JPH03214676A - Pin-type amorphous silicon solar cell and manufacture thereof - Google Patents
Pin-type amorphous silicon solar cell and manufacture thereofInfo
- Publication number
- JPH03214676A JPH03214676A JP2008231A JP823190A JPH03214676A JP H03214676 A JPH03214676 A JP H03214676A JP 2008231 A JP2008231 A JP 2008231A JP 823190 A JP823190 A JP 823190A JP H03214676 A JPH03214676 A JP H03214676A
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- Prior art keywords
- film
- amorphous silicon
- solar cell
- layer
- pin
- 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.)
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- 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
- Y02E10/545—Microcrystalline silicon PV 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
- Y02E10/548—Amorphous silicon PV cells
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Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、pin Wアモルファスシリコン太陽電池お
よびその製造方法に関する。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a pin W amorphous silicon solar cell and a method for manufacturing the same.
pin型アモルファスシリコン太陽電池は、高効率化な
実現するために、t層に、水素化アモルファスシリコン
( a−Si : H )よりも光学ギャップの小サイ
、水素化アモルファスシリコンゲルマニウム( a −
SiGg : H )を用いて、長波長光の吸収を増
大させる工夫がされてきた。In order to achieve high efficiency, pin-type amorphous silicon solar cells use hydrogenated amorphous silicon germanium (a-Si:H), which has a smaller optical gap than hydrogenated amorphous silicon (a-Si:H), in the T layer.
Efforts have been made to increase the absorption of long wavelength light using SiGg:H).
しかし、α−SiGa:H膜は、膜形成する際のSi原
料ガスとG6原料ガスの反応性が大きく異なる。However, in the α-SiGa:H film, the reactivity of the Si source gas and the G6 source gas during film formation is significantly different.
このため、この膜は均一にSi原子とG−原子が分布し
、しかも膜中のダングリングボンドの少ない膜を形成す
ることが難しく、a−SiGg:H膜の優位性を発揮で
きなかった。For this reason, it was difficult to form a film in which Si atoms and G atoms were uniformly distributed and there were few dangling bonds in the film, and the superiority of the a-SiGg:H film could not be demonstrated.
そこで、ジャーナル・オブ・ノンクリスタル・ソリッズ
97.98巻(1987年)第1667〜第1374頁
( JowrnaL of Non − Cryzta
llirx !;olidz + 97&98 ( 1
987 ) LS67〜1374)に、トライオード方
式のプラズマCVD法あるいは水素希釈法により、α−
SiGe:H膜の光導寛特性を改善することが提案され
ている。Therefore, Journal of Non-Crystal Solids, Vol. 97.98 (1987), pp. 1667-1374.
llirx! ;olidz + 97 & 98 ( 1
987) LS67 to 1374), α-
It has been proposed to improve the light guiding properties of SiGe:H films.
さらに最近、高真空域でマイクロ波プラズマCVD法を
用いることにより, Si原料ガスとGa原料ガスの分
解反応性の差をなくし、光導電特性を改嵜する方法も注
目されている。Furthermore, recently, a method of improving photoconductive properties by eliminating the difference in decomposition reactivity between Si source gas and Ga source gas by using microwave plasma CVD in a high vacuum region has also been attracting attention.
しかし、トライオード方式を用いると、成膜速度が1彩
一以下と遅く、膜厚が数10oo i必要なpin型太
陽電池のt層としては実用的ではない。However, when the triode method is used, the film formation rate is as slow as one color or less, and it is not practical as a T-layer of a pin-type solar cell, which requires a film thickness of several 10 oo i.
また、水素希釈法あるいはマイクロ波プラズマCVD法
を用いた時、光導電特性が優れたpin型太陽電池のi
層を形成する成膜条件では、原料ガス( SzH4 ,
GgH4等)から多くの水累ガスが発生し、基板上に
形成されている膜に損傷を生じやすく、結局、変換効率
が低下してしまう。In addition, when hydrogen dilution method or microwave plasma CVD method is used, pin-type solar cells with excellent photoconductive properties can be produced.
Under the film forming conditions for forming the layer, source gases (SzH4,
(GgH4, etc.), which tends to damage the film formed on the substrate, resulting in a decrease in conversion efficiency.
