CN103779430A - Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell - Google Patents
Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell Download PDFInfo
- Publication number
- CN103779430A CN103779430A CN201210416053.2A CN201210416053A CN103779430A CN 103779430 A CN103779430 A CN 103779430A CN 201210416053 A CN201210416053 A CN 201210416053A CN 103779430 A CN103779430 A CN 103779430A
- Authority
- CN
- China
- Prior art keywords
- layer
- conductive
- solar cell
- silicon solar
- crystalline silicon
- Prior art date
- Legal status (The legal status 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 status listed.)
- Pending
Links
- 229910021419 crystalline silicon Inorganic materials 0.000 title abstract description 42
- 239000010410 layer Substances 0.000 claims abstract description 128
- 238000002161 passivation Methods 0.000 claims abstract description 70
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 64
- 239000010703 silicon Substances 0.000 claims abstract description 64
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 58
- 239000000758 substrate Substances 0.000 claims abstract description 38
- 239000002346 layers by function Substances 0.000 claims abstract description 17
- 229910006404 SnO 2 Inorganic materials 0.000 claims abstract description 8
- 238000000034 method Methods 0.000 claims description 20
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 17
- 230000003647 oxidation Effects 0.000 claims description 15
- 238000007254 oxidation reaction Methods 0.000 claims description 15
- 238000000151 deposition Methods 0.000 claims description 13
- 230000008021 deposition Effects 0.000 claims description 12
- 238000001755 magnetron sputter deposition Methods 0.000 claims description 11
- 238000002360 preparation method Methods 0.000 claims description 7
- 238000005229 chemical vapour deposition Methods 0.000 claims description 5
- 238000004549 pulsed laser deposition Methods 0.000 claims description 3
- 238000000623 plasma-assisted chemical vapour deposition Methods 0.000 claims 2
- 230000001588 bifunctional effect Effects 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000003980 solgel method Methods 0.000 claims 1
- 238000006243 chemical reaction Methods 0.000 abstract description 9
- 239000000969 carrier Substances 0.000 abstract description 8
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 238000011049 filling Methods 0.000 abstract description 3
- 230000006798 recombination Effects 0.000 abstract description 3
- 238000005215 recombination Methods 0.000 abstract description 3
- 239000010408 film Substances 0.000 description 62
- 210000004027 cell Anatomy 0.000 description 47
- 238000004544 sputter deposition Methods 0.000 description 34
- 235000012431 wafers Nutrition 0.000 description 25
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 22
- XOLBLPGZBRYERU-UHFFFAOYSA-N tin dioxide Chemical compound O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 description 18
- 229910052581 Si3N4 Inorganic materials 0.000 description 16
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 16
- 230000000694 effects Effects 0.000 description 14
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 12
- 239000004408 titanium dioxide Substances 0.000 description 11
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 10
- 239000007789 gas Substances 0.000 description 8
- 238000012360 testing method Methods 0.000 description 8
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 7
- 239000001301 oxygen Substances 0.000 description 7
- 229910052760 oxygen Inorganic materials 0.000 description 7
- 230000008569 process Effects 0.000 description 7
- 230000000052 comparative effect Effects 0.000 description 6
- 239000002003 electrode paste Substances 0.000 description 6
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 6
- 235000012239 silicon dioxide Nutrition 0.000 description 6
- 239000000377 silicon dioxide Substances 0.000 description 6
- 239000002344 surface layer Substances 0.000 description 6
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 5
- 229910052786 argon Inorganic materials 0.000 description 5
- 238000011068 loading method Methods 0.000 description 5
- 229920005591 polysilicon Polymers 0.000 description 5
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000002310 reflectometry Methods 0.000 description 4
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 3
- 229910007570 Zn-Al Inorganic materials 0.000 description 3
- 238000001035 drying Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910000077 silane Inorganic materials 0.000 description 3
- 239000002356 single layer Substances 0.000 description 3
- 239000013077 target material Substances 0.000 description 3
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- 229910010413 TiO 2 Inorganic materials 0.000 description 2
- 229910021529 ammonia Inorganic materials 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000010894 electron beam technology Methods 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- -1 hydrogen ions Chemical class 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 229910003437 indium oxide Inorganic materials 0.000 description 2
- PJXISJQVUVHSOJ-UHFFFAOYSA-N indium(iii) oxide Chemical compound [O-2].[O-2].[O-2].[In+3].[In+3] PJXISJQVUVHSOJ-UHFFFAOYSA-N 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000006213 oxygenation reaction Methods 0.000 description 2
- 238000007639 printing Methods 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 229910001887 tin oxide Inorganic materials 0.000 description 2
- 239000011787 zinc oxide Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 210000005056 cell body Anatomy 0.000 description 1
- 229910052681 coesite Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 229910052906 cristobalite Inorganic materials 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000005527 interface trap Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000000615 nonconductor Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 125000004430 oxygen atom Chemical group O* 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000012495 reaction gas Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000007650 screen-printing Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 229910052682 stishovite Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 229910052905 tridymite Inorganic materials 0.000 description 1
- 238000007738 vacuum evaporation Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/30—Coatings
- H10F77/306—Coatings for devices having potential barriers
- H10F77/311—Coatings for devices having potential barriers for photovoltaic cells
- H10F77/315—Coatings for devices having potential barriers for photovoltaic cells the coatings being antireflective or having enhancing optical properties
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F71/00—Manufacture or treatment of devices covered by this subclass
- H10F71/121—The active layers comprising only Group IV materials
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/20—Electrodes
- H10F77/206—Electrodes for devices having potential barriers
- H10F77/211—Electrodes for devices having potential barriers for photovoltaic cells
- H10F77/219—Arrangements for electrodes of back-contact photovoltaic cells
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/20—Electrodes
- H10F77/244—Electrodes made of transparent conductive layers, e.g. transparent conductive oxide [TCO] layers
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/20—Electrodes
- H10F77/244—Electrodes made of transparent conductive layers, e.g. transparent conductive oxide [TCO] layers
- H10F77/247—Electrodes made of transparent conductive layers, e.g. transparent conductive oxide [TCO] layers comprising indium tin oxide [ITO]
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/547—Monocrystalline silicon PV cells
Landscapes
- Photovoltaic Devices (AREA)
Abstract
本发明提供一种晶体硅太阳电池的导电减反射膜,所述导电减反射膜为双功能层结构,靠近晶体硅太阳电池硅衬底的功能层为钝化层,远离晶体硅太阳电池硅衬底的功能层为导电层;导电层所采用的导电介质选自AZO、ITO、ATO、SnO2中的至少一种。本发明还提供了一种采用该导电减反射膜的晶体硅太阳电池。本发明提供的导电减反射膜,对硅表面进行良好钝化,还能有效收集PN结产生的光生载流子、使其复合被抑制,光利用率大;同时导电层还可以将电池向光面电极的栅线有效连接,使电极电阻分布均匀,电池的串联电阻变小,填充因子显著增加,提高电池的光电转化效率。另外,本发明提供的晶体硅太阳电池的制造工艺简单,适合大规模商业化生产。
The invention provides a conductive anti-reflection film for a crystalline silicon solar cell, the conductive anti-reflection film has a double-functional layer structure, the functional layer close to the silicon substrate of the crystalline silicon solar cell is a passivation layer, and is far away from the silicon lining of the crystalline silicon solar cell The bottom functional layer is a conductive layer; the conductive medium used in the conductive layer is selected from at least one of AZO, ITO, ATO, and SnO 2 . The invention also provides a crystalline silicon solar cell using the conductive anti-reflection film. The conductive anti-reflection film provided by the invention can passivate the silicon surface well, and can also effectively collect the photogenerated carriers generated by the PN junction, so that their recombination is suppressed, and the light utilization rate is large; at the same time, the conductive layer can also direct the battery to the light. The grid lines of the surface electrodes are effectively connected, so that the electrode resistance is evenly distributed, the series resistance of the battery is reduced, the filling factor is significantly increased, and the photoelectric conversion efficiency of the battery is improved. In addition, the manufacturing process of the crystalline silicon solar cell provided by the invention is simple and suitable for large-scale commercial production.
