the surface of the part to be split of the silicon wafer shrinks to form tensile stress; the silicon wafer is under the compressive stress and the tensile stress Splitting occurs under the action of the silicon wafer; at least a part of the surface of the silicon wafer is exposed to plasma, and plasma etching is performed on at least a part of the surface of the silicon wafer, wherein at least a part of the surface of the silicon wafer includes the part where the splitting occurs in the silicon wafer s surface.
相对于现有技术而言,本发明至少具有如下有益效果:Compared with the prior art, the present invention at least has the following beneficial effects:
本发明将应力裂片和等离子体刻蚀联合应用于硅片的预处理中。首先,采用激光束对硅片待裂片部位的内部快速加热,使硅片待裂片部位的内部膨胀形成压应力;采用流体束对硅片待裂片部位的表面快速冷却,使硅片待裂片部位的表面收缩形成拉应力;由于脆性材料抗压刚度远大于抗拉强度,当拉应力达到硅片的断裂强度时,硅片就会发生自然断裂,裂纹会随着激光及冷却移动轨道稳定扩展。本发明的方法避免了传统的“激光切割结合机械裂片”过程中对硅片的热力损伤和机械损伤,有效改善硅片断面的质量,同时也降低裂片过程中的破片率。其次,在使硅片发生应力裂片之后,对硅片进行等离子体刻蚀,去除硅片表面的扩散层以及裂片部位表面的轻微裂纹或粉尘,进一步改善了硅片的表面性质。The present invention combines stress slicing and plasma etching in the pretreatment of silicon wafers. First, a laser beam is used to rapidly heat the interior of the silicon wafer to be split, so that the internal expansion of the silicon wafer to be split forms compressive stress; a fluid beam is used to rapidly cool the surface of the silicon wafer to be split, so that the silicon wafer is to be split. The surface shrinks to form tensile stress; since the compressive stiffness of the brittle material is much greater than the tensile strength, when the tensile stress reaches the breaking strength of the silicon wafer, the silicon wafer will fracture naturally, and the crack will expand steadily with the laser and the cooling moving track. The method of the invention avoids the thermal damage and mechanical damage to the silicon wafer in the traditional process of "laser cutting combined with mechanical cracking", effectively improves the quality of the section of the silicon wafer, and also reduces the fragmentation rate during the splitting process. Secondly, after the silicon wafer is subjected to stress splits, plasma etching is performed on the silicon wafer to remove the diffusion layer on the surface of the silicon wafer and the slight cracks or dust on the surface of the split part, thereby further improving the surface properties of the silicon wafer.
本发明的第二方面还提供了一种叠焊太阳能组件的制备方法,该方法包括:根据本发明第一方面所述的方法对硅片进行预处理,将预处理后的硅片采用叠焊技术制备成太阳能组件。采用本发明第二方面所提供的方法制备的太阳能组件,纹路隐裂问题得到显著改善。The second aspect of the present invention also provides a method for preparing a stitch-bonded solar module, the method comprising: pre-processing a silicon wafer according to the method described in the first aspect of the present invention, and stitch-bonding the pre-treated silicon wafer technology to prepare solar modules. With the solar module prepared by the method provided in the second aspect of the present invention, the problem of cracking of lines is significantly improved.
优选地,在本发明所提供的硅片的预处理方法中,所述采用激光束对硅片待裂片部位的内部快速加热的步骤依次包括:采用波长为320~400nm、功率为3~5W的紫外激光束对所述硅片待裂片部位的内部快速加热;采用波长为1060~1100nm、功率为100~150W的红外激光束对所述硅片待裂片部位的内部快速加热。Preferably, in the pretreatment method for silicon wafers provided by the present invention, the step of rapidly heating the interior of the silicon wafer to be split by a laser beam sequentially includes: using a laser beam with a wavelength of 320-400 nm and a power of 3-5W The ultraviolet laser beam rapidly heats the interior of the silicon wafer to be split; the infrared laser beam with a wavelength of 1060-1100 nm and a power of 100 to 150 W is used to rapidly heat the interior of the silicon wafer to be split.
优选地,在本发明所提供的硅片的预处理方法中,所述硅片待裂片部位的内部与所述硅片待裂片部位的表面之间的距离为1~3mm。在该距离范围内,应力裂片的成功率和裂片效果最好。Preferably, in the pretreatment method of the silicon wafer provided by the present invention, the distance between the interior of the portion of the silicon wafer to be split and the surface of the portion to be split of the silicon wafer is 1˜3 mm. In this distance range, the success rate of stress cleavage and the cleaving effect are the best.
优选地,在本发明所提供的硅片的预处理方法中,所述采用流体束对硅片待裂片部位的表面快速冷却的步骤中,所述流体束选自液态水、液态二氧化碳、液态氢、液氮、低温惰性气体、低温二氧化碳气体、低温氢气、低温氮气中的至少一种。Preferably, in the pretreatment method for silicon wafers provided by the present invention, in the step of rapidly cooling the surface of the silicon wafer to be split by a fluid beam, the fluid beam is selected from liquid water, liquid carbon dioxide, liquid hydrogen , at least one of liquid nitrogen, low temperature inert gas, low temperature carbon dioxide gas, low temperature hydrogen gas, and low temperature nitrogen gas.