このようにいまだ、アモルファスシリコンゲルマニウム
の特性を生かした太陽電池は、開発されていなかった。Thus, a solar cell that takes advantage of the characteristics of amorphous silicon germanium has not yet been developed.
そこで、本発明の目的は、長波長光の吸収に優レt.−
水素化アモルファスシリコンゲルマニウム(α−Si
Ge:H) を用いた、安価で、光導電特性に優れ、変
換効率に優れている太陽電池を提供することにある。SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a t. −
Hydrogenated amorphous silicon germanium (α-Si
An object of the present invention is to provide a solar cell using Ge:H) that is inexpensive, has excellent photoconductive properties, and has excellent conversion efficiency.
本発明の目的は
ilとしてアモルファスシリコンゲルマニウムを用いた
pin型アモルファスシリコン太陽電池において、
p N トアモルファスシリコンゲルマニウム膜トの間
に、少なくとも1層の水素ガス耐性のある保護膜を有す
ることを特徴とするアモルファスシリコン太陽電池によ
って達成される。The object of the present invention is to provide a pin-type amorphous silicon solar cell using amorphous silicon germanium as an il, which is characterized by having at least one protective film resistant to hydrogen gas between the pN amorphous silicon germanium films. This is achieved by amorphous silicon solar cells.
また、本発明の目的は、
少なくともp層、i層、ル層および基板からなるアモル
ファスシリコン太陽電池において、i Ni カ少ナ<
ト4 ,アモルファスシリコンゲルマニウム膜と、水
素ガス耐性のある保護膜とがらなり、
前記保護膜が前記アモルファスシリコンゲルマニウム膜
より基板側にあることを特徴とするpin型アモルファ
スシリコン太陽電池によって達成される。It is also an object of the present invention to provide an amorphous silicon solar cell comprising at least a p layer, an i layer, a layer and a substrate,
(4) This is achieved by a pin type amorphous silicon solar cell comprising an amorphous silicon germanium film and a protective film resistant to hydrogen gas, wherein the protective film is located closer to the substrate than the amorphous silicon germanium film.
さらに、本発明の目的は、
アモルファスシリコンゲルマニウムを用(・たpin型
アモルファスシリコン太陽電池の製造方法において、
i層の形成にあたり、プラズマパワー密度が0. 0
5 W/一以下で、水素含有量10チ以下のガスをプラ
ズマ分解することにより、p層上にアモルファスシリコ
ン膜を成膜した後、
前記アモルファスシリコン膜上にアモルファスシリコン
ゲルマニウム膜を形成したことを特徴とするpin型ア
モルファスシリコン太陽電池の製造方法によっても達成
される。Furthermore, an object of the present invention is to provide a method for manufacturing a pin-type amorphous silicon solar cell using amorphous silicon germanium, in which the plasma power density is 0.0 when forming an i-layer.
After forming an amorphous silicon film on the p-layer by plasma decomposing a gas with a hydrogen content of 10 or less at 5 W/1 or less, an amorphous silicon germanium film was formed on the amorphous silicon film. This can also be achieved by a method for manufacturing a pin-type amorphous silicon solar cell.
保賎膜の組成は、製造時に、保護膜形成以前に基板に成
膜されている膜(例えば、電極膜やP層を指す。以下,
下地膜という.)に損傷を与えなければ、特に限定され
ることはないが、光導電特性の優れたa−Si:H膜が
好ましく用いられる。The composition of the protective film is the film formed on the substrate before the formation of the protective film (for example, electrode film or P layer.Hereinafter, it refers to the film formed on the substrate before forming the protective film.
It is called the base film. ), an a-Si:H film having excellent photoconductive properties is preferably used, although there are no particular limitations.
この場合には、α一Si:H膜とα−SiGa:H膜よ
りなる多層化した龜層を有するpin型太¥jhvL池
となる。本発明においては,1層は何層になろうと限定
されない。In this case, it becomes a pin type thick layer having a multilayered head layer made of an α-Si:H film and an α-SiGa:H film. In the present invention, one layer is not limited to any number of layers.
