JPS61108178A - Solar cell module - Google Patents
Solar cell moduleInfo
- Publication number
- JPS61108178A JPS61108178A JP59230956A JP23095684A JPS61108178A JP S61108178 A JPS61108178 A JP S61108178A JP 59230956 A JP59230956 A JP 59230956A JP 23095684 A JP23095684 A JP 23095684A JP S61108178 A JPS61108178 A JP S61108178A
- Authority
- JP
- Japan
- Prior art keywords
- solar cell
- cell element
- protection sheet
- adhered
- cell module
- 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
- 229920005989 resin Polymers 0.000 claims abstract description 6
- 239000011347 resin Substances 0.000 claims abstract description 6
- 239000011159 matrix material Substances 0.000 claims description 7
- 229910052751 metal Inorganic materials 0.000 abstract description 3
- 239000002184 metal Substances 0.000 abstract description 3
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 abstract 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 abstract 1
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 238000010276 construction Methods 0.000 abstract 1
- 229910052731 fluorine Inorganic materials 0.000 abstract 1
- 239000011737 fluorine Substances 0.000 abstract 1
- 229910000679 solder Inorganic materials 0.000 abstract 1
- 238000000034 method Methods 0.000 description 6
- 230000001681 protective effect Effects 0.000 description 4
- 239000011521 glass Substances 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- DQXBYHZEEUGOBF-UHFFFAOYSA-N but-3-enoic acid;ethene Chemical compound C=C.OC(=O)CC=C DQXBYHZEEUGOBF-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000005038 ethylene vinyl acetate Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 description 2
- 229920002037 poly(vinyl butyral) polymer Polymers 0.000 description 2
- 239000004925 Acrylic resin Substances 0.000 description 1
- 229920000178 Acrylic resin Polymers 0.000 description 1
- JBRZTFJDHDCESZ-UHFFFAOYSA-N AsGa Chemical compound [As]#[Ga] JBRZTFJDHDCESZ-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/02—Details
- H01L31/0216—Coatings
- H01L31/02161—Coatings for devices characterised by at least one potential jump barrier or surface barrier
- H01L31/02167—Coatings for devices characterised by at least one potential jump barrier or surface barrier for solar cells
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、複数の太陽電池素子を並べて形成した太陽電
池モジー−ルに関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a solar cell module formed by arranging a plurality of solar cell elements.
一般に、太陽電池モジー−ルは、所要の出力に適合する
ように複数個の太陽電池素子を直列、並列、あるいは直
並列に接続することによシマトリックスを形成し、該マ
トリックス全過酷な自然環境、例えば、風雨、降雪、降
雪、あるいは大きな温度変化等に耐えるように、透明な
樹脂、ガラスおよび枠8策等で保護した構造を有してい
る。In general, solar cell modules are constructed by connecting a plurality of solar cell elements in series, parallel, or series-parallel to meet the required output to form a matrix, and the matrix can be used in harsh natural environments. For example, it has a structure protected by transparent resin, glass, and a frame to withstand wind, rain, snowfall, large temperature changes, and the like.
従来の太陽電池モジー−ルは、上記構造に組上げられる
工程中、太陽電池基板の強度だけで同工程中に課せられ
る種々の力、あるいは衝撃に耐えなければならなかった
。したがって、複数個の太陽電池素子からなるマトリッ
クスの取扱いは細心の注意を要している。特に近年、太
陽電池素子の大口径化が進むにつれてマトリックスの取
扱いの注意に要する負担は増加しつつある。In the conventional solar cell module, during the process of assembling it into the above-mentioned structure, the strength of the solar cell substrate alone had to withstand various forces or impacts imposed during the process. Therefore, handling of a matrix consisting of a plurality of solar cell elements requires great care. Particularly in recent years, as solar cell elements have become larger in diameter, the burden of careful handling of the matrix has been increasing.