Description
技术领域 technical field
本发明涉及太阳能电池领域,更具体地说,本发明涉及一种晶体硅太阳电池的导电减反射膜以及包含该导电减反射膜的晶体硅太阳电池。 The invention relates to the field of solar cells, more specifically, the invention relates to a conductive anti-reflection film of a crystalline silicon solar cell and a crystalline silicon solar cell comprising the conductive anti-reflection film.
背景技术 Background technique
太阳能作为一种绿色能源,以其取之不竭、无污染、不受地域资源限制等优点越来越受到人们的重视。为了提高晶体硅太阳能电池的光电转换效率,减少电池表面的光反射损失,增加光透射,太阳电池结构中的减反射膜起着非常重要的作用。 As a kind of green energy, solar energy has attracted more and more attention due to its advantages of inexhaustibility, no pollution, and no limitation of geographical resources. In order to improve the photoelectric conversion efficiency of crystalline silicon solar cells, reduce the light reflection loss on the surface of the cell, and increase light transmission, the antireflection film in the solar cell structure plays a very important role.
目前已经大规模产业化的工艺是采用等离子化学气相沉积法(PECVD)在扩散完成后的硅片上沉积一层合适厚度的氮化硅薄膜,该氮化硅薄膜层在具有减反射效果的同时,还具有一定的钝化效果。在通过PECVD沉积氮化硅薄膜的过程中,反应气体氨气与硅烷气体离子化后 ,其中的氢离子与硅表面的悬挂键结合,形成表面钝化效果,从而可以有效抑制光生载流子的复合,提高电池的光电转换效率。然而,单层氮化硅薄膜的减反射率还不是很低,仍然存在改善的空间。 At present, the process that has been industrialized on a large scale is to deposit a layer of silicon nitride film with a suitable thickness on the silicon wafer after diffusion by plasma chemical vapor deposition (PECVD). The silicon nitride film layer has anti-reflection effect while , also has a certain passivation effect. In the process of depositing silicon nitride film by PECVD, after the reaction gas ammonia gas and silane gas are ionized, the hydrogen ions in it combine with the dangling bonds on the silicon surface to form a surface passivation effect, which can effectively suppress the photogenerated carriers. Composite, improve the photoelectric conversion efficiency of the battery. However, the anti-reflectivity of a single-layer silicon nitride film is not very low, and there is still room for improvement.
因此,如何进一步增加入射光的利用率,提高电池的光电效率,是目前电池研究的一个热点。CN201120218873公开了一种晶体硅太阳能电池双层减反射膜,其是由二氧化钛薄膜和氮化硅薄膜钝化层组成,氮化硅薄膜位于二氧化钛薄膜和硅片之间;该双层减反射膜可以降低电池表面对光的反射,在光谱范围300~1200nm之间的反射率与未涂敷相比降低10%左右。该方法中仅通过双层结构的反射膜来降低入射光的反射率,降低光反射的效果提升非常有限,采用该双层结构减反射膜的太阳电池的光电转化效率仍较低。 Therefore, how to further increase the utilization rate of incident light and improve the photoelectric efficiency of the battery is a hot spot in battery research at present. CN201120218873 discloses a double-layer anti-reflection film for crystalline silicon solar cells, which is composed of a titanium dioxide film and a silicon nitride film passivation layer, and the silicon nitride film is located between the titanium dioxide film and the silicon wafer; the double-layer anti-reflection film can be Reduce the reflection of light on the surface of the battery, and the reflectance between 300 and 1200nm in the spectral range is reduced by about 10% compared with that without coating. In this method, the reflectivity of incident light is only reduced by using a double-layer structure reflective film, and the effect of reducing light reflection is very limited. The photoelectric conversion efficiency of the solar cell using the double-layer structure anti-reflection film is still low.
CN201859880U提供了一种具有导电减反射膜的太阳电池,它包括在太阳电池本体的上表面设有钝化层,在钝化层的表面蒸镀有一条主电极,然后在主电极周围蒸镀导电减反射膜;导电减反射膜由底层(TiO2)和表层(SiO2或Al2O3)组成。该电池期望通过导电减反射膜代替太阳电池向光面的栅电极,即导电减反射膜还用于收集电流,从而增加电池的受光面积。但由于该导电减反射膜覆盖在钝化层之上,钝化膜通常为不导电体,因此实际上该导电减反射膜根本不能收集到光生电流。而且由该类氧化物组成的导电减反射膜的导电效果也并不好。 CN201859880U provides a solar cell with a conductive anti-reflection film, which includes a passivation layer on the upper surface of the solar cell body, a main electrode is evaporated on the surface of the passivation layer, and then a conductive electrode is evaporated around the main electrode. Anti-reflection coating; conductive anti-reflection coating consists of bottom layer (TiO 2 ) and surface layer (SiO 2 or Al 2 O 3 ). The battery is expected to replace the grid electrode on the light-facing side of the solar cell with a conductive anti-reflection film, that is, the conductive anti-reflection film is also used to collect current, thereby increasing the light-receiving area of the battery. However, since the conductive anti-reflection film is covered on the passivation layer, the passivation film is usually a non-conductor, so in fact the conductive anti-reflection film cannot collect photo-generated current at all. Moreover, the conductive effect of the conductive anti-reflection film composed of such oxides is not good.
发明内容 Contents of the invention
本发明针对现有技术中晶体硅太阳电池存在的减反射膜对入射光的反射率降低程度有限、导致电池的光电转化效率仍较低的技术问题,提供一种具有新型结构的晶体硅太阳电池的导电减反射膜和采用该导电减反射膜的晶体硅太阳电池。 The present invention aims at the technical problem that the anti-reflection film existing in the crystalline silicon solar cell has a limited reduction in the reflectivity of the incident light, resulting in a low photoelectric conversion efficiency of the cell, and provides a crystalline silicon solar cell with a new structure The conductive anti-reflection film and the crystalline silicon solar cell using the conductive anti-reflection film.