优选地,在本发明所提供的硅片的预处理方法中,所述流体束的温度为20~30℃。在本发明的方法中,激光束可使硅片待裂片部位的内部温度达到150~200℃,同时配合本发明的激光参数和加热位置,只需要在硅片待裂片部位的表面施以20~30℃的流体束进行快速冷却,就可实现应力裂片。20~30℃的流体束极易获取,并便于利用,使得本发明的方法可操作性好,易于工业应用。Preferably, in the pretreatment method for silicon wafers provided by the present invention, the temperature of the fluid beam is 20-30°C. In the method of the present invention, the laser beam can make the internal temperature of the part of the silicon wafer to be split to reach 150-200° C. At the same time, according to the laser parameters and the heating position of the present invention, it is only necessary to apply 20 to 20 to the surface of the part of the silicon wafer to be split. Stress splitting can be achieved by rapid cooling of the fluid beam at 30°C. The fluid beam at 20-30° C. is easy to obtain and easy to use, so that the method of the present invention has good operability and easy industrial application.
优选地,在本发明所提供的硅片的预处理方法中,所述等离子体刻蚀步骤在等离子体刻蚀机中进行。Preferably, in the method for pretreatment of silicon wafers provided by the present invention, the plasma etching step is performed in a plasma etcher.
优选地,在本发明所提供的硅片的预处理方法中,形成所述等离子体的气体至少包含CF4和O2,所述CF4的流量为100~120sccm/min,所述O2的流量为10~15sccm/min。Preferably, in the pretreatment method for silicon wafers provided by the present invention, the gas for forming the plasma contains at least CF 4 and O 2 , the flow rate of the CF 4 is 100-120 sccm/min, and the flow rate of the O 2 is 100-120 sccm/min. The flow rate is 10~15sccm/min.
优选地,在本发明所提供的硅片的预处理方法中,激发所述等离子体的高频辉光的压力为300~350Pa,功率为100~120W。Preferably, in the pretreatment method for silicon wafers provided by the present invention, the pressure of the high-frequency glow that excites the plasma is 300-350 Pa, and the power is 100-120 W.
优选地,在本发明所提供的硅片的预处理方法中,开启所述高频辉光的时间为10~18分钟,优选14分钟。Preferably, in the pretreatment method for silicon wafers provided by the present invention, the time for turning on the high-frequency glow is 10-18 minutes, preferably 14 minutes.
在本发明所提供的上述等离子体气体流量范围和高压辉光的压力和功率条件下,当开启高频辉光、对硅片表面进行的等离子体刻蚀时间为14分钟时,可使叠焊太阳能组件隐裂的改善效果达到最佳,整个组件的隐裂数量能控制在4处以内。Under the above-mentioned plasma gas flow rate range and the pressure and power conditions of the high-pressure glow provided by the present invention, when the high-frequency glow is turned on and the plasma etching time on the surface of the silicon wafer is 14 minutes, the stitched solar modules can be welded. The improvement effect of cracks is the best, and the number of cracks in the whole assembly can be controlled within 4 places.
附图说明Description of drawings
图1为实施例3中根据本发明的方法预处理后的硅片裂片边缘的扫描电子显微镜图;1 is a scanning electron microscope image of the edge of a silicon wafer lobe pretreated according to the method of the present invention in Example 3;
图2为对比例1中传统激光切片和等离子体刻蚀处理后的硅片切割边缘的扫描电子显微镜图;Fig. 2 is the scanning electron microscope picture of the silicon wafer cutting edge after traditional laser slicing and plasma etching treatment in Comparative Example 1;
图3为实施例3中根据本发明的方法预处理后的硅片裂片断面的扫描电子显微镜图;Fig. 3 is the scanning electron microscope image of the sliced section of the silicon wafer after pretreatment according to the method of the present invention in Example 3;
图4为对比例1中传统激光切片和等离子体刻蚀处理后的硅片切割断面的扫描电子显微镜图;Fig. 4 is the scanning electron microscope picture of the silicon wafer cut section after traditional laser slicing and plasma etching treatment in Comparative Example 1;
图5为一实施例的叠焊太阳能组件中相邻两个硅片搭接串联的结构示意图。FIG. 5 is a schematic structural diagram of two adjacent silicon wafers connected in series in a stitch-bonded solar module according to an embodiment.
具体实施方式Detailed ways
为了能够更清楚理解本发明的目的、特点和优势,下面结合附图对本发明的实施方式进行详细描述。所用材料未注明生产厂商者,均为可以通过市售购买获得的常规产品。对示例性实施方式的描述仅仅是出于示范目的,而非对本发明及其应用的限制。In order to understand the objects, features and advantages of the present invention more clearly, the embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The materials used without specifying the manufacturer are conventional products that can be purchased from the market. The description of the exemplary embodiments is for illustrative purposes only, and not for the purpose of limiting the invention and its applications.
