JP2934366B2 - Solar cells with interconnectors - Google Patents
Solar cells with interconnectorsInfo
- Publication number
- JP2934366B2 JP2934366B2 JP5104359A JP10435993A JP2934366B2 JP 2934366 B2 JP2934366 B2 JP 2934366B2 JP 5104359 A JP5104359 A JP 5104359A JP 10435993 A JP10435993 A JP 10435993A JP 2934366 B2 JP2934366 B2 JP 2934366B2
- Authority
- JP
- Japan
- Prior art keywords
- interconnector
- adhesive
- semiconductor substrate
- solar cell
- thickness
- 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.)
- Expired - Fee Related
Links
Classifications
-
- 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
- Photovoltaic Devices (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、太陽電池セル、特に宇
宙空間において人工衛星搭載用のインターコネクタ付き
太陽電池セルの構造に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a solar cell, and more particularly to a structure of a solar cell with an interconnector for mounting on a satellite in space.
【0002】[0002]
【従来の技術】人工衛星や宇宙ステーションの電源とし
ては、太陽電池セルが並直列につなげられた太陽電池パ
ネルが使用されている。この太陽電池パネルは、人工衛
星を打ち上げるロケットに打ち上げ重量に制限があるた
め、軽量であることが望ましい。人工衛星の中には、一
基で数万枚の太陽電池を使用するものもあり、太陽電池
セル単体も軽量にする必要がある。2. Description of the Related Art As a power source of an artificial satellite or a space station, a solar cell panel in which solar cells are connected in parallel is used. Since the launch weight of a rocket for launching an artificial satellite is limited, it is desirable that the solar battery panel be lightweight. Some artificial satellites use tens of thousands of solar cells, and it is necessary to reduce the weight of solar cells alone.
【0003】図2(a)及び(b)はそれぞれ、従来例
による太陽電池セルの断面図及び裏面図である。FIGS. 2A and 2B are a sectional view and a rear view, respectively, of a conventional solar cell.
【0004】図2(a)及び(b)に示すように、半導
体基板1の上面(受光面)及び裏面にはそれぞれ電極
2,2’が形成されている。この電極2,2’の厚さは
5〜10μm程度である。また、電極2には、他の太陽
電池セルと連結するためのインターコネクタ3が接続さ
れている。インターコネクタ3は通常、電極の厚さより
厚く20〜50μm程度の厚さである。電極2とインタ
ーコネクタ3の接続は、溶接、ハンダ付け等の方法があ
るAs shown in FIGS. 2A and 2B, electrodes 2 and 2 'are formed on the upper surface (light receiving surface) and the rear surface of the semiconductor substrate 1, respectively. The thickness of the electrodes 2, 2 'is about 5 to 10 [mu] m. In addition, an interconnector 3 for connecting to another solar cell is connected to the electrode 2. The interconnector 3 is usually about 20 to 50 μm thicker than the electrode. The connection between the electrode 2 and the interconnector 3 includes a method such as welding or soldering.
【0005】半導体基板1の上面にはさらに、宇宙空間
における放射線の被曝低減及び紫外線遮断のため、カバ
ーガラス4が接着剤5によって接着されている。[0005] A cover glass 4 is further adhered to the upper surface of the semiconductor substrate 1 with an adhesive 5 in order to reduce radiation exposure in space and to block ultraviolet rays.
【0006】このカバーガラス4を接着するには、太陽
電池セルの受光面またはカバーガラス4の裏面に接着剤
を塗布し、太陽電池セルとカバーガラス4を貼り合わせ
る。宇宙空間は真空であるため、この貼り合わせの際に
気泡が入ると気泡が大きくなり接着剤が剥離する可能性
がある。このため、接着剤の中にある気泡を取り除く必
要がある。具体的には、カバーガラスを接着した後、真
空中で脱泡を行い、気泡を取り除いてから接着剤を硬化
させる方法がとられている。To bond the cover glass 4, an adhesive is applied to the light receiving surface of the solar cell or the back surface of the cover glass 4, and the solar cell and the cover glass 4 are bonded together. Since the outer space is in a vacuum, if air bubbles enter during bonding, the air bubbles become larger and the adhesive may peel off. For this reason, it is necessary to remove air bubbles in the adhesive. Specifically, a method has been adopted in which, after bonding a cover glass, defoaming is performed in a vacuum to remove air bubbles and then cure the adhesive.