具体地,本发明的技术方案为: Specifically, the technical solution of the present invention is:
一种晶体硅太阳电池的导电减反射膜,所述导电减反射膜为双功能层结构,其中靠近晶体硅太阳电池硅衬底的功能层为钝化层,远离晶体硅太阳电池硅衬底的功能层为导电层;所述导电层所采用的导电介质选自AZO(掺铝的氧化锌)、ITO(掺锡的氧化铟)、ATO(掺锑的氧化锡)或者SnO2(二氧化锡)中的至少一种。 A conductive anti-reflection film for a crystalline silicon solar cell, the conductive anti-reflection film is a double-functional layer structure, wherein the functional layer close to the silicon substrate of the crystalline silicon solar cell is a passivation layer, and the functional layer far away from the silicon substrate of the crystalline silicon solar cell is a passivation layer. The functional layer is a conductive layer; the conductive medium used in the conductive layer is selected from AZO (aluminum-doped zinc oxide), ITO (tin-doped indium oxide), ATO (antimony-doped tin oxide) or SnO 2 (tin dioxide ) at least one of the
一种晶体硅太阳电池,所述晶体硅太阳电池包括硅衬底、位于硅衬底向光面的减反射层、位于减反射层表面且穿过减反射层与硅衬底接触的向光面电极;所述减反射层为本发明提供的导电减反射膜。 A crystalline silicon solar cell comprising a silicon substrate, an anti-reflection layer located on the light-facing surface of the silicon substrate, and a light-facing surface located on the surface of the anti-reflection layer and in contact with the silicon substrate through the anti-reflection layer Electrodes; the anti-reflection layer is the conductive anti-reflection film provided by the present invention.
本发明提供的晶体硅太阳电池的导电减反射膜,为双功能层结构,导电层和钝化层均具有对入射光的减反射作用,该双层减反射膜一方面能对硅表面进行良好钝化,还能有效收集PN结产生的光生载流子、使光生载流子的复合被抑制,光利用率大;同时导电层还可以将电池向光面电极的细栅线有效连接,使电极电阻分布均匀,采用该导电减反射膜的晶体硅太阳电池的串联电阻变小,填充因子显著增加,从而使电池的光电转化效率得到明显提高。另外,本发明提供的晶体硅太阳电池的制造工艺简单,额外增加的成本小,适合大规模商业化生产。 The conductive anti-reflection film of the crystalline silicon solar cell provided by the present invention has a double-functional layer structure, and both the conductive layer and the passivation layer have an anti-reflection effect on incident light. Passivation can also effectively collect the photo-generated carriers generated by the PN junction, inhibit the recombination of photo-generated carriers, and increase the light utilization rate; at the same time, the conductive layer can also effectively connect the battery to the thin grid line of the photo-surface electrode, so that The electrode resistance is evenly distributed, the series resistance of the crystalline silicon solar cell adopting the conductive anti-reflection film is reduced, and the filling factor is significantly increased, so that the photoelectric conversion efficiency of the cell is significantly improved. In addition, the manufacturing process of the crystalline silicon solar cell provided by the invention is simple, the additional cost is small, and it is suitable for large-scale commercial production.
附图说明 Description of drawings
图1是本发明提供的晶体硅太阳电池的结构示意图。 Fig. 1 is a schematic structural diagram of a crystalline silicon solar cell provided by the present invention.
图中: 1——导电层,2——钝化层,3——向光面电极,4——硅衬底,5——背场,6——背面电极。 In the figure: 1—conductive layer, 2—passivation layer, 3—light-facing electrode, 4—silicon substrate, 5—back field, 6—back electrode. the
具体实施方式 Detailed ways
本发明提供了一种晶体硅太阳电池的导电减反射膜,所述导电减反射膜为双功能层结构,其中靠近晶体硅太阳电池硅衬底的功能层为钝化层,远离晶体硅太阳电池硅衬底的功能层为导电层;所述导电层所采用的导电介质选自AZO、ITO、ATO或者SnO2中的至少一种。 The invention provides a conductive anti-reflection film for a crystalline silicon solar cell, the conductive anti-reflection film is a double-functional layer structure, wherein the functional layer close to the silicon substrate of the crystalline silicon solar cell is a passivation layer, and is far away from the crystalline silicon solar cell The functional layer of the silicon substrate is a conductive layer; the conductive medium used in the conductive layer is selected from at least one of AZO, ITO, ATO or SnO 2 .
虽然CN201120218873公开了一种晶体硅太阳能电池双层减反射膜,其二氧化钛层和氮化硅薄膜层均用于降低将射光的反射,即其仅通过双层膜进一步降低反射,而未对各层减反射膜性能本质上进行改善;而CN201859880U提供的导电膜(SiO2或Al2O3)覆盖在钝化层(TiO2)之上,导电膜并未和硅片接触,而该钝化膜作为不良导体。该发明的电池无细栅线,实际上,单纯的主栅线并不能有效收集光生载流子,因此,电池的效率提升有限。 Although CN201120218873 discloses a double-layer anti-reflection film for crystalline silicon solar cells, its titanium dioxide layer and silicon nitride film layer are used to reduce the reflection of the incident light, that is, it only further reduces the reflection through the double-layer film, and does not affect each layer. The performance of the anti-reflection film is essentially improved; while the conductive film (SiO 2 or Al 2 O 3 ) provided by CN201859880U is covered on the passivation layer (TiO 2 ), the conductive film is not in contact with the silicon wafer, and the passivation film as a poor conductor. The battery of this invention has no thin grid lines. In fact, the simple main grid lines cannot effectively collect photo-generated carriers, so the efficiency of the battery is limited.
本发明提供的晶体硅太阳电池的导电减反射膜,其结构为双功能层结构,靠近硅衬底的功能层(记为底层)为钝化层;远离硅衬底的功能层(记为表层)为导电层。导电层和钝化层均具有对入射光具有减反射作用,该双层减反射膜一方面能对硅表面进行良好钝化,减少或者抑制光生载流子在硅片表面的复合,还能更有效地收集PN结产生的光生载流子、使载流子的收集几率增加,因此光利用率增大大;同时,减反射膜中的导电层(表层)还可以将电池向光面电极的细栅线有效连接起来,将光生电流收集并向主栅汇集,使电极电阻分布均匀,串联电阻变小,填充因子显著增加,从而使电池的光电转化效率得到明显提高。 The conductive anti-reflection film of the crystalline silicon solar cell provided by the present invention has a double-functional layer structure, and the functional layer close to the silicon substrate (referred to as the bottom layer) is a passivation layer; the functional layer far away from the silicon substrate (referred to as the surface layer) ) is the conductive layer. Both the conductive layer and the passivation layer have an anti-reflection effect on incident light. On the one hand, the double-layer anti-reflection film can passivate the silicon surface well, reduce or inhibit the recombination of photogenerated carriers on the surface of the silicon wafer, and can also be more Effectively collect the photo-generated carriers generated by the PN junction and increase the probability of carrier collection, so the light utilization rate increases greatly; at the same time, the conductive layer (surface layer) in the anti-reflection film can also transfer the battery to the thin surface of the light electrode. The gate lines are effectively connected to collect the photo-generated current and gather it to the main grid, so that the electrode resistance is evenly distributed, the series resistance is reduced, and the filling factor is significantly increased, so that the photoelectric conversion efficiency of the battery is significantly improved.
采用该导电减反射膜的太阳电池,表层(即导电层)用于接受光照层。本发明对表层中采用的导电介质的材质,通过大量实验进行选择,最后发现,采用AZO(掺铝的氧化锌)、ITO(掺锡的氧化铟)、ATO(掺锑的氧化锡)或者SnO2(二氧化锡)中的至少一种作为导电介质时,该类物质形成的导电层对入射光的反射很少,同时其具有良好的导电性。 In the solar cell using the conductive anti-reflection film, the surface layer (that is, the conductive layer) is used to receive light. The present invention selects the material of the conductive medium used in the surface layer through a large number of experiments, and finally finds that AZO (aluminum-doped zinc oxide), ITO (tin-doped indium oxide), ATO (antimony-doped tin oxide) or SnO When at least one of 2 (tin dioxide) is used as a conductive medium, the conductive layer formed by this type of material has little reflection of incident light, and it has good conductivity.
本发明中,所述导电层的厚度可根据底层(即钝化层)材质的种类及厚度进行适当选择,其选择原则是保证钝化层叠加上导电层所组成的双功能层,导电减反射膜对入射光的反射率最小。此外,导电层(表层)也可以采用两种或两种以上的导电介质,如采用AZO与SnO2两种组合作为导电层,即先制备一层AZO,再在AZO上制备一层SnO2,一般情况下,采用两种导电介质组合形成的导电层的减反射效果要比单层的要好,但其制备工艺复杂,成本会大幅度增加,因此,优选采用单一导电介质层。 In the present invention, the thickness of the conductive layer can be properly selected according to the type and thickness of the material of the bottom layer (i.e. the passivation layer). The reflectivity of the film to incident light is minimal. In addition, the conductive layer (surface layer) can also use two or more conductive media, such as using a combination of AZO and SnO 2 as the conductive layer, that is, first prepare a layer of AZO, and then prepare a layer of SnO 2 on the AZO, Generally speaking, the anti-reflection effect of the conductive layer formed by the combination of two conductive media is better than that of a single layer, but its preparation process is complicated and the cost will increase greatly. Therefore, it is preferable to use a single conductive media layer.
因此,本发明中,优选情况下所述导电层可直接采用单层AZO。发明人发现,形成AZO导电膜层的原材料来源相对丰富,其对环境污染小,膜的导电性能更佳,和钝化层的光学性能匹配性好,且该膜的制备工艺简单、成熟。 Therefore, in the present invention, preferably, the conductive layer can directly use single-layer AZO. The inventors found that the source of raw materials for forming the AZO conductive film layer is relatively abundant, it has less environmental pollution, the film has better electrical conductivity, and the optical performance of the passivation layer is well matched, and the preparation process of the film is simple and mature.
本发明导电减反射膜中导电层的厚度为20~80nm,其具体厚度可根据导电介质的种类以及钝化层介质种类和厚度而定,其设计原则是使整个减反射膜的光反射率最小,并且导电层的导电率则尽可能大。 The thickness of the conductive layer in the conductive antireflection film of the present invention is 20 ~ 80nm, and its specific thickness can be determined according to the type of the conductive medium and the medium type and thickness of the passivation layer. The design principle is to minimize the light reflectance of the entire antireflection film , and the conductivity of the conductive layer is as large as possible.
所述导电层的制备方法可采用现有技术中常用的磁控溅射法、脉冲激光沉积(PLD)法、溶胶-凝胶(Sol-Gel)法或化学气相沉积(CVD)法。优选采用磁控溅射法,因为该方法沉积速率高,基片温度低,成膜粘附性好,成本低,容易控制。磁控溅射的靶材为相应所镀物质的合金或者纯氧化物,靶材在磁控溅射形成导电氧化物的具体工艺为薄膜制备人员所公知。例如,以沉积AZO导电层为例,磁控溅射时的靶材可采用Zn-Al金属靶,采用氧气氧化,并通入氩气稀释,控制溅射压强为0.5~1.0Pa,氩气流量为10~30sccm,硅衬底温度为200~300℃,溅射时间可根据所需要沉积到硅片上的AZO膜的高度而定。 The preparation method of the conductive layer may adopt magnetron sputtering method, pulsed laser deposition (PLD) method, sol-gel (Sol-Gel) method or chemical vapor deposition (CVD) method commonly used in the prior art. The magnetron sputtering method is preferred, because this method has high deposition rate, low substrate temperature, good film adhesion, low cost and easy control. The target material of magnetron sputtering is an alloy or pure oxide corresponding to the substance to be plated, and the specific process of forming a conductive oxide on the target material by magnetron sputtering is well known to thin film preparation personnel. For example, taking the deposition of AZO conductive layer as an example, the target material during magnetron sputtering can be a Zn-Al metal target, oxidized with oxygen, diluted with argon gas, and the sputtering pressure is controlled at 0.5~1.0Pa, and the flow rate of argon gas The temperature of the silicon substrate is 200-300°C, and the sputtering time can be determined according to the height of the AZO film deposited on the silicon wafer.
本发明中,所述钝化层可采用现有技术中常用的钝化层。优选情况下,本发明中,所述钝化层所采用的钝化介质为SiO2或Si3N4。所述钝化层一方面能对硅衬底表面起到良好的钝化作用,同时也对入射光具有减反射作用。 In the present invention, the passivation layer may be a passivation layer commonly used in the prior art. Preferably, in the present invention, the passivation medium used in the passivation layer is SiO 2 or Si 3 N 4 . On the one hand, the passivation layer can have a good passivation effect on the surface of the silicon substrate, and at the same time, it can also have an anti-reflection effect on incident light.
具体地,本发明中,若钝化层采用SiO2作为钝化介质,其可通过热氧化或者真空蒸镀法制备形成。热氧化的方法工艺简单,设备成本少,因此优选采用热氧化工艺。在热氧化过程中,大量的氧原子和硅衬底表面未饱和的硅原子相结合形成一层SiO2膜,从而降低悬挂键的密度,能够很好地控制界面陷阱和固定电荷,降低表面态密度,起到表面钝化作用。具体地,对硅衬底表面钝化形成钝化层的步骤包括:将制绒、扩散、刻蚀、去磷硅玻璃后的硅片衬底放入氧气气氛中进行热氧化,在氧化阶段同时通入保护气体氮气,氧化温度设置为800~850℃,氧化时间则根据所需要得到的SiO2膜的厚度而定,一般控制在100~500s之间。 Specifically, in the present invention, if the passivation layer uses SiO 2 as the passivation medium, it can be formed by thermal oxidation or vacuum evaporation. The thermal oxidation method has simple process and low equipment cost, so thermal oxidation process is preferred. During the thermal oxidation process, a large number of oxygen atoms and unsaturated silicon atoms on the surface of the silicon substrate combine to form a layer of SiO2 film, thereby reducing the density of dangling bonds, which can well control the interface traps and fixed charges, and reduce the surface state Density acts as a surface passivator. Specifically, the step of passivating the surface of the silicon substrate to form a passivation layer includes: putting the silicon wafer substrate after texturing, diffusion, etching, and dephosphorous silicon glass into an oxygen atmosphere for thermal oxidation, and simultaneously during the oxidation stage The protective gas nitrogen is introduced, and the oxidation temperature is set at 800~850°C. The oxidation time is determined according to the thickness of the SiO 2 film to be obtained, and is generally controlled between 100~500s.
由于SiO2的钝化效果一般优于氮化硅,因此,本发明中,钝化层所采用的钝化介质优选为SiO2。并且,硅片衬底的热氧化可双面进行,即不需要保护硅片的背光面,背光面得到的二氧化硅同样具有钝化表面的效果,对抑制背表面的光生载流子同样有益。进一步地,本发明中,所述钝化层采用的钝化介质为SiO2时,钝化层的厚度为5~20nm。钝化层厚度太小会影响对硅片表面的钝化效果,太大则会增加形成钝化层的时间,高温导致硅片内的杂质重新分布而影响硅片的质量,从而导致电池的Voc和ISC流均有下降。 Since the passivation effect of SiO 2 is generally better than that of silicon nitride, in the present invention, the passivation medium used for the passivation layer is preferably SiO 2 . Moreover, the thermal oxidation of the silicon wafer substrate can be carried out on both sides, that is, there is no need to protect the backlight surface of the silicon wafer, and the silicon dioxide obtained on the backlight surface also has the effect of passivating the surface, which is also beneficial to suppress the photogenerated carriers on the back surface . Further, in the present invention, when the passivation medium used for the passivation layer is SiO 2 , the thickness of the passivation layer is 5-20 nm. If the thickness of the passivation layer is too small, it will affect the passivation effect on the surface of the silicon wafer. If the thickness of the passivation layer is too large, it will increase the time for forming the passivation layer. High temperature will cause the impurities in the silicon wafer to redistribute and affect the quality of the silicon wafer. Both oc and I SC flow decreased.
钝化层中采用的钝化介质也可为氮化硅。采用氮化硅作为钝化介质时,对应的钝化层的厚度为15~60 nm之间,这是因为氮化硅的钝化作用弱于SiO2,并且其沉积的温度低,因此其选择厚度可以大于SiO2。氮化硅的钝化机理为本领域人员所公知,此处不再赘述。形成氮化硅钝化层的制备方法可采用化学气相沉积(PECVD)法,其具体工艺为本领域技术人员所公知。 The passivation medium employed in the passivation layer may also be silicon nitride. When silicon nitride is used as the passivation medium, the thickness of the corresponding passivation layer is between 15 and 60 nm. This is because the passivation effect of silicon nitride is weaker than that of SiO 2 , and its deposition temperature is low, so its choice The thickness can be greater than SiO 2 . The passivation mechanism of silicon nitride is well known to those skilled in the art and will not be repeated here. The preparation method for forming the silicon nitride passivation layer can be a chemical vapor deposition (PECVD) method, and its specific process is well known to those skilled in the art.
本发明还提供了一种采用该导电减反射膜的晶体硅太阳电池,其结构如图1所示,具体包括硅衬底4、位于硅衬底4向光面的减反射层、位于减反射层表面且穿过减反射层与硅衬底接触的向光面电极3;所述减反射层为本发明提供的导电减反射膜,即包括导电层1和钝化层2,其中导电层1远离硅衬底4,而钝化层2靠近硅衬底4。 The present invention also provides a crystalline silicon solar cell using the conductive anti-reflection film, the structure of which is shown in Fig. The light-facing electrode 3 on the surface of the layer and in contact with the silicon substrate through the anti-reflection layer; the anti-reflection layer is the conductive anti-reflection film provided by the present invention, that is, it includes a conductive layer 1 and a passivation layer 2, wherein the conductive layer 1 away from the silicon substrate 4 , while the passivation layer 2 is close to the silicon substrate 4 .
作为本领域技术人员的公知常识,所述所述硅衬底4背面还设有背场5和背面电极6,背面电极6穿过背场5与硅衬底4背面接触,如图1所示。
As the common knowledge of those skilled in the art, the back side of the silicon substrate 4 is also provided with a
经测试,采用本发明提供的导电减反射膜制备得到的156×156多晶太阳电池的平均光电效率提高0.15%以上。另外,本发明提供的晶体硅太阳电池的制造工艺简单,额外增加的成本小,适合大规模商业化生产。 After testing, the average photoelectric efficiency of the 156×156 polycrystalline solar cells prepared by using the conductive anti-reflection film provided by the invention is increased by more than 0.15%. In addition, the manufacturing process of the crystalline silicon solar cell provided by the invention is simple, the additional cost is small, and it is suitable for large-scale commercial production.
为了使本发明所解决的技术问题、技术方案及有益效果更加清楚明白,以下结合实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不用于限定本发明。 In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
实施例1 Example 1
(1)将156×156 P型多晶硅制绒、扩散、刻蚀、去磷硅玻璃后得到的硅片放入氧气气氛中进行双面热氧化,氧化炉内的温度设置为820℃,氧化时间为312s,得到的SiO2钝化层的厚度为11.5±0.1nm(由美国Ambious Technology Inc公司生产的探针式台阶仪测量,下同)。 (1) Put the 156×156 P-type polysilicon textured, diffused, etched, and dephosphorized silicon wafers into silicon wafers for double-sided thermal oxidation in an oxygen atmosphere. The temperature in the oxidation furnace is set at 820°C, and the oxidation time is is 312s, and the thickness of the obtained SiO 2 passivation layer is 11.5±0.1nm (measured by a probe-type step meter produced by Ambious Technology Inc of the United States, the same below).
(2)将步骤(1)得到的硅片放在直流磁控溅射机的载片台上固定,然后将其放入溅射腔中,以预先固定在腔室内Zn-Al(Al含量为3wt%)金属靶材进行溅射,合上溅射腔室门,对腔室抽真空,设置溅射压强为0.6Pa,硅片衬底温度为250℃,氧气与氩气流量(以体积流量mL/min计量,下同)比为10:40,溅射功率为55W,溅射时间为1920s,得到AZO导电层,测试其厚度为67.5±0.1nm。 (2) Place the silicon wafer obtained in step (1) on the loading table of the DC magnetron sputtering machine, and then put it into the sputtering chamber to pre-fix Zn-Al in the chamber (the Al content is 3wt%) metal target for sputtering, close the sputtering chamber door, evacuate the chamber, set the sputtering pressure to 0.6Pa, the temperature of the silicon wafer substrate to 250°C, the flow rate of oxygen and argon (in terms of volume flow mL/min measurement, the same below) The ratio is 10:40, the sputtering power is 55W, and the sputtering time is 1920s, and the AZO conductive layer is obtained, and its thickness is 67.5±0.1nm. the
(3)将步骤(2)得到的硅片采用200目丝网印刷背面银导电浆料(型号为杜邦PV505,三线八段制,印刷湿重为35~50 mg),再采用280目丝网印刷背场铝浆料(型号为硕禾108C,印刷湿重为1.4~1.6g),烘干,烘干温度均为150℃,烘干时间为5分钟,然后采用360目、线宽为40μm、线径为16μm、膜厚为5μm的网版印刷正面银浆(型号为杜邦17A,印刷湿重为120~130mg),烧结后得到的本实施例的晶体硅太阳电池,记为S1。 (3) Use 200-mesh screen printing silver conductive paste on the back of the silicon wafer obtained in step (2) (model is DuPont PV505, three-line eight-stage system, printing wet weight is 35~50 mg), and then use 280-mesh screen Print back field aluminum paste (model is Shuohe 108C, printing wet weight is 1.4~1.6g), drying, drying temperature is 150°C, drying time is 5 minutes, and then use 360 mesh, line width is 40μm The crystalline silicon solar cell of this embodiment obtained after sintering the front side silver paste with a wire diameter of 16 μm and a film thickness of 5 μm (the model is DuPont 17A, and the printed wet weight is 120-130 mg) is denoted as S1.