根据本发明的第一方面,本发明的实施方式提供了一种硅片的预处理方法,依次包括:采用激光束对硅片待裂片部位的内部快速加热,以使所述硅片待裂片部位的内部膨胀形成压应力;采用流体束对硅片待裂片部位的表面快速冷却,以使所述硅片待裂片部位的表面收缩形成拉应力;所述硅片在所述压应力和所述拉应力的作用下发生裂片;将硅片的至少一部分表面暴露于等离子体中,对所述硅片的至少一部分表面进行等离子体刻蚀,其中,所述硅片的至少一部分表面包括硅片发生裂片部位的表面。According to the first aspect of the present invention, an embodiment of the present invention provides a method for preprocessing a silicon wafer, which sequentially includes: using a laser beam to rapidly heat the interior of the portion of the silicon wafer to be split, so that the portion of the silicon wafer to be split is rapidly heated. The internal expansion of the silicon wafer forms compressive stress; the surface of the silicon wafer to be split is rapidly cooled by a fluid beam, so that the surface of the silicon wafer to be split is contracted to form tensile stress; the silicon wafer is under the compressive stress and the tensile stress. Splitting occurs under the action of stress; at least a part of the surface of the silicon wafer is exposed to plasma, and at least a part of the surface of the silicon wafer is subjected to plasma etching, wherein at least a part of the surface of the silicon wafer includes the splitting of the silicon wafer surface of the part.
本发明的部分实施方式中,所述采用激光束对硅片待裂片部位的内部快速加热的步骤依次包括:先采用波长为320~400nm、功率为3~5W的紫外激光束对所述硅片待裂片部位的内部快速加热;然后采用波长为1060~1100nm、功率为100~150W的红外激光束对所述硅片待裂片部位的内部快速加热。作为一些实施方式的举例,可以采用波长为320nm、功率为3W的紫外激光束;波长为350nm、功率为5W的紫外激光束;波长为380nm、功率为4W的紫外激光束;波长为400nm、功率为4.5W的紫外激光束等。同样的,作为一些实施方式的举例,可以采用波长为1060nm、功率为100W的红外激光束;波长为1070nm、功率为110W的红外激光束;波长为1080nm、功率为120W的红外激光束;波长为1090nm、功率为130W的红外激光束;波长为1100nm、功率为150W的红外激光束等。In some embodiments of the present invention, the step of rapidly heating the interior of the silicon wafer to be split by a laser beam sequentially includes: firstly using an ultraviolet laser beam with a wavelength of 320-400 nm and a power of 3-5W to heat the silicon wafer The interior of the part to be split is rapidly heated; and then an infrared laser beam with a wavelength of 1060-1100 nm and a power of 100-150 W is used to rapidly heat the interior of the part to be split of the silicon wafer. As an example of some embodiments, an ultraviolet laser beam with a wavelength of 320nm and a power of 3W can be used; an ultraviolet laser beam with a wavelength of 350nm and a power of 5W; an ultraviolet laser beam with a wavelength of 380nm and a power of 4W; 4.5W UV laser beam, etc. Similarly, as an example of some embodiments, an infrared laser beam with a wavelength of 1060nm and a power of 100W can be used; an infrared laser beam with a wavelength of 1070nm and a power of 110W; an infrared laser beam with a wavelength of 1080nm and a power of 120W; the wavelength is Infrared laser beam with 1090nm and power of 130W; infrared laser beam with wavelength of 1100nm and power of 150W, etc.
本发明的部分实施方式中,所述硅片待裂片部位的内部与所述硅片待裂片部位的表面之间的距离为1~3mm。作为一些实施方式的举例,所述硅片待裂片部位的内部与所述硅片待裂片部位的表面之间的距离可以为1mm、1.5mm、2mm、2.5mm、3mm等。In some embodiments of the present invention, the distance between the interior of the portion to be split of the silicon wafer and the surface of the portion to be split of the silicon wafer is 1˜3 mm. As an example of some embodiments, the distance between the interior of the portion to be split of the silicon wafer and the surface of the portion to be split of the silicon wafer may be 1 mm, 1.5 mm, 2 mm, 2.5 mm, 3 mm, or the like.
本发明的部分实施方式中,所述采用流体束对硅片待裂片部位的表面快速冷却的步骤中,所述流体束选自液态水、液态二氧化碳、液态氢、液氮、低温惰性气体、低温二氧化碳气体、低温氢气、低温氮气中的至少一种。In some embodiments of the present invention, in the step of using a fluid beam to rapidly cool the surface of the silicon wafer to be split, the fluid beam is selected from liquid water, liquid carbon dioxide, liquid hydrogen, liquid nitrogen, low temperature inert gas, low temperature At least one of carbon dioxide gas, low temperature hydrogen gas, and low temperature nitrogen gas.
本发明的部分实施方式中,所述流体束的温度为20~30℃。作为一些实施方式的举例,所述流体束的温度可以为20℃、24℃、26℃、28℃或30℃等。In some embodiments of the present invention, the temperature of the fluid beam is 20-30°C. As an example of some embodiments, the temperature of the fluid beam may be 20°C, 24°C, 26°C, 28°C, or 30°C, and the like.