【0007】[0007]
【発明が解決しようとする課題】ところで、図2に示す
従来の太陽電池セルは、基板のインターコネクタ3の接
続部の厚さaと接続部以外の厚さbとが同じ厚さであ
る。従って、インターコネクタ3を接続するとインター
コネクタ3の厚さだけ接続部全体の厚さが厚くなり、c
に示す厚さのようになる。この太陽電池セルにカバーガ
ラス4を接着すると、インターコネクタ3の接続部上の
接着剤5の厚さと接続部の上以外の接着剤5の厚さが異
なるために応力に差が生じ、宇宙環境のような温度差の
大きい環境下では接着剤5が剥離する可能性がある。こ
のため、従来は接着剤5の塗布量を多くして接着剤5全
体の厚さを厚くし応力の差を少なくしている。Meanwhile, in the conventional solar cell shown in FIG. 2, the thickness a of the connection portion of the interconnector 3 on the substrate and the thickness b other than the connection portion are the same. Therefore, when the interconnector 3 is connected, the thickness of the entire connecting portion is increased by the thickness of the interconnector 3, and c
It becomes like the thickness shown in. When the cover glass 4 is adhered to this solar cell, a difference occurs in stress due to the difference in thickness of the adhesive 5 on the connection part of the interconnector 3 and the thickness of the adhesive 5 other than on the connection part, and a space environment is generated. In an environment having a large temperature difference as described above, the adhesive 5 may peel off. Therefore, conventionally, the application amount of the adhesive 5 is increased to increase the thickness of the entire adhesive 5 and reduce the difference in stress.
【0008】しかし、この方法は、接着剤を多くするこ
とから太陽電池セルの重量が増加するという問題があっ
た。また、d部では段差があるために、接着剤5が広が
る際に気泡が残るという問題があり、この気泡を取り除
くために接着後に真空中で脱泡して気泡を取り除く必要
があり、手間を要するという問題があった。[0008] However, this method has a problem that the weight of the solar battery cell increases because the amount of the adhesive is increased. Further, there is a problem that air bubbles remain when the adhesive 5 spreads because there is a step in the d portion. In order to remove these air bubbles, it is necessary to remove air bubbles by defoaming in a vacuum after bonding. There was a problem of cost.
【0009】[0009]
【課題を解決するための手段】前記目的を達成するため
に本発明は、半導体基板と、該半導体基板の上面端部に
接続されるインターコネクタと、前記半導体基板の上面
及び前記インターコネクタの接続部上に接着剤を介して
接着されるカバーガラスと、を有してなるインターコネ
クタ付き太陽電池セルにおいて、前記インターコネクタ
の上面と前記半導体基板の上面が略面一となるように、
前記半導体基板の前記インターコネクタ接続部の厚みを
接続部以外の部分よりも薄く形成してなることを特徴と
する。In order to achieve the above object, the present invention provides a semiconductor substrate, an interconnector connected to an upper end of the semiconductor substrate, and a connection between the upper surface of the semiconductor substrate and the interconnector. A cover glass adhered to the portion via an adhesive, in an interconnector-equipped solar cell comprising: such that the upper surface of the interconnector and the upper surface of the semiconductor substrate are substantially flush with each other;
The thickness of the interconnector connecting portion of the semiconductor substrate is formed to be thinner than a portion other than the connecting portion.