保膜膜の膜厚は、太陽電池を構成する他の膜の成膜条件
により異なるが、一般的に10oo,;以上が好ましい
。10oo iより膜が薄いと下地膜への損傷を食い止
める効果が少なくなってしま5。The film thickness of the film-holding film varies depending on the film-forming conditions of other films constituting the solar cell, but is generally preferably 100 mm or more. If the film is thinner than 10 oo i, it will be less effective in preventing damage to the underlying film5.
保腰膜の成膜手段は,光CVD法,あるいは成膜速度の
小さいグロー放電プラズマCVD法等が好ましい。The method for forming the lumbar protection film is preferably a photo-CVD method or a glow discharge plasma CVD method, which has a low film-forming rate.
a−.5i:H膜を、プラスマバヮー密度0. 0 5
f /一以下で、水素含有量10%以下のガスをプラ
ズマ分解して形成することが好ましい。a-. 5i:H film at a plasma bower density of 0. 0 5
It is preferable to form by plasma decomposition of a gas having f/1 or less and a hydrogen content of 10% or less.
水素含有量が10%以上のガスを用いると、下地膜に損
傷を与え変換効率が低下する.また、ブラx” −r
ハ’7 − 密度0. 0 5 F/一以上のプラズマ
分解でも、下地膜に損傷を与えてしまう。If a gas with a hydrogen content of 10% or more is used, the underlying film will be damaged and the conversion efficiency will decrease. Also, bra x”-r
C'7 - Density 0. Even plasma decomposition of 0 5 F/1 or more damages the underlying film.
本発明のアモルファスシリコンゲルマニウムを用いた太
陽電池は、α−SiGa:H膜を形成する以前に、水素
ガスから下地膜上を保獲する膜を作る。In the solar cell using the amorphous silicon germanium of the present invention, before forming the α-SiGa:H film, a film is made from hydrogen gas to capture the base film.
上記保膜膜が、光導電特性が高いα−.SiGt :
H農の製造時に発生する水素ガスによって引き起こされ
る、ドーピングを施した下地膜に対する物理的、化学的
な損傷を防止する。The above-mentioned film-retaining film has α-. SiGt:
Prevents physical and chemical damage to the doped base film caused by hydrogen gas generated during the production of hydrogen.
さらに、上記保護膜としてプラズマバワー密度が0.0
5W/cm3以下で、水素含有1ik10%以下のカス
をプラズマ分解して成膜したα一.Si:H膜を用いれ
ば、下地膜が水素ガスにより損傷を受けない、光導電特
性が優れた膜を成膜1−ることかできる。Furthermore, the protective film has a plasma power density of 0.0.
The α-1 film was formed by plasma decomposition of scum with a hydrogen content of 10% or less at a power of 5W/cm3 or less. By using the Si:H film, it is possible to form a film with excellent photoconductive properties in which the underlying film is not damaged by hydrogen gas.
本発明の実施例について説明するが、本発明はこれに限
定されるものではない。Examples of the present invention will be described, but the present invention is not limited thereto.
第1図は、本発明のa − SiGg : E膜を用い
た太陽電池の構成を示す断面図である。FIG. 1 is a sectional view showing the structure of a solar cell using the a-SiGg:E film of the present invention.
太陽電池は、Sn 0 2膜2を形成したガラス基板1
上に、p層としてのB原子ドープα一.Si:H膜ろと
、保膿膜して8Il!,1項目のi層のα−Si:H膜
4、第21一目のt層としてのa − SiGa :
H a5と、P原子ドープ微結晶.5i膜6と裏面M′
vlL極7とを順次積層して構成されている。The solar cell includes a glass substrate 1 on which a Sn 0 2 film 2 is formed.
Above, B atom-doped α-1 as a p-layer. Si:H membrane and purulent membrane are 8Il! , α-Si:H film 4 of the i-layer of item 1, a-SiGa as the t-layer of the 21st item:
Ha5 and P atom-doped microcrystals. 5i film 6 and back surface M'
It is constructed by sequentially stacking vlL poles 7.
カラス基板1は青板ガラスを用い、この上に.5 n
O2膜2を5000 i程度形成する。p型α一S龜:
H膜は、H,希釈B,H6とS L E4を通常の1!
1.56MHzの平行平板型τfプラズマCVD法によ
り形成する。The glass substrate 1 is made of blue plate glass. 5 n
An O2 film 2 is formed to a thickness of about 5000 i. p-type α-S:
For the H film, add H, dilution B, H6 and S L E4 to the usual 1!