本发明的部分实施方式中,所述等离子体刻蚀步骤在等离子体刻蚀机中进行。本发明的实施方式对等离子体刻蚀机的牌号和型号没有特别的要求,只要能完成下述等离子体刻蚀工艺的等离子体刻蚀机都可适用:在低压下,反应气体在射频功率的激发下,产生电离并形成等离子体,等离子体是由带电的电子和离子组成,反应腔体中的气体在电子的撞击下,除了转变成离子外,还能吸收能量并形成大量的活性反应基团;活性反应基团和被刻蚀物质表面发生化学反应并形成挥发性的反应生成物;反应生成物脱离被刻蚀物质表面,并被真空系统抽出腔体。In some embodiments of the present invention, the plasma etching step is performed in a plasma etcher. The embodiment of the present invention has no special requirements on the brand and model of the plasma etching machine, as long as the plasma etching machine that can complete the following plasma etching process is applicable: under low pressure, the reaction gas is Under excitation, ionization is generated and a plasma is formed. The plasma is composed of charged electrons and ions. Under the impact of the electrons, the gas in the reaction chamber can absorb energy and form a large number of active reactive radicals in addition to being converted into ions. The active reactive group reacts chemically with the surface of the material to be etched and forms a volatile reaction product; the reaction product separates from the surface of the material to be etched and is drawn out of the cavity by the vacuum system.
本发明的部分实施方式中,形成所述等离子体的气体至少包含CF4和O2,所述CF4的流量为100~120sccm/min,所述O2的流量为10~15sccm/min。作为一些实施方式的举例,CF4的流量可以为100sccm/min、105sccm/min、110sccm/min、115sccm/min、120sccm/min等;O2的流量可以为10sccm/min、11sccm/min、12sccm/min、13sccm/min、14sccm/min、15sccm/min等。In some embodiments of the present invention, the gas forming the plasma contains at least CF 4 and O 2 , the flow rate of the CF 4 is 100-120 sccm/min, and the flow rate of the O 2 is 10-15 sccm/min. As an example of some embodiments, the flow rate of CF 4 may be 100sccm/min, 105sccm/min, 110sccm/min, 115sccm/min, 120sccm/min, etc.; the flow rate of O 2 may be 10sccm/min, 11sccm/min, 12sccm/min min, 13sccm/min, 14sccm/min, 15sccm/min, etc.
本发明的部分实施方式中,激发所述等离子体的高频辉光的压力为300~350Pa,功率为100~120W。作为一些实施方式的举例,激发所述等离子体的高频辉光的压力可以为300Pa、310Pa、320Pa、340Pa、350Pa等;功率可以为100W、105W、110W、115W、120W等。In some embodiments of the present invention, the pressure of the high-frequency glow for exciting the plasma is 300-350 Pa, and the power is 100-120 W. As an example of some embodiments, the pressure to excite the high-frequency glow of the plasma may be 300Pa, 310Pa, 320Pa, 340Pa, 350Pa, etc.; the power may be 100W, 105W, 110W, 115W, 120W, etc.
本发明的部分实施方式中,开启所述高频辉光的时间为10~18分钟。例如,开启所述高频辉光的时间可以为10分钟、12分钟、14分钟、16分钟、18分钟等。In some embodiments of the present invention, the high-frequency glow is turned on for 10-18 minutes. For example, the time for turning on the high-frequency glow may be 10 minutes, 12 minutes, 14 minutes, 16 minutes, 18 minutes, and the like.
根据本发明的第二方面,本发明的实施方式还提供了一种叠焊太阳能组件的制备方法,包括:根据本发明第一方面所述的方法对硅片进行预处理,将预处理后的硅片采用叠焊技术制备成太阳能组件。According to the second aspect of the present invention, an embodiment of the present invention further provides a method for preparing a stitch-bonded solar module, comprising: pre-processing a silicon wafer according to the method described in the first aspect of the present invention, Silicon wafers are fabricated into solar modules by stitch welding technology.
本发明的实施方式对采用叠焊技术制备太阳能组件的具体工艺步骤没有特殊的限定,可以按照本领域内常规的叠焊太阳能组件的制备方法进行。The embodiments of the present invention do not have special limitations on the specific process steps for preparing a solar module by using the stitch welding technology, which can be performed according to the conventional preparation method of a stitch welding solar module in the art.
本发明实施方式所提供的叠焊太阳能组件中,若干预处理后的硅片前后相互搭接串联,且相邻两个硅片之间设有焊带。在叠焊太阳能组件的制备过程中,可将焊带定位至相邻两个硅片之间,进行焊接,得到由若干硅片前后相互搭接串联的电池串;然后进行层压,并将玻璃基板、EVA胶膜层、电池串和背板等加热固化成刚性整体。由于预处理过程中的硅片裂片部位正处于与焊带重合的位置,因而在焊接和层压过程中,对硅片裂片部位的表面性质和抗应力性具有较高要求,如裂片部位在裂片过程中受到热影响或机械损伤,或者在裂片部位的表面具有较多微裂纹或毛刺,则导致层压后的组件中易产生纹路隐裂。In the stitch welding solar module provided by the embodiment of the present invention, a plurality of pretreated silicon wafers are overlapped and connected in series with each other, and a welding tape is provided between two adjacent silicon wafers. In the preparation process of the stitched solar module, the welding tape can be positioned between two adjacent silicon wafers and welded to obtain a battery string that is overlapped and connected in series by several silicon wafers; The substrate, EVA film layer, battery string and backplane are heated and cured into a rigid whole. Since the split part of the silicon wafer in the pretreatment process is in a position that coincides with the welding tape, the surface properties and stress resistance of the split part of the silicon wafer have higher requirements during the welding and lamination process. If it is thermally affected or mechanically damaged during the process, or there are many microcracks or burrs on the surface of the split part, it is easy to cause cracks in the laminated components.