【0010】[0010]
【作用】インターコネクタの上面と半導体基板の上面を
略面一とできるので、両者のさらに上に塗布する接着剤
の厚みを薄くでき、太陽電池セルの軽量化、コストダウ
ンを図れる。また、接着剤の厚みが均一になるので、応
力がかかることがなく高信頼性が得られる。さらに、イ
ンターコネクタ上面及び半導体基板上面の段差がない、
あるいは少ないことから接着剤の塗布時に、気泡を巻き
込むことがない。従って、従来不可欠であった接着剤塗
布後の真空中の脱泡工程が不要となり、製造工程を簡略
化できる。Since the upper surface of the interconnector and the upper surface of the semiconductor substrate can be substantially flush with each other, the thickness of the adhesive applied thereon can be reduced, and the weight and cost of the solar cell can be reduced. In addition, since the thickness of the adhesive becomes uniform, high reliability can be obtained without stress. Furthermore, there is no step between the upper surface of the interconnector and the upper surface of the semiconductor substrate,
Alternatively, air bubbles are not involved when the adhesive is applied because of a small amount. Therefore, the defoaming step in vacuum after application of the adhesive, which is conventionally indispensable, becomes unnecessary, and the manufacturing process can be simplified.
【0011】[0011]
【実施例】本発明の一実施例について、図1を参照して
説明する。図1(a)及び(b)はそれぞれ、本実施例
によるインターコネクタ付き太陽電池セルの断面図及び
裏面図である。図1に示す従来例と同一機能部分には同
一記号を付している。ここでは、主に従来例と異なる点
について説明する。An embodiment of the present invention will be described with reference to FIG. FIGS. 1A and 1B are a cross-sectional view and a rear view, respectively, of a solar cell with an interconnector according to the present embodiment. The same symbols are given to the same functional parts as the conventional example shown in FIG. Here, points different from the conventional example will be mainly described.
【0012】本実施例の太陽電池セルは、図1に示すよ
うに、インターコネクタ3の溶接部全体の厚さc’が溶
接部以外の厚さb’とほぼ同じになっている点に特徴が
ある。 本実施例においては、半導体基板1’の内イン
ターコネクタ3を接続する溶接部の厚みを薄く形成す
る。この方法としては、例えば、フォトリソグラフィー
でパターンを形成した後に、エッチングにより部分的に
基板をエッチングする方法がある。ここで、この薄い部
分は、電極2、インターコネクタ3を設けることによっ
てインターコネクタ3の上面と半導体基板1’の溶接部
以外の上面とが面一となるような厚みとしておく。As shown in FIG. 1, the solar cell of this embodiment is characterized in that the thickness c 'of the entire welded portion of the interconnector 3 is substantially the same as the thickness b' of the portion other than the welded portion. There is. In the present embodiment, the thickness of the welded portion connecting the inner interconnector 3 of the semiconductor substrate 1 'is formed thin. As this method, for example, there is a method of forming a pattern by photolithography and then partially etching the substrate by etching. Here, the thin portion is provided with the electrode 2 and the interconnector 3 so that the upper surface of the interconnector 3 is flush with the upper surface of the semiconductor substrate 1 'other than the welded portion.
【0013】次に、この半導体基板1’の上面に接着剤
5’を介してカバーガラス4を接着する。Next, the cover glass 4 is adhered to the upper surface of the semiconductor substrate 1 'via an adhesive 5'.
【0014】以上のような形状とすることによって、接
着剤5’の厚さを均一にすることができ、従来の問題点
であった応力の差を無くすことができ信頼性の向上を図
れる。 また、接着剤4’を塗布する際には、d’より
明らかなように、従来のような段差がないので、接着剤
4’が広がる時に気泡を巻き込むことがなくなり、従来
不可欠であった接着剤塗布後の真空中での気泡の脱泡工
程が不要となり、製造工程を簡略化できる。さらに、段
差がないことから、従来採用できなかった接着剤を使用
しないダイレクトボンド法も適用できる。By adopting the above-mentioned shape, the thickness of the adhesive 5 'can be made uniform, and the difference in stress, which has been a conventional problem, can be eliminated, and the reliability can be improved. Also, when applying the adhesive 4 ', as is clear from d', since there is no step as in the conventional case, air bubbles are not involved when the adhesive 4 'spreads, and the adhesive which has been indispensable in the past. The step of removing bubbles in a vacuum after application of the agent is not required, and the manufacturing process can be simplified. Furthermore, since there is no step, a direct bonding method that does not use an adhesive, which has not been conventionally adopted, can also be applied.