实施例2 Example 2
采用与实施例1相同的步骤制备本实施例的晶体硅太阳电池S2,不同之处在于: The same steps as in Example 1 were used to prepare the crystalline silicon solar cell S2 of this example, except that:
步骤(1)中,氧化炉内的温度设置为850℃,氧化时间为480s,得到的SiO2钝化层的厚度为18.4±0.1nm; In step (1), the temperature in the oxidation furnace is set to 850°C, the oxidation time is 480s, and the thickness of the obtained SiO 2 passivation layer is 18.4±0.1nm;
步骤(2)中,溅射时间为1680 s,得到的AZO导电层的厚度为61.3±0.1nm。 In step (2), the sputtering time was 1680 s, and the thickness of the obtained AZO conductive layer was 61.3±0.1nm. the
通过上述步骤,得到本实施例的晶体硅太阳电池S2。 Through the above steps, the crystalline silicon solar cell S2 of this embodiment is obtained.
实施例3 Example 3
(1)将156×156 P型多晶硅制绒、扩散、刻蚀、去磷硅玻璃后得到的硅片放入PECVD炉中进行沉积,真空度压力为25Pa,沉积温度为440℃,氨气与硅烷气体的流量比为2786:214,沉积时的功率为2900W,沉积时间为253s,得到氮化硅钝化层,测试其厚度为45±0.1nm。 (1) Put the 156×156 P-type polysilicon textured, diffused, etched, and dephosphorized silicon wafers into a PECVD furnace for deposition. The vacuum pressure is 25 Pa, the deposition temperature is 440 ° C, ammonia and The flow ratio of silane gas is 2786:214, the power during deposition is 2900W, and the deposition time is 253s to obtain a silicon nitride passivation layer, and its thickness is 45±0.1nm. the
(2)采用与实施例1步骤(2)相同的步骤在钝化层表面沉积导电层,不同之处在于:溅射时间为1146s,得到的AZO导电层的厚度为40.7±0.1nm。 (2) A conductive layer was deposited on the surface of the passivation layer by the same steps as in step (2) of Example 1, except that the sputtering time was 1146s, and the thickness of the obtained AZO conductive layer was 40.7±0.1 nm. the
(3)采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本实施例的晶体硅太阳电池,记为S3。 (3) The electrode paste and the back field paste were printed in the same steps as in step (3) of Example 1, dried and sintered to obtain the crystalline silicon solar cell of this example, denoted as S3.
实施例4 Example 4
(1)采用与实施例1步骤(1)相同的步骤在硅衬底表面形成SiO2钝化层。 (1) A SiO 2 passivation layer is formed on the surface of the silicon substrate by the same steps as in step (1) of Embodiment 1.
(2)将步骤(1)得到的硅片放在直流磁控溅射机的载片台上固定,然后将其放入溅射腔中,以预先固定在腔室内In-Sn(Sn含量为5.0wt%)金属靶材进行溅射,合上溅射腔室门,对腔室抽真空,设置溅射压强为0.6Pa,衬底温度为250℃,氧气与氩气的流量比15:42,溅射功率为75W,溅射时间为2350s,得到ITO导电层,测试其厚度为72.4±0.1nm。 (2) Place the silicon wafer obtained in step (1) on the loading stage of the DC magnetron sputtering machine, and then put it into the sputtering chamber to pre-fix the In-Sn in the chamber (the Sn content is 5.0wt%) metal target for sputtering, close the sputtering chamber door, evacuate the chamber, set the sputtering pressure to 0.6Pa, the substrate temperature to 250°C, and the flow ratio of oxygen to argon to be 15:42 , the sputtering power was 75W, and the sputtering time was 2350s to obtain an ITO conductive layer, whose thickness was measured to be 72.4±0.1nm. the
(3)采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本实施例的晶体硅太阳电池,记为S4。 (3) The electrode paste and the back field paste were printed by the same steps as in step (3) of Example 1, dried and sintered to obtain the crystalline silicon solar cell of this example, denoted as S4.
实施例5 Example 5
(1)采用与实施例1步骤(1)相同的步骤在硅衬底表面形成SiO2钝化层。 (1) A SiO 2 passivation layer is formed on the surface of the silicon substrate by the same steps as in step (1) of Embodiment 1.
(2)将步骤(1)得到的硅片放在直流磁控溅射机的载片台上固定,然后将其放入溅射腔中,以预先固定在腔室内SnO2 氧化物靶材进行溅射,合上溅射腔室门,对腔室抽真空,设置溅射压强为0.4Pa,衬底温度为200℃,溅射功率为90W,溅射时间为1850s,得到SnO2导电层,测试SnO2导电层厚度为52.5±0.1nm。 (2) Place the silicon wafer obtained in step (1) on the loading stage of the DC magnetron sputtering machine, and then put it into the sputtering chamber to pre-fix the SnO2 oxide target in the chamber for further processing. Sputtering, close the sputtering chamber door, vacuumize the chamber, set the sputtering pressure to 0.4Pa, the substrate temperature to 200°C, the sputtering power to 90W, and the sputtering time to 1850s to obtain the SnO2 conductive layer, The thickness of the SnO2 conductive layer was tested to be 52.5±0.1nm.
(3)采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本实施例的晶体硅太阳电池,记为S5。 (3) The electrode paste and the back field paste were printed in the same steps as in step (3) of Example 1, dried and sintered to obtain the crystalline silicon solar cell of this example, denoted as S5.
实施例6 Example 6
(1)采用与实施例1步骤(1)相同的步骤在硅衬底表面形成SiO2钝化层。 (1) A SiO 2 passivation layer is formed on the surface of the silicon substrate by the same steps as in step (1) of Embodiment 1.
(2)将步骤(1)得到的硅片放在直流磁控溅射机的载片台上固定,然后将其放入溅射腔中,以预先固定在腔室内Zn-Al(Al含量为3wt%)金属靶材进行溅射,合上溅射腔室门,对腔室抽真空,设置溅射压强为0.6Pa,硅片衬底温度为250℃,氧气与氩气流量(以体积流量mL/min计量,下同)比为10:40,溅射功率为55W,溅射时间为1100s,得到AZO导电层,测试其厚度为32.4±0.1nm。 (2) Place the silicon wafer obtained in step (1) on the loading stage of the DC magnetron sputtering machine, and then put it into the sputtering chamber to pre-fix Zn-Al in the chamber (the Al content is 3wt%) metal target for sputtering, close the sputtering chamber door, evacuate the chamber, set the sputtering pressure to 0.6Pa, the temperature of the silicon wafer substrate to 250°C, the oxygen and argon gas flow rate (in terms of volumetric flow rate mL/min measurement, the same below) The ratio is 10:40, the sputtering power is 55W, and the sputtering time is 1100s to obtain an AZO conductive layer, and its thickness is 32.4±0.1nm. the
(3)将步骤(2)得到的具有AZO导电层的硅片重新放入溅射腔中,以预先固定在腔室内SnO2 氧化物靶材进行溅射,合上溅射腔室门,对腔室抽真空,设置溅射压强为0.4Pa,衬底温度为200℃,溅射功率为65W,溅射时间为950s,得到覆盖在AZO层上的SnO2导电层,测试SnO2导电层厚度为26.1±0.1nm。 (3) Put the silicon wafer with AZO conductive layer obtained in step (2) back into the sputtering chamber to sputter with the SnO2 oxide target fixed in the chamber in advance, close the door of the sputtering chamber, and The chamber is evacuated, the sputtering pressure is set to 0.4Pa, the substrate temperature is 200°C, the sputtering power is 65W, and the sputtering time is 950s to obtain a SnO2 conductive layer covering the AZO layer, and test the thickness of the SnO2 conductive layer It is 26.1±0.1nm.