以下结合具体实施例进一步说明本申请的优势。应理解,这些实施例仅用于说明本申请而不用于限制本申请的范围。除非特别规定,本说明书中涉及的各种参数具有本领域公知的通用含义,可以按本领域公知的方法进行测量。例如,可以按照在本申请的实施例中给出的方法进行测试。另外,各种优选实施例中给出的各种不同参数的优选范围和选项可以进行任意组合,由此得到的各种组合都视为在本申请的公开范围之内。The advantages of the present application are further described below with reference to specific embodiments. It should be understood that these examples are only used to illustrate the present application and not to limit the scope of the present application. Unless otherwise specified, various parameters involved in this specification have general meanings known in the art, and can be measured according to methods known in the art. For example, the tests can be performed according to the methods given in the examples of the present application. In addition, the preferred ranges and options of various parameters given in various preferred embodiments can be combined arbitrarily, and various combinations obtained thereby are considered to be within the scope of the disclosure of the present application.
实施例1~12Examples 1 to 12
1、硅片的预处理1. Pretreatment of silicon wafers
硅片分选后,先采用紫外激光束(连续激光)对硅片待裂片部位的内部快速加热1~2秒;然后采用红外激光束(连续激光)对硅片待裂片部位的内部快速加热1~2秒,以使硅片待裂片部位的内部膨胀形成压应力。采用流体束对硅片待裂片部位的表面快速冷却,冷却时间1~2秒,以使硅片待裂片部位的表面收缩形成拉应力。硅片在压应力和拉应力的作用下发生断裂,裂纹随着激光束与流体束的移动轨道稳定扩展。After the silicon wafer is sorted, the ultraviolet laser beam (continuous laser) is used to rapidly heat the interior of the silicon wafer to be split for 1-2 seconds; then the infrared laser beam (continuous laser) is used to rapidly heat the interior of the silicon wafer to be split for 1. ~2 seconds, so that the internal expansion of the silicon wafer to be split to form a compressive stress. A fluid beam is used to rapidly cool the surface of the silicon wafer to be split, and the cooling time is 1-2 seconds, so that the surface of the silicon wafer to be split is contracted to form tensile stress. The silicon wafer breaks under the action of compressive stress and tensile stress, and the crack expands stably with the moving track of the laser beam and the fluid beam.
将硅片置于等离子体刻蚀机中进行等离子体刻蚀,形成所述等离子体的气体包含CF4和O2,控制CF4的流量为100~120sccm/min、O2的流量为10~15sccm/min。等离子体刻蚀的具体工艺流程简述如下:开气,整机上电,高频预热,开泵,预抽尾气,关预抽开主抽,送入工艺气体(CF4和O2)并稀释,当压力稳定在设定值时开高频辉光放电,关闭高频辉光,关闭工艺气体,送氮气,充气开盖,取走硅片。The silicon wafer is placed in a plasma etching machine for plasma etching, the gas for forming the plasma contains CF 4 and O 2 , and the flow rate of CF 4 is controlled to be 100-120 sccm/min, and the flow rate of O 2 is 10- 15sccm/min. The specific process flow of plasma etching is briefly described as follows: turn on the gas, power on the whole machine, high-frequency preheating, turn on the pump, pre-pump the tail gas, turn off the pre-pump and open the main pump, and send the process gas (CF 4 and O 2 ) And diluted, when the pressure is stable at the set value, turn on the high-frequency glow discharge, turn off the high-frequency glow, turn off the process gas, send nitrogen, inflate the lid, and remove the silicon wafer.
2、叠焊太阳能组件的制备2. Preparation of stitch welding solar modules
采用常规的叠焊技术制备太阳能组件,具体工艺步骤简述如下:取若干预处理后的硅片,将焊带分别定位至相邻两个预处理后的硅片之间,进行焊接,得到由若干预处理后的硅片前后相互搭接串联的电池串;然后进行层压;并将玻璃基板、EVA胶膜层、电池串和背板等加热固化成刚性整体,得到叠焊太阳能组件。Using conventional stitch welding technology to prepare solar modules, the specific process steps are briefly described as follows: take a number of pretreated silicon wafers, position the welding strips between two adjacent pretreated silicon wafers, and weld them to obtain a A number of pretreated silicon wafers are overlapped with each other in series with battery strings; then laminated; and the glass substrate, EVA film layer, battery string and backplane are heated and cured into a rigid whole to obtain a stitched solar module.
实施例1~12的具体工艺参数参见表1所示。The specific process parameters of Examples 1-12 are shown in Table 1.
对比例1Comparative Example 1
对比例1与实施例3的区别在于:采用常规的激光切片机,以100W紫外激光对硅片进行激光开槽,随后用机械方式将其掰开。后续对硅片的等离子体刻蚀和叠焊太阳能组件的制备步骤与实施例3相同,具体工艺参数参见表1所示。The difference between Comparative Example 1 and Example 3 is that a conventional laser slicer is used to perform laser grooving on a silicon wafer with a 100W ultraviolet laser, and then mechanically break it apart. Subsequent preparation steps for plasma etching of silicon wafers and stitch welding of solar modules are the same as in Example 3, and the specific process parameters are shown in Table 1.