【0015】しかも、接着剤の厚さを薄く、即ち接着剤
の重量を軽量化できるので太陽電池セルとしての軽量化
を図れるとともにコストダウンを図れる。In addition, since the thickness of the adhesive can be reduced, that is, the weight of the adhesive can be reduced, the weight of the solar cell can be reduced and the cost can be reduced.
【0016】なお、c’の厚みはb’より若干大きくて
も、従来に比べると段差を小さくできるので程度は下が
るものの、上記と同様の効果を奏することができる。Even if the thickness of c 'is slightly larger than b', the same effect as described above can be obtained, though to a lesser extent, since the step can be made smaller than in the prior art.
【0017】[0017]
【発明の効果】半導体基板にカバーガラスを接着するた
めの接着剤の厚さを均一にでき、従来の問題点であった
応力の差を無くすことができ、信頼性を向上できる。ま
た、従来不可欠であった真空中での気泡の脱泡工程が不
要となり、製造工程を簡略化できる。さらに、接着剤量
を低減できるので太陽電池セルとしての軽量化を図れる
とともにコストダウンできる。According to the present invention, the thickness of the adhesive for bonding the cover glass to the semiconductor substrate can be made uniform, the difference in stress, which has been a problem in the past, can be eliminated, and the reliability can be improved. In addition, the step of removing bubbles in a vacuum, which is indispensable in the past, becomes unnecessary, and the manufacturing process can be simplified. Further, since the amount of the adhesive can be reduced, the weight of the solar cell can be reduced and the cost can be reduced.
【図1】(a)及び(b)はそれぞれ、本発明の一実施
例によるインターコネクタ付き太陽電池セルの断面図及
び裏面図である。FIGS. 1A and 1B are a cross-sectional view and a rear view, respectively, of a solar cell with an interconnector according to an embodiment of the present invention.
【図2】(a)及び(b)はそれぞれ、従来例によるイ
ンターコネクタ付き太陽電池セルの断面図及び裏面図で
ある。FIGS. 2A and 2B are a cross-sectional view and a rear view, respectively, of a conventional solar cell with an interconnector.
1’ 半導体基板 3 インターコネクタ 4 カバーガラス 5’ 接着剤 1 'semiconductor substrate 3 interconnector 4 cover glass 5' adhesive
Claims (1)
接続されるインターコネクタと、前記半導体基板の上面
及び前記インターコネクタの接続部上に接着剤を介して
接着されるカバーガラスと、を有してなるインターコネ
クタ付き太陽電池セルにおいて、 前記インターコネクタの上面と前記半導体基板の上面が
略面一となるように、前記半導体基板の前記インターコ
ネクタ接続部の厚みを接続部以外の部分よりも薄く形成
してなることを特徴とするインターコネクタ付き太陽電
池セル。1. A semiconductor substrate, an interconnector connected to an upper end of the semiconductor substrate, a cover glass adhered on an upper surface of the semiconductor substrate and a connecting portion of the interconnector via an adhesive, In a solar cell with an interconnect comprising: a portion other than a connecting portion of the interconnector connecting portion of the semiconductor substrate so that an upper surface of the interconnector and an upper surface of the semiconductor substrate are substantially flush with each other. A solar cell with an interconnector characterized by being formed thinner than the above.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5104359A JP2934366B2 (en) | 1993-04-30 | 1993-04-30 | Solar cells with interconnectors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5104359A JP2934366B2 (en) | 1993-04-30 | 1993-04-30 | Solar cells with interconnectors |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH06314810A JPH06314810A (en) | 1994-11-08 |
| JP2934366B2 true JP2934366B2 (en) | 1999-08-16 |
Family
ID=14378653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5104359A Expired - Fee Related JP2934366B2 (en) | 1993-04-30 | 1993-04-30 | Solar cells with interconnectors |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2934366B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5980540B2 (en) * | 2012-04-02 | 2016-08-31 | シャープ株式会社 | Method for producing thin film compound solar cell with interconnector, method for producing thin film compound solar cell string, and method for producing thin film compound solar cell array |
-
1993
- 1993-04-30 JP JP5104359A patent/JP2934366B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH06314810A (en) | 1994-11-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |