JPS6182485A - Solar battery panel - Google Patents
Solar battery panelInfo
- Publication number
- JPS6182485A JPS6182485A JP59204449A JP20444984A JPS6182485A JP S6182485 A JPS6182485 A JP S6182485A JP 59204449 A JP59204449 A JP 59204449A JP 20444984 A JP20444984 A JP 20444984A JP S6182485 A JPS6182485 A JP S6182485A
- Authority
- JP
- Japan
- Prior art keywords
- substrate
- sheet
- solar cell
- conductor
- cells
- 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
- 239000000758 substrate Substances 0.000 claims abstract description 29
- 230000005540 biological transmission Effects 0.000 claims abstract description 25
- 239000004020 conductor Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 9
- 238000000151 deposition Methods 0.000 claims abstract description 4
- 239000000853 adhesive Substances 0.000 abstract description 3
- 230000001070 adhesive effect Effects 0.000 abstract description 3
- 229910052751 metal Inorganic materials 0.000 abstract description 2
- 239000002184 metal Substances 0.000 abstract description 2
- 239000012212 insulator Substances 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 241000785736 Pholis crassispina Species 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 239000002699 waste material Substances 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
- H01L31/04—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 adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
- H01L31/05—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells
- H01L31/0504—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells specially adapted for series or parallel connection of solar cells in a module
- H01L31/0508—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells specially adapted for series or parallel connection of solar cells in a module the interconnection means having a particular shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
-
- 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
- H01L31/02002—Arrangements for conducting electric current to or from the device in operations
- H01L31/02005—Arrangements for conducting electric current to or from the device in operations for device characterised by at least one potential jump barrier or surface barrier
- H01L31/02008—Arrangements for conducting electric current to or from the device in operations for device characterised by at least one potential jump barrier or surface barrier for solar cells or solar cell modules
-
- 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)
- Microelectronics & Electronic Packaging (AREA)
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Power Engineering (AREA)
- Sustainable Energy (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の技術分野〕
本発明は例えば人工衛星の電源等として使用される太陽
電池素子を基板に実装した太陽電池・ぐネルに関する。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a solar cell/gunnel in which a solar cell element is mounted on a substrate, and is used, for example, as a power source for an artificial satellite.
太陽電池素子は、光エネルギを電気エネルギに変換する
機能を有しているが、１個の太陽電池素子では大きな電
力力を取れないので、目的とする電力を得るためには、
必要な数の太陽電池素子を電気的に直並列に接続した太
陽電池アレイを、サブストレートと称する基板に実装す
るのが一般的な方法である。Solar cell elements have the function of converting light energy into electrical energy, but since a single solar cell element cannot generate a large amount of power, in order to obtain the desired power,
A common method is to mount a solar cell array in which a required number of solar cell elements are electrically connected in series and parallel on a substrate called a substrate.
第５図及び第６図に従来の実施例を示す。第５図は、太
陽電池素子２の実装面を示し、褌数の太陽電池素子２を
４直列、２並列に接続した太陽電池アレイが基板１に５
モジユール実装されている。各アレイの出力はインタコ
ネクタ３から配線材４により、貫通穴５を通して基板１
の裏面に引き出される。第６図は第５図の裏面図である
。各アレイの配線材４が基板１の端部に集められている
。配線材４は接着剤６によ）基板１に固定される。Conventional embodiments are shown in FIGS. 5 and 6. FIG. 5 shows the mounting surface of the solar cell elements 2, and a solar cell array in which 4 solar cell elements 2 are connected in series and 2 in parallel is mounted on the substrate 1.
Module is implemented. The output of each array is transmitted from the interconnector 3 through the wiring material 4 to the board 1 through the through hole 5.
It is pulled out to the back side. FIG. 6 is a back view of FIG. 5. The wiring members 4 of each array are gathered at the edge of the substrate 1. The wiring material 4 is fixed to the substrate 1 with an adhesive 6).
しかしながら、このような従来の配線処理の方法では基
板１の両側寄りに貫通穴５を多数あけなければならず、
又、そのためのスペースは、太陽電池素子の実装効率の
面から見ると無駄なスペースとなシ、ひいては・臂ネル
の重量増につながる。人工衛星などでは極力軽くて、小
形であることが要求されるので、太陽電池パネルのわず
かな面積、重量の増加は大きな問題となる。However, in such a conventional wiring processing method, it is necessary to make a large number of through holes 5 on both sides of the board 1,
Further, the space for this is a waste of space from the viewpoint of mounting efficiency of the solar cell element, and this leads to an increase in the weight of the armpit. Since satellites and the like are required to be as light and compact as possible, a small increase in the area and weight of solar panels poses a major problem.
又、大きな電力が必畳な場合は、・９ネルのサイズも当
然大きくなるが、それに伴なって、配線材４の線長、本
数が増えることにより、配線重量が増加する。又、配線
固定の手間や、穴あけの手間も多くなるという欠点があ
りた。Furthermore, if a large amount of electric power is required, the size of the 9-channel will naturally increase, and accordingly, the length and number of wiring members 4 will increase, resulting in an increase in the weight of the wiring. Another disadvantage is that it requires more time and effort to fix the wiring and to drill holes.
本発明は上記の欠点を除去するもので、太陽電池素子の
出力を一般の配線材ではなく絶縁シート上に導電体を蒸
着、もしくは導電板を接着した伝送シートを、基板の側
面、あるいは側面と裏面に装着して太陽電池素子の出力
電力の伝送路として用いることによシ、軽量化と電力損
失の低減及びアセンブリの簡単な太陽電池パネルを提供
することを目的とする。The present invention eliminates the above-mentioned drawbacks and connects the output of a solar cell element not to a general wiring material but by depositing a conductor on an insulating sheet or using a transmission sheet with a conductive plate bonded to the side surface of the substrate or the side surface of the substrate. The object of the present invention is to provide a solar cell panel that is lightweight, reduces power loss, and is easy to assemble by being attached to the back side and used as a transmission path for the output power of a solar cell element.
本発明は、複数の太陽電池素子が搭載された基板と、こ
の基板の側面、もしくは側面と裏面に設けられ絶縁シー
ト上に導電体が蒸着あるいは導電板が接着されてなる導
電部が設けられた伝送シートと、この伝送シートの導電
部に前記各太陽電池素子を電気的に接続する配線材とよ
りなるものである。The present invention provides a substrate on which a plurality of solar cell elements are mounted, and a conductive part provided on the side surface of the substrate, or on the side surface and the back surface, and formed by depositing a conductor or adhering a conductive plate on an insulating sheet. It consists of a transmission sheet and a wiring material that electrically connects each of the solar cell elements to the conductive portion of the transmission sheet.
以下図面を参照して本発明の実施例を詳細に説明する。 Embodiments of the present invention will be described in detail below with reference to the drawings.
第１図は本発明の一実施例で、太陽電池素子２を基板１
に実装する方法は従来と同一手法で行なう。すなわち、
８個の太陽電池素子２で４直列、２並列のアレイを構成
し、各プレイに対応した５個のモジー−ルが基板１に接
着剤で固定される。この基板１の側面及び裏面には第３
図に示すように伝送シート９が設けられる。この場合、
基板１の裏面において、両側面に沿った中央部に伝送シ
ートが設けられていない絶縁部１０が設けられる。前記
伝送シート９は第２図に示すように、絶縁シート８の表
面Ｋ例えば金属等の導電体を蒸着もしくは薄い導電板が
接着された導電部１を設けて構成される。而して、前記
各太陽電池素子２は各アレイ毎に電気的にインタコネク
タ３で接続している。それぞれの７レイの両端のインタ
コネクタ３に配線材４の一端を接続し、配線材４の他端
は、基板Ｉの側面に設けられた伝送シート９の導電部７
に接続する。これによシ各太陽電池素子２の出力のプラ
ス側及びマイナス側は基板１０両側面の導電部２に取シ
出されることになる。FIG. 1 shows an embodiment of the present invention, in which a solar cell element 2 is placed on a substrate 1.
The implementation method is the same as the conventional method. That is,
Eight solar cell elements 2 constitute a four-series, two-parallel array, and five modules corresponding to each play are fixed to the substrate 1 with adhesive. The side and back surface of this board 1 have a third
A transmission sheet 9 is provided as shown in the figure. in this case,
On the back surface of the substrate 1, an insulating section 10 without a transmission sheet is provided at the center along both side surfaces. As shown in FIG. 2, the transmission sheet 9 is constructed by providing a conductive portion 1 on the surface K of an insulating sheet 8, on which a conductive material such as metal is deposited or a thin conductive plate is adhered. The solar cell elements 2 are electrically connected to each other by interconnectors 3 for each array. One end of the wiring material 4 is connected to the interconnector 3 at both ends of each 7-lay, and the other end of the wiring material 4 is connected to the conductive portion 7 of the transmission sheet 9 provided on the side surface of the board I.
Connect to. As a result, the positive and negative outputs of each solar cell element 2 are taken out to the conductive parts 2 on both sides of the substrate 10.
なお、第３図に示すようＫ、導電部７が基板１の裏面ま
で設けられている場合には、人工衛星などの熱制御に用
いるアルミニウム蒸着の断熱シートを伝送シート９とし
ても利用できる。In addition, as shown in FIG. 3, when the conductive part 7 is provided up to the back surface of the substrate 1, an aluminum vapor-deposited heat insulating sheet used for heat control of artificial satellites etc. can also be used as the transmission sheet 9.
又、第４図は伝送シート９を基板１の両側面のみに設け
て全体の軽量化を図った一例である。Further, FIG. 4 shows an example in which the transmission sheet 9 is provided only on both sides of the substrate 1 to reduce the overall weight.
上記構成によれば、各太陽電池素子２からの発生電力の
伝送路として伝送シート９の導電部７のような大面積の
導体を利用できるので直流抵抗も小さくなシ、伝送ロス
を低減できる。又、伝送シート９は、絶縁フィルムよシ
なる絶縁シート８上に導電体を蒸着した導電部７を用い
ることで非常に軽く製作できる。更に、人工衛星の太陽
電池パネルでは高温になると太陽電池の発生電力が減少
するため、・母ネルの裏面に熱制御用の塗料を塗るとか
、アルミニウム蒸着されたフィルムを貼る対策がとられ
る。本発明では第３図に示すように、アルミニウム蒸着
等のシートを基板１の裏面中央部分で分割するだけで熱
制御用のアルミニウム蒸着フィルムラ伝送シート９とし
て兼用することが可能である。又、本発明では、伝送シ
ート９を基板１の両側の面、あるいは裏面としているた
め、太陽電池素子２は基板１０表面のｌ”ｔは全面に実
装することができ、面積効率を上げることができ、結果
として軽い太陽電池パネルを実現することができる。According to the above configuration, a large-area conductor such as the conductive portion 7 of the transmission sheet 9 can be used as a transmission path for the power generated from each solar cell element 2, so that direct current resistance is small and transmission loss can be reduced. Further, the transmission sheet 9 can be made very light by using the conductive portion 7 in which a conductor is deposited on the insulating sheet 8 such as an insulating film. Furthermore, when solar panels on satellites reach high temperatures, the power generated by the solar cells decreases, so countermeasures are taken, such as applying a heat-controlling paint to the back of the mother panel or pasting an aluminum vapor-deposited film. In the present invention, as shown in FIG. 3, by simply dividing an aluminum vapor-deposited sheet at the center of the back surface of the substrate 1, it can be used as an aluminum-deposited film transmission sheet 9 for heat control. Further, in the present invention, since the transmission sheet 9 is provided on both sides or the back surface of the substrate 1, the solar cell element 2 can be mounted on the entire surface of the substrate 10, and the area efficiency can be increased. As a result, a lightweight solar panel can be realized.
なお、本発明は人工衛星の太陽電池・セネルなどのよう
に、特に軽量化、高効率を要求される場合に有効である
が、地上で使用される太陽電池・Ｉネルにおいても本発
明の要旨が適用できることは勿論である。Although the present invention is particularly effective in cases where light weight and high efficiency are required, such as solar cells and solar cells for artificial satellites, the gist of the present invention also applies to solar cells and solar cells used on the ground. Of course, this can be applied.
以上述べたように本発明によれば、薄い絶縁シートの表
面に導電体を蒸着もしくは薄い導電板が接着された伝送
シートを、太陽電池素子が搭載された基板の側面、ある
いは側面と裏面に配置して各太陽電池素子の発生電力の
伝送路として用いることにより、面積効率が良く、シか
も軽量化に寄与し、製作コストも安い太陽電池・ぐネル
を提供することができる。As described above, according to the present invention, a transmission sheet in which a conductor is deposited on the surface of a thin insulating sheet or a thin conductive plate is adhered to the surface of the thin insulating sheet is placed on the side surface of the substrate on which the solar cell element is mounted, or on the side surface and the back surface of the substrate on which the solar cell element is mounted. By using it as a transmission path for the power generated by each solar cell element, it is possible to provide a solar cell/gunnel that has good area efficiency, contributes to light weight, and is inexpensive to manufacture.
第１図は本発明の一実施例を示す斜視図、第２図は本発
明に係る伝送シートの一例を示す断面図、第３図は第１
図の正面図、第４図は本発明の他の実施例の正面図、第
５図は従来の太陽電池・母ネルの表面ｌｐＨの斜視図、
第６図は同じく裏面側の斜視図である。
１・・・基板、２・・・太陽電池素子、３・・・インタ
コネクタ、４・・・配線材、７・・・導電部、８・・・
絶縁シート、９・・・伝送シート、１０・・・絶縁部。FIG. 1 is a perspective view showing one embodiment of the present invention, FIG. 2 is a sectional view showing an example of the transmission sheet according to the present invention, and FIG.
4 is a front view of another embodiment of the present invention, FIG. 5 is a perspective view of the surface lpH of a conventional solar cell/mother panel,
FIG. 6 is a perspective view of the back side as well. DESCRIPTION OF SYMBOLS 1... Substrate, 2... Solar cell element, 3... Interconnector, 4... Wiring material, 7... Conductive part, 8...
Insulating sheet, 9... Transmission sheet, 10... Insulating section.
Claims (1)
側面、もしくは側面と裏面に設けられ絶縁シート上に導
電体が蒸着あるいは導電板が接着されてなる導電部が設
けられた伝送シートと、この伝送シートの導電部に前記
各太陽電池素子を電気的に接続する配線材とを具備する
ことを特徴とする太陽電池パネル。A transmission sheet having a substrate on which a plurality of solar cell elements are mounted, and a conductive part provided on the side surface of the substrate, or the side surface and the back surface, and formed by depositing a conductor or adhering a conductive plate on an insulating sheet; A solar cell panel comprising a wiring material for electrically connecting each of the solar cell elements to the conductive portion of the transmission sheet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59204449A JPS6182485A (en) | 1984-09-29 | 1984-09-29 | Solar battery panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59204449A JPS6182485A (en) | 1984-09-29 | 1984-09-29 | Solar battery panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6182485A true JPS6182485A (en) | 1986-04-26 |
Family
ID=16490708
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59204449A Pending JPS6182485A (en) | 1984-09-29 | 1984-09-29 | Solar battery panel |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6182485A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1840976A1 (en) * | 2006-03-31 | 2007-10-03 | Sanyo Electric Co., Ltd. | Internal electrical connections used for a photovoltaic module |
| EP1998379A1 (en) * | 2007-05-29 | 2008-12-03 | Sanyo Electric Co., Ltd. | Solar cell module and method of manufacturing the solar cell module |
| US7812247B2 (en) * | 2006-10-23 | 2010-10-12 | Ascent Solar Technologies Inc. | Flexible photovoltaic array with integrated wiring and control circuitry, and associated methods |
| JP2015002318A (en) * | 2013-06-18 | 2015-01-05 | 三菱電機株式会社 | Solar cell module and manufacturing method thereof |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS51110985A (en) * | 1975-03-25 | 1976-09-30 | Sharp Kk | |
| JPS5615084A (en) * | 1979-07-17 | 1981-02-13 | Matsushita Electric Ind Co Ltd | Structure of solar battery |
| JPS5617081A (en) * | 1979-07-20 | 1981-02-18 | Matsushita Electric Ind Co Ltd | Solar cell structure |
-
1984
- 1984-09-29 JP JP59204449A patent/JPS6182485A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS51110985A (en) * | 1975-03-25 | 1976-09-30 | Sharp Kk | |
| JPS5615084A (en) * | 1979-07-17 | 1981-02-13 | Matsushita Electric Ind Co Ltd | Structure of solar battery |
| JPS5617081A (en) * | 1979-07-20 | 1981-02-18 | Matsushita Electric Ind Co Ltd | Solar cell structure |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1840976A1 (en) * | 2006-03-31 | 2007-10-03 | Sanyo Electric Co., Ltd. | Internal electrical connections used for a photovoltaic module |
| US8927850B2 (en) | 2006-03-31 | 2015-01-06 | Sanyo Electric Co., Ltd. | Photovoltaic module |
| US7812247B2 (en) * | 2006-10-23 | 2010-10-12 | Ascent Solar Technologies Inc. | Flexible photovoltaic array with integrated wiring and control circuitry, and associated methods |
| US9640692B2 (en) | 2006-10-23 | 2017-05-02 | Joseph H. Armstrong | Flexible photovoltaic array with integrated wiring and control circuitry, and associated methods |
| US9653635B2 (en) | 2006-10-23 | 2017-05-16 | Ascent Solar Technologies, Inc. | Flexible high-voltage adaptable current photovoltaic modules and associated methods |
| EP1998379A1 (en) * | 2007-05-29 | 2008-12-03 | Sanyo Electric Co., Ltd. | Solar cell module and method of manufacturing the solar cell module |
| EP2388831A3 (en) * | 2007-05-29 | 2012-05-23 | Sanyo Electric Co., Ltd. | Solar cell module and method of manufacturing the solar cell module |
| US10483419B2 (en) | 2007-05-29 | 2019-11-19 | Panasonic Intellectual Property Management Co., Ltd. | Solar cell module and method of manufacturing the solar cell module |
| JP2015002318A (en) * | 2013-06-18 | 2015-01-05 | 三菱電機株式会社 | Solar cell module and manufacturing method thereof |
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