对比例2Comparative Example 2
对比例1与实施例3的区别在于:先采用红外激光束(连续激光)对硅片待裂片部位的内部快速加热1~2秒;再采用紫外激光束(连续激光)对硅片待裂片部位的内部快速加热1~2秒;然后采用流体束对硅片待裂片部位的表面快速冷却,硅片无法实现自然应力裂片,以机械方式配合裂片。后续对硅片的等离子体刻蚀和叠焊太阳能组件的制备步骤与实施例3相同,具体工艺参数参见表1所示。The difference between Comparative Example 1 and Example 3 is that: first, an infrared laser beam (continuous laser) is used to rapidly heat the interior of the silicon wafer to be split for 1 to 2 seconds; then an ultraviolet laser beam (continuous laser) is used to heat the silicon wafer to be split. The interior of the silicon wafer is rapidly heated for 1 to 2 seconds; then the surface of the silicon wafer to be split is rapidly cooled by a fluid beam, the silicon wafer cannot achieve natural stress splitting, and the splitting is mechanically matched. Subsequent preparation steps for plasma etching of silicon wafers and stitch welding of solar modules are the same as in Example 3, and the specific process parameters are shown in Table 1.
分别对实施例1~12、对比例1~2中预处理后的硅片和制备的叠焊太阳能组件进行硅片断面质量、硅片破片率和组件内纹路隐裂的观察与检测。The pretreated silicon wafers and the prepared stitch-bonded solar modules in Examples 1-12 and Comparative Examples 1-2 were respectively observed and detected for the cross-sectional quality of silicon wafers, the fragmentation rate of silicon wafers, and the cracks in the lines of the modules.
其中,组件内纹路隐裂的检测使用EL测试仪(太阳能电池组件缺陷检测全自动测试仪)进行测试,该测试仪利用晶体硅的电致发光原理,采用高分辨率的CCD相机拍摄组件的近红外图像,获取并判定组件的纹路隐裂缺陷。Among them, the detection of cracks in the module is carried out using an EL tester (automatic tester for defect detection of solar cell modules), which uses the electroluminescence principle of crystalline silicon and uses a high-resolution CCD camera to capture the close-up of the module. Infrared images to obtain and determine the cracking defects of the components.
图1为实施例3中根据本发明的方法预处理后的硅片裂片边缘的扫描电子显微镜图;图2为对比例1中传统激光切片和等离子体刻蚀处理后的硅片切割边缘的扫描电子显微镜图。Fig. 1 is the scanning electron microscope image of the edge of the silicon wafer after pretreatment according to the method of the present invention in Example 3; Fig. 2 is the scanning of the cutting edge of the silicon wafer after conventional laser slicing and plasma etching treatment in Comparative Example 1 Electron microscope image.
图3为实施例3中根据本发明的方法预处理后的硅片裂片断面的扫描电子显微镜图;图4为对比例1中传统激光切片和等离子体刻蚀处理后的硅片切割断面的扫描电子显微镜图。Fig. 3 is the scanning electron microscope image of the sliced section of the silicon wafer after pretreatment according to the method of the present invention in Example 3; Fig. 4 is the scanning of the cut section of the silicon wafer after conventional laser sectioning and plasma etching treatment in Comparative Example 1 Electron microscope image.
根据图1~4的对比可知:本发明实施例3中的硅片边缘无任何热影响区域,在硅片断面上,绝大部分区域内(>92%)不存在激光加工产生的微裂纹,仅有极少的材料去除,粉尘产生量可大大减少。这说明本发明所提供的预处理方法可有效降低电池片的切割损伤,提升硅片的机械强度,并使硅片有更好的电性能表现。而对比例1所采用的常规激光切片技术会在硅片边缘留下明显的热影响区域,对硅片断面产生的激光损伤深度几乎达到材料厚度的50%,硅片的断面上微裂纹较多,由此可导致硅片的机械强度降低,并且在加工过程中必然伴随大量粉尘的产生。According to the comparison of Figures 1 to 4, it can be seen that the edge of the silicon wafer in Example 3 of the present invention does not have any heat-affected zone. With very little material removed, dust generation can be greatly reduced. This shows that the pretreatment method provided by the present invention can effectively reduce the cutting damage of the cell, improve the mechanical strength of the silicon wafer, and make the silicon wafer have better electrical performance. In contrast, the conventional laser slicing technology used in Comparative Example 1 will leave an obvious heat-affected zone on the edge of the silicon wafer, the laser damage depth to the section of the silicon wafer is almost 50% of the material thickness, and there are many micro-cracks on the section of the silicon wafer. , which can reduce the mechanical strength of the silicon wafer, and must be accompanied by a large amount of dust during the processing.
图5为本发明一实施例的叠焊太阳能组件中相邻两个硅片搭接串联的结构示意图。如图5所示,经本发明方法预处理后的两个硅片1前后相互搭接串联,焊带2连接于相邻两个硅片中的第一硅片的下表面和第二硅片的上表面,硅片1的边缘3与焊带2重合,其中,硅片1的边缘3即为预处理过程中的硅片裂片部位。由于采用本发明所提供的方法预处理的硅片,其裂片部位未受到明显的热影响和机械损伤,且具有较佳的表面性质和较高的机械强度,因而在焊接和层压过程中不易产生纹路隐裂。FIG. 5 is a schematic structural diagram of two adjacent silicon wafers connected in series in a stitch-bonded solar module according to an embodiment of the present invention. As shown in FIG. 5 , the two
其余检测结果参见表1所示。The rest of the test results are shown in Table 1.