さらに、最近PVB(ポリビニルブチラール)シートあ
るいはEVA(エチレンビニルアセテート)シートに太
陽電池マトリ、クスをサンドイッチ状にはさみ込み、加
熱と加圧によシ該マトリックスを透明樹脂中へ封入する
方法が封着技術として一般的になっている。この方法に
おいては、加圧時の微妙な条件が太陽電池素子に偏った
力を加え、素子を破壊させる確率が高い。しかも、この
工程においては、−素子でも破壊すると、その−素子の
みを修理または取換えることができず、モジー−ル全体
が不良となシ経済的に大きな損失を招く。Furthermore, recently, a method has been developed in which solar cell matrices and plastics are sandwiched between PVB (polyvinyl butyral) sheets or EVA (ethylene vinyl acetate) sheets, and the matrices are encapsulated in transparent resin by heating and pressure. It has become a common technology. In this method, delicate conditions during pressurization apply biased force to the solar cell element, and there is a high probability that the element will be destroyed. Moreover, in this process, if even an element is destroyed, it is impossible to repair or replace only that element, and the entire module becomes defective, resulting in a large economic loss.
すなわち、第4図は従来の太陽電池モジュールの断面図
である。本図において、太陽電池素子1は素子接続リー
ド2を介して相互に電気的接続がなされ、透明樹脂3中
に封じられ、さらにガラス板5に接着された状態で金属
枠6にはめ込まれた構造となっている。なお、図中外部
リードは4により示されている。That is, FIG. 4 is a sectional view of a conventional solar cell module. In this figure, solar cell elements 1 are electrically connected to each other via element connection leads 2, sealed in transparent resin 3, and fitted into a metal frame 6 while being adhered to a glass plate 5. It becomes. Note that the external lead is indicated by 4 in the figure.
このような太陽電池素子1の機械的強度は基板そのもの
の強度で決まり、例えば、シリコン(Si )あるいは
砒化ガリウム(GaAs)のように比較的脆弱な場合が
多く、モジー−ル完成後の機械的歪みばかりでなく、モ
ジュール製作工程中での破損が生じ易い。The mechanical strength of such a solar cell element 1 is determined by the strength of the substrate itself. For example, silicon (Si) or gallium arsenide (GaAs) are often relatively fragile, and the mechanical strength of the solar cell element 1 after completion of the module is determined by the strength of the substrate itself. Not only distortion but also damage during the module manufacturing process is likely to occur.
上述のとおシ、従来においては、太陽電池マトリックス
をモジュールに組立途中で、マトリックスを構成する太
陽電池素子の破壊が頻発するという点に問題がある。As described above, in the conventional method, there is a problem in that the solar cell elements constituting the matrix frequently break during assembly of the solar cell matrix into a module.
上記問題点に対し、本発明では、各太陽電池素子の受光
面と反対側の面に保護板を貼付けておく。In order to solve the above problems, in the present invention, a protection plate is attached to the surface of each solar cell element opposite to the light-receiving surface.
つぎに本発明全実施例によシ説明する。 Next, all embodiments of the present invention will be explained.
第1図は本発明の一実施例の断面図である。第1図にお
いて、これを第4図の従来例と比べると、太陽電池素子
1の裏面には保護板7が貼り付は補強されている点が違
い、その他は同じ構造である。FIG. 1 is a sectional view of an embodiment of the present invention. Comparing this with the conventional example shown in FIG. 4 in FIG. 1, the structure is the same except that a protective plate 7 is attached to the back surface of the solar cell element 1 for reinforcement.
第2図は、第1図の太陽電池素子を取り出して示した裏
面図である。保護板7は接続リード2の部分を除いてほ
ぼ全面にわたシ貼付けられている状態を示す。FIG. 2 is a back view of the solar cell element shown in FIG. 1 taken out. The protection plate 7 is shown in a state where it is pasted over almost the entire surface except for the connection lead 2 portion.
第3図は、保護板8がメツシー状金呈している例を示す
。FIG. 3 shows an example in which the protection plate 8 has a mesh-like shape.
保護板7,8としては、金属板、アクリル樹脂または弗
素樹脂が用いられ、その貼付けは、半田付け、接着剤に
よる接着によりなされ、さらに、貼付けは接続リードに
よる接続前または接続後の何れでも行い得る。The protective plates 7 and 8 are made of metal plates, acrylic resin, or fluororesin, and are attached by soldering or adhesive bonding, and can be attached either before or after connection with connection leads. obtain.
本発明によれば、太陽電池素子が保護板により裏打補強
されているので、太陽電池モジュール組立工程中に割れ
たシすることはなくなり、製造歩留りおよび信頼性が向
上する。According to the present invention, since the solar cell element is lined and reinforced with a protective plate, cracking during the solar cell module assembly process is eliminated, and manufacturing yield and reliability are improved.
第1図は本発明の一実施例の断面図、第2図は第1図の
太陽電池素子の裏面図、第3図はメツシー保護板を貼付
けた太陽電池素子の裏面図、第4図は従来の太陽電池モ
ジュールの断面図である。
1・・・・・・太陽電池素子、2・・・・・・接続リー
ド、3・・・・・・封止樹脂、4・・・・・・引出しリ
ード、5・・・・・・ガラス板、6・・・・・・全縮フ
レーム、7.8・・・・・・保護板。
第7図
め/ フ
第3図Fig. 1 is a sectional view of an embodiment of the present invention, Fig. 2 is a back view of the solar cell element shown in Fig. 1, Fig. 3 is a back view of the solar cell element with a mesh protection plate attached, and Fig. 4 is a back view of the solar cell element shown in Fig. 1. FIG. 2 is a cross-sectional view of a conventional solar cell module. 1... Solar cell element, 2... Connection lead, 3... Sealing resin, 4... Drawer lead, 5... Glass Board, 6... Fully retracted frame, 7.8... Protective plate. Figure 7/F Figure 3
Claims (1)
続した太陽電池マトリックスを透明樹脂またはシートに
封じてなる太陽電池モジュールにおいて、前記太陽電池
素子に保護板を貼付けたことを特徴とする太陽電池モジ
ュール。A solar cell module comprising a solar cell matrix in which a plurality of solar cell elements are connected in series, parallel or series-parallel and sealed in a transparent resin or sheet, characterized in that a protection plate is attached to the solar cell elements. .
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59230956A JPS61108178A (en) | 1984-11-01 | 1984-11-01 | Solar cell module |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59230956A JPS61108178A (en) | 1984-11-01 | 1984-11-01 | Solar cell module |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS61108178A true JPS61108178A (en) | 1986-05-26 |
Family
ID=16915951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP59230956A Pending JPS61108178A (en) | 1984-11-01 | 1984-11-01 | Solar cell module |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61108178A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995018466A1 (en) * | 1993-12-30 | 1995-07-06 | Jean Vivier | Solar lamp with dual optimised solar and wind power supply |
JP2007201331A (en) * | 2006-01-30 | 2007-08-09 | Sanyo Electric Co Ltd | Photovoltaic module |
JP2007281530A (en) * | 2007-07-31 | 2007-10-25 | Sanyo Electric Co Ltd | Solar battery module |
US7307210B2 (en) * | 2001-06-13 | 2007-12-11 | Sharp Kabushiki Kaisha | Solar cell and method of producing the same |
WO2012124464A1 (en) * | 2011-03-16 | 2012-09-20 | 三洋電機株式会社 | Solar cell |
-
1984
- 1984-11-01 JP JP59230956A patent/JPS61108178A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995018466A1 (en) * | 1993-12-30 | 1995-07-06 | Jean Vivier | Solar lamp with dual optimised solar and wind power supply |
FR2714715A1 (en) * | 1993-12-30 | 1995-07-07 | Vivier Jean | Solar street lamp with dual power optimized sun and wind. |
US7307210B2 (en) * | 2001-06-13 | 2007-12-11 | Sharp Kabushiki Kaisha | Solar cell and method of producing the same |
JP2007201331A (en) * | 2006-01-30 | 2007-08-09 | Sanyo Electric Co Ltd | Photovoltaic module |
JP2007281530A (en) * | 2007-07-31 | 2007-10-25 | Sanyo Electric Co Ltd | Solar battery module |
WO2012124464A1 (en) * | 2011-03-16 | 2012-09-20 | 三洋電機株式会社 | Solar cell |
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