本实施例得到的具有AZO和SnO2双导电介质的导电功能层的共同厚度为58.5±0.2nm。 The common thickness of the conductive functional layer with AZO and SnO 2 double conductive media obtained in this embodiment is 58.5±0.2nm.
(4)采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本实施例的晶体硅太阳电池,记为S6。 (4) The electrode paste and the back field paste were printed by the same steps as in step (3) of Example 1, dried and sintered to obtain the crystalline silicon solar cell of this example, denoted as S6.
对比例1 Comparative example 1
(1)将156×156 P型多晶硅制绒、扩散、刻蚀、去磷硅玻璃后得到的硅片放入PECVD炉中进行沉积,真空度压力为25Pa,沉积温度为440℃,氨气与硅烷气体的流量比为2786:214,沉积时的功率为2900W,沉积时间为450s,得到氮化硅减反射层,测试其厚度为76.8±0.1nm。 (1) Put the 156×156 P-type polysilicon textured, diffused, etched, and dephosphorized silicon wafers into a PECVD furnace for deposition. The vacuum pressure is 25 Pa, the deposition temperature is 440 ° C, ammonia and The flow ratio of silane gas was 2786:214, the power during deposition was 2900W, and the deposition time was 450s to obtain a silicon nitride anti-reflection layer with a thickness of 76.8±0.1nm. the
(3)采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本对比例的晶体硅太阳电池,记为DS1。 (3) The electrode paste and the back field paste were printed by the same steps as in step (3) of Example 1, dried and sintered to obtain the crystalline silicon solar cell of this comparative example, denoted as DS1.
对比例2 Comparative example 2
采用CN201120218873中具体实施方式公开的步骤在156×156 P型多晶硅片表面依次沉积厚度为45nm的氮化硅薄膜和厚度为42nm的二氧化钛薄膜,然后采用与实施例1步骤(3)相同的步骤印刷电极浆料和背场浆料,烘干烧结,得到本对比例的晶体硅太阳电池,记为DS2。 Using the steps disclosed in the specific implementation method in CN201120218873, a silicon nitride film with a thickness of 45nm and a titanium dioxide film with a thickness of 42nm were sequentially deposited on the surface of a 156×156 P-type polycrystalline silicon wafer, and then printed using the same steps as in step (3) of Example 1 The electrode paste and the back field paste were dried and sintered to obtain the crystalline silicon solar cell of this comparative example, denoted as DS2.
对比例3 Comparative example 3
将156×156 P型多晶硅制绒、扩散、刻蚀、去磷硅玻璃后得到的硅片放在直流磁控溅射机的载片台上固定,然后将其放入溅射腔中,在相应的坩埚内分别装满二氧化钛和二氧化硅,关上真空室门和放气阀,先抽低真空,然后抽高真空;选择二氧化钛的坩埚,打开扫描、枪灯丝、高压和束流,调节电子束流,调整光斑位置,使坩埚内二氧化钛充分熔融,调整光板位置使落在干过中心,调节电子束流使二氧化钛稳定蒸发,打开充氧阀,打开挡板进行蒸发二氧化钛;二氧化钛蒸发完毕后继续充氧,选择二氧化硅的坩埚,打开挡板继续蒸发,二氧化硅蒸发完毕后继续充氧,最后关闭充氧开放气阀对真空室充气,得到表明具有钝化层和导电减反射膜的硅片,取出后在导电减反射膜表面印刷一条主电极,背面印刷背场和背面电极,烘干烧结,得到本对比例的晶体硅太阳电池,记为DS3。 Place the 156×156 P-type polysilicon textured, diffused, etched, and phosphorus-silicate silicon wafers on the loading stage of the DC magnetron sputtering machine, and then put them into the sputtering chamber. The corresponding crucibles are filled with titanium dioxide and silicon dioxide respectively, close the vacuum chamber door and the air release valve, first draw a low vacuum, and then pump a high vacuum; select the crucible of titanium dioxide, turn on the scanning, gun filament, high voltage and beam current, and adjust the electron beam Adjust the position of the light spot to fully melt the titanium dioxide in the crucible, adjust the position of the light plate so that it falls on the center of the dry pass, adjust the electron beam current to make the titanium dioxide evaporate stably, open the oxygenation valve, open the baffle to evaporate the titanium dioxide; continue to charge the titanium dioxide after the evaporation of the titanium dioxide is completed Oxygen, choose the crucible of silicon dioxide, open the baffle and continue to evaporate, continue to oxygenate after the silicon dioxide is evaporated, finally close the oxygenation and open the gas valve to inflate the vacuum chamber, and obtain the silicon dioxide that has a passivation layer and a conductive anti-reflection film. After taking it out, print a main electrode on the surface of the conductive anti-reflection film, print the back field and the back electrode on the back, dry and sinter to obtain the crystalline silicon solar cell of this comparative example, which is denoted as DS3.
性能测试 Performance Testing
表面状况:采用3~5倍放大镜观察上述制备的晶体硅太阳电池S1-S6与DS1-DS3的减反射膜颜色是否均匀,有无明显色差,观察表面是否光滑等。若无明显色差、表面光滑则记为OK,否则记为NG。 Surface condition: Use a magnifying glass of 3 to 5 times to observe whether the color of the anti-reflection coating of the above-prepared crystalline silicon solar cells S1-S6 and DS1-DS3 is uniform, whether there is obvious color difference, and observe whether the surface is smooth, etc. If there is no obvious color difference and the surface is smooth, it is recorded as OK, otherwise it is recorded as NG.
串联电阻、填充因子与光电转化效率:采用单次闪光模拟测试仪器对上述制备的晶体硅太阳电池样品S1-S6与DS1-DS3进行测试。测试条件为标准测试条件(STC):光强:1000W/m2;光谱:AM1.5;温度:25℃。串联电阻的单位为mΩ。 Series resistance, fill factor and photoelectric conversion efficiency: The crystalline silicon solar cell samples S1-S6 and DS1-DS3 prepared above were tested with a single flash simulation test instrument. The test conditions are standard test conditions (STC): light intensity: 1000W/m 2 ; spectrum: AM1.5; temperature: 25°C. The unit of series resistance is mΩ.
测试结果如表1所示。 The test results are shown in Table 1. the
表1 Table 1
。 .