表1Table 1
实施例1~12采用了本发明所提供的方法对硅片进行预处理,并将预处理后的硅片制备成叠焊太阳能组件。对比例1采用了采用现有技术中常规的激光切片机切割结合机械掰开的方式对硅片进行切割,然后对切割后的硅片进行等离子体刻蚀,并进一步制备成叠焊太阳能组件。从表1中的检测结果可知,实施例1~12中的硅片断面均呈现出均匀、无毛刺和裂纹的状态,而对比例1的硅片断面不均匀,毛刺和裂纹较多。同时,实施例1~12的硅片破片率和组件纹路隐裂数量相较于对比例1都呈明显下降。这说明,本发明所提供的硅片预处理方法,可显著减少激光对硅片的切割损伤,使硅片裂片部位材质更加光滑均匀,无毛刺或裂纹,显著改善组件的纹路隐裂问题,并具有极低的破片率,有利于产能的提高。In Examples 1 to 12, the method provided by the present invention was used to pretreat the silicon wafer, and the pretreated silicon wafer was prepared into a stitch welding solar module. In Comparative Example 1, a conventional laser slicer cutting method combined with mechanical breaking is used to cut a silicon wafer, and then plasma etching is performed on the cut silicon wafer, and a stitch welding solar module is further prepared. From the test results in Table 1, it can be seen that the sections of the silicon wafers in Examples 1 to 12 are uniform and free of burrs and cracks, while the sections of the silicon wafers in Comparative Example 1 are uneven and have many burrs and cracks. At the same time, compared with Comparative Example 1, the silicon wafer fragmentation rate and the number of cracks in the component lines of Examples 1 to 12 were significantly decreased. This shows that the silicon wafer pretreatment method provided by the present invention can significantly reduce the laser cutting damage to the silicon wafer, make the material of the silicon wafer split part more smooth and uniform, without burrs or cracks, and significantly improve the cracking problem of the components. It has a very low fragmentation rate, which is beneficial to the improvement of production capacity.
对比例2虽然也采用了激光束对硅片内部加热、流体束对硅片表面冷却,但是其先采用红外激光束加热,后采用紫外激光束加热。在两步激光内部加热之后,结合流体束的表面冷却,硅片无法实现自然应力裂片,需机械力配合裂片。从表1的检测结果可知,对比例2对于硅片断面质量、破片率以及组件纹路隐裂的改善不明显。In Comparative Example 2, although the laser beam is also used to heat the inside of the silicon wafer and the fluid beam to cool the surface of the silicon wafer, it first uses an infrared laser beam for heating, and then uses an ultraviolet laser beam for heating. After the two-step laser internal heating, combined with the surface cooling of the fluid beam, the silicon wafer cannot achieve natural stress splitting, and mechanical force is required to cooperate with the splitting. From the test results in Table 1, it can be seen that Comparative Example 2 does not significantly improve the silicon chip section quality, fragmentation rate and component cracks.
实施例1~8和实施例9、10的区别在于:采用激光束对硅片待裂片部位的内部快速加热的步骤中,硅片内部的加热部位与硅片表面的距离不同。实施例1~8中的距离为1~3mm,而实施例9、10中的距离分别为0.5mm和4mm。从表1的检测结果可知,采用激光束对硅片待裂片部位的内部快速加热的步骤中,当硅片内部的加热部位与硅片表面的距离在1~3mm范围内,硅片的破片率最低,在裂片过程中对硅片的切割损伤最小。The difference between Examples 1 to 8 and Examples 9 and 10 is that in the step of rapidly heating the interior of the silicon wafer to be split by using a laser beam, the distance between the heating portion inside the silicon wafer and the surface of the silicon wafer is different. The distances in Examples 1 to 8 were 1 to 3 mm, while the distances in Examples 9 and 10 were 0.5 mm and 4 mm, respectively. From the test results in Table 1, it can be seen that in the step of rapidly heating the interior of the silicon wafer to be split by the laser beam, when the distance between the heating part inside the silicon wafer and the surface of the silicon wafer is within the range of 1 to 3 mm, the fragmentation rate of the silicon wafer will be reduced. Lowest, minimal dicing damage to the silicon wafer during the splitting process.
实施例1~8和实施例11~12的区别在于:对硅片进行等离子体刻蚀的步骤中,开启高频辉光的时间不同,即进行等离子体刻蚀的时间不同。实施例1~8中的离子体刻蚀的时间在10~18min范围内,而实施例11、12中的离子体刻蚀的时间分别为7min和23min。从表1的检测结果可知,等离子体刻蚀的时间在10~18min范围内,对组件纹路隐裂的改善效果最为明显。The difference between Examples 1 to 8 and Examples 11 to 12 is that in the step of plasma etching the silicon wafer, the time for turning on the high-frequency glow is different, that is, the time for plasma etching is different. The plasma etching time in Examples 1 to 8 is in the range of 10 to 18 min, while the plasma etching time in Examples 11 and 12 is 7 min and 23 min, respectively. From the test results in Table 1, it can be seen that the plasma etching time is in the range of 10 to 18 minutes, and the improvement effect on the cracks of the component lines is the most obvious.
上述实例只为说明本发明的技术构思及特点,其目的在于让熟悉此项技术的人是能够了解本发明的内容并据以实施,并不能以此限制本发明的保护范围。凡根据本发明精神实质所做的等效变换或修饰,都应涵盖在本发明的保护范围之内。The above examples are only to illustrate the technical concept and characteristics of the present invention, and the purpose is to enable those who are familiar with the technology to understand the content of the present invention and implement it accordingly, and cannot limit the protection scope of the present invention. All equivalent transformations or modifications made according to the spirit of the present invention should be covered within the protection scope of the present invention.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112599637A (en) * | 2020-12-09 | 2021-04-02 | 成都晔凡科技有限公司 | Method for manufacturing solar cell piece and solar cell piece |
| CN113555472A (en) * | 2021-07-16 | 2021-10-26 | 安徽华晟新能源科技有限公司 | Heterojunction cell processing method, sliced heterojunction cell and heterojunction cell assembly |
| CN114823317A (en) * | 2022-03-29 | 2022-07-29 | 通威太阳能(安徽)有限公司 | Silicon wafer cutting method and battery |
| CN115117193A (en) * | 2021-03-19 | 2022-09-27 | 黄河水电西宁太阳能电力有限公司 | Nondestructive splitting method for reducing efficiency loss of solar cell |
| JP7784018B1 (en) * | 2024-10-10 | 2025-12-10 | 鄂爾多斯市隆基光伏科技有限公司 | Solar cells and solar modules |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006035710A (en) * | 2004-07-28 | 2006-02-09 | Cyber Laser Kk | Laser glass processing method and apparatus |
| CN105436712A (en) * | 2015-12-07 | 2016-03-30 | 武汉铱科赛科技有限公司 | Brittle slivering method and system for brittle semiconductor material |
| CN105895745A (en) * | 2016-06-21 | 2016-08-24 | 苏州协鑫集成科技工业应用研究院有限公司 | Method for cutting heterojunction solar cell |
| TW201903870A (en) * | 2017-06-01 | 2019-01-16 | 鈦昇科技股份有限公司 | Wafer cutting method eliminating cracks generated during grinding and stress of the wafer, ensuring that the wafer does not crack due to the stress and guaranteeing the quality of the wafer, and increasing the yield of the chips |
| JP2020021968A (en) * | 2015-06-01 | 2020-02-06 | エバナ テクノロジーズ ユーエービー | Scribing method for semiconductor processing object |
| JP2020031135A (en) * | 2018-08-22 | 2020-02-27 | 株式会社ディスコ | Silicon wafer processing method and plasma etching system |
-
2020
- 2020-07-24 CN CN202010723818.1A patent/CN111834211B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006035710A (en) * | 2004-07-28 | 2006-02-09 | Cyber Laser Kk | Laser glass processing method and apparatus |
| JP2020021968A (en) * | 2015-06-01 | 2020-02-06 | エバナ テクノロジーズ ユーエービー | Scribing method for semiconductor processing object |
| CN105436712A (en) * | 2015-12-07 | 2016-03-30 | 武汉铱科赛科技有限公司 | Brittle slivering method and system for brittle semiconductor material |
| CN105895745A (en) * | 2016-06-21 | 2016-08-24 | 苏州协鑫集成科技工业应用研究院有限公司 | Method for cutting heterojunction solar cell |
| TW201903870A (en) * | 2017-06-01 | 2019-01-16 | 鈦昇科技股份有限公司 | Wafer cutting method eliminating cracks generated during grinding and stress of the wafer, ensuring that the wafer does not crack due to the stress and guaranteeing the quality of the wafer, and increasing the yield of the chips |
| JP2020031135A (en) * | 2018-08-22 | 2020-02-27 | 株式会社ディスコ | Silicon wafer processing method and plasma etching system |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112599637A (en) * | 2020-12-09 | 2021-04-02 | 成都晔凡科技有限公司 | Method for manufacturing solar cell piece and solar cell piece |
| CN112599637B (en) * | 2020-12-09 | 2022-05-31 | 成都晔凡科技有限公司 | Method for manufacturing solar cell piece and solar cell piece |
| CN115117193A (en) * | 2021-03-19 | 2022-09-27 | 黄河水电西宁太阳能电力有限公司 | Nondestructive splitting method for reducing efficiency loss of solar cell |
| CN113555472A (en) * | 2021-07-16 | 2021-10-26 | 安徽华晟新能源科技有限公司 | Heterojunction cell processing method, sliced heterojunction cell and heterojunction cell assembly |
| CN113555472B (en) * | 2021-07-16 | 2023-12-29 | 安徽华晟新能源科技有限公司 | Heterojunction battery processing method, sliced heterojunction battery and heterojunction battery assembly |
| CN114823317A (en) * | 2022-03-29 | 2022-07-29 | 通威太阳能(安徽)有限公司 | Silicon wafer cutting method and battery |
| CN114823317B (en) * | 2022-03-29 | 2024-07-19 | 通威太阳能(安徽)有限公司 | Silicon wafer cutting method and battery |
| JP7784018B1 (en) * | 2024-10-10 | 2025-12-10 | 鄂爾多斯市隆基光伏科技有限公司 | Solar cells and solar modules |
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