从上表1的测试结果比较可以看出,采用本发明提供的导电减反射膜制备得到的晶体硅太阳电池的向光面电极的体电阻分布均匀,电池的串联电阻变小,填充因子显著增加,电池光电转换效率得到了提升;经产线实验证明:156×156多晶硅电池的平均光电效率提高0.15%以上。 From the comparison of the test results in Table 1 above, it can be seen that the volume resistance distribution of the light-facing electrode of the crystalline silicon solar cell prepared by using the conductive anti-reflection film provided by the present invention is uniform, the series resistance of the battery becomes smaller, and the fill factor increases significantly. , The photoelectric conversion efficiency of the cell has been improved; the production line experiment proves that the average photoelectric efficiency of the 156×156 polysilicon cell has increased by more than 0.15%.
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本发明的保护范围之内。 The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present invention should be included in the protection of the present invention. within range.
Claims (12)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201210416053.2A CN103779430A (en) | 2012-10-26 | 2012-10-26 | Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201210416053.2A CN103779430A (en) | 2012-10-26 | 2012-10-26 | Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103779430A true CN103779430A (en) | 2014-05-07 |
Family
ID=50571473
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201210416053.2A Pending CN103779430A (en) | 2012-10-26 | 2012-10-26 | Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103779430A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104465889A (en) * | 2014-12-26 | 2015-03-25 | 浙江正泰太阳能科技有限公司 | Method for manufacturing crystalline silicon solar cells |
CN105355708A (en) * | 2015-10-14 | 2016-02-24 | 广东爱康太阳能科技有限公司 | Solar cell provided with Ag transparent thin film and preparation method for solar cell |
CN109037359A (en) * | 2014-11-28 | 2018-12-18 | Lg电子株式会社 | solar battery |
CN110473922A (en) * | 2019-09-11 | 2019-11-19 | 南京爱通智能科技有限公司 | A kind of crystalline silicon high-efficiency photovoltaic cell structure |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101170139A (en) * | 2006-10-26 | 2008-04-30 | 中美矽晶制品股份有限公司 | Solar cell and method for manufacturing same |
CN101305472A (en) * | 2005-11-08 | 2008-11-12 | Lg化学株式会社 | High-efficiency solar cell and its preparation method |
KR100976454B1 (en) * | 2008-03-04 | 2010-08-17 | 삼성에스디아이 주식회사 | Solar cell and manufacturing method thereof |
CN201859880U (en) * | 2010-11-02 | 2011-06-08 | 上海太阳能工程技术研究中心有限公司 | Solar cell with conductive anti-reflecting film |
CN102270675A (en) * | 2010-06-03 | 2011-12-07 | 锦州华昌光伏科技有限公司 | Solar cell |
-
2012
- 2012-10-26 CN CN201210416053.2A patent/CN103779430A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101305472A (en) * | 2005-11-08 | 2008-11-12 | Lg化学株式会社 | High-efficiency solar cell and its preparation method |
CN101170139A (en) * | 2006-10-26 | 2008-04-30 | 中美矽晶制品股份有限公司 | Solar cell and method for manufacturing same |
KR100976454B1 (en) * | 2008-03-04 | 2010-08-17 | 삼성에스디아이 주식회사 | Solar cell and manufacturing method thereof |
CN102270675A (en) * | 2010-06-03 | 2011-12-07 | 锦州华昌光伏科技有限公司 | Solar cell |
CN201859880U (en) * | 2010-11-02 | 2011-06-08 | 上海太阳能工程技术研究中心有限公司 | Solar cell with conductive anti-reflecting film |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109037359A (en) * | 2014-11-28 | 2018-12-18 | Lg电子株式会社 | solar battery |
US11133426B2 (en) | 2014-11-28 | 2021-09-28 | Lg Electronics Inc. | Solar cell and method for manufacturing the same |
US11239379B2 (en) | 2014-11-28 | 2022-02-01 | Lg Electronics Inc. | Solar cell and method for manufacturing the same |
CN109037359B (en) * | 2014-11-28 | 2022-06-03 | Lg电子株式会社 | Solar battery |
US11616153B2 (en) | 2014-11-28 | 2023-03-28 | Shangrao Jinko Solar Technology Development Co., Ltd | Solar cell and method for manufacturing the same |
CN104465889A (en) * | 2014-12-26 | 2015-03-25 | 浙江正泰太阳能科技有限公司 | Method for manufacturing crystalline silicon solar cells |
CN105355708A (en) * | 2015-10-14 | 2016-02-24 | 广东爱康太阳能科技有限公司 | Solar cell provided with Ag transparent thin film and preparation method for solar cell |
CN110473922A (en) * | 2019-09-11 | 2019-11-19 | 南京爱通智能科技有限公司 | A kind of crystalline silicon high-efficiency photovoltaic cell structure |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3651932B2 (en) | Back surface reflective layer for photovoltaic device, method for forming the same, photovoltaic device and method for manufacturing the same | |
CN102810572A (en) | Refractive index matching of thin film layers for photovoltaic devices and method of manufacturing the same | |
JPH07297421A (en) | Method for manufacturing thin film semiconductor solar cell | |
CN102482796A (en) | doped transparent conductive oxide | |
US8390122B2 (en) | Sputtering targets including excess cadmium for forming a cadmium stannate layer | |
CN110416328A (en) | A kind of HJT battery and preparation method thereof | |
CN201402813Y (en) | A thin-film solar cell with high photoelectric conversion efficiency | |
CN103779430A (en) | Conductive antireflection film of crystalline silicon solar cell and crystalline silicon solar cell | |
CN104362211A (en) | Heterojunction solar cell and manufacturing method thereof | |
CN102237418B (en) | The cadmium sulfide layer used based on the film photovoltaic device of cadmium telluride and manufacture method thereof | |
CN101705473B (en) | Physical vapor deposition equipment for use in study on light trapping structure of silicon thin-film battery | |
CN104409528B (en) | Electrode and application before the HAZO/AZO composite transparent conductions that a kind of wide spectrum characteristic improves | |
CN104576824B (en) | Novel method for slotting front grid line electrode of crystalline silicon solar battery and manufacturing method of solar battery | |
CN111403551A (en) | Preparation method of high-efficiency monocrystalline silicon PERC solar cell | |
CN207009459U (en) | The silicon based hetero-junction solar cell that a kind of tow sides can generate electricity | |
CN102312190A (en) | Sputter is used for the method based on the RTB film of the photovoltaic device of cadmium telluride | |
CN116487447A (en) | Heterojunction solar cells and methods of making the same | |
CN101724821B (en) | Magnetic control sputtering system capable of adjusting and controlling growth of light trapping structure film of silicon film battery | |
CN104966759B (en) | A kind of preparation method of clad metal electrode solar cell | |
CN109065648A (en) | A kind of solar battery and preparation method thereof | |
JPH0818084A (en) | Method and apparatus for manufacturing solar cell | |
CN208622756U (en) | A kind of solar battery | |
JP3437422B2 (en) | Method for forming indium oxide thin film, substrate for semiconductor device using the indium oxide thin film, and photovoltaic device | |
JPH08107225A (en) | Manufacture of thin film solar cell | |
JP2002222969A (en) | Laminated solar battery |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140507 |