It is formed by a 1.56 MHz parallel plate type τf plasma CVD method.
保護膜である第1層目のi−a−si:H膜4はS *
H4ガスを通常の1 5. 56 MHzの平行平板
型rfプラズマCVD法により、低い電力密度(好まし
くは15y++F/一以下)で1500ノ形成する。The first layer ia-a-si:H film 4, which is a protective film, is S*
H4 gas as usual 15. 1,500 layers are formed at a low power density (preferably 15y++F/1 or less) by a 56 MHz parallel plate type rf plasma CVD method.
第2N目のt一α−SiGa:H膜5は、第3図に示す
ような有磁場マイクロ波プラズマCVD装置を用いて形
成する。上記有磁場マイクロ波プラズマCVI)装置は
、排気口19がら排気される真空呈12と、その上部に
、配置された放電管13と、マイクロ波を供給するマグ
ネトロン10と,供給されるマイクロ波を上記放電管1
3に導波する導波管11とを備える。上記放電管13の
周囲には、磁場を発生するソレノイドコイル14が設け
られている。真空室12には,基&17を載置する試料
台18が設けてあり、また先端が放電管13方向に開口
する放電ガス導入口15と、試料台18方向に開口する
成膜ガス導入口16が設けてある。上記ル型微結晶Si
膜6は、平行平板壓rfプラズマCVD法により形成す
ることができる。また、裏面M電極7は通常の真空蒸着
法により形成する。The 2Nth t-α-SiGa:H film 5 is formed using a magnetic field microwave plasma CVD apparatus as shown in FIG. The above-mentioned magnetic field microwave plasma CVI) apparatus includes a vacuum chamber 12 that is evacuated through an exhaust port 19, a discharge tube 13 disposed above the vacuum chamber 12, a magnetron 10 that supplies microwaves, and a The above discharge tube 1
3 and a waveguide 11 for guiding the wave. A solenoid coil 14 that generates a magnetic field is provided around the discharge tube 13. The vacuum chamber 12 is provided with a sample stand 18 on which the substrate &17 is placed, and a discharge gas inlet 15 whose tip opens toward the discharge tube 13 and a film-forming gas inlet 16 which opens toward the sample stand 18. is provided. The above le-type microcrystalline Si
The film 6 can be formed by a parallel plate RF plasma CVD method. Further, the back surface M electrode 7 is formed by a normal vacuum evaporation method.
本発明の太陽電池と、本発明外の太陽電池の性能を比較
するために、次のような太陽電池を製造した。In order to compare the performance of the solar cells of the present invention and solar cells other than the present invention, the following solar cells were manufactured.
(本発明の太陽電池の製造)
青板ガラスからなるガラス基板1上に、Sルo2膜2を
約5000 ;形成したものを用いた。この基板に13
.56MHz の平行平板壓rfプラズマCVD法を用
い、原料ガスとしてH,希釈1%B,H,(シボラン)
20sccmとSiH4 20 sccmを流し、基板
温度160℃、反応圧力200mTorr , rf
電力3Wの条件でB原子をドーブしたα−Si二H膜6
を形成した。(Manufacture of solar cell of the present invention) A solar cell was used in which approximately 5,000 layers of S2O2 film 2 were formed on a glass substrate 1 made of soda lime glass. 13 on this board
.. Using a 56MHz parallel plate RF plasma CVD method, H was used as the raw material gas, and diluted 1% B, H, (ciborane) was used.
Flowing 20 sccm and SiH4 20 sccm, substrate temperature 160°C, reaction pressure 200 mTorr, rf
α-Si diH film 6 doped with B atoms under the condition of power 3W
was formed.
次にこの上に保護膜である第1層目のt,層4として、
SiH4 25 sccm,基板温度180℃,反応圧
力200 mTorr , rf電力3F(プラズマバ
ヮー密度9.6W/c1/l)の条件でa−.Si:H
ppを+1+ 10oo.; ,+21 1500,4
, (3) 20004 各々形成したものを作製し
た。なお、水素ガス濃度は0チである。Next, on top of this, the first layer t, which is a protective film, is layer 4.
A-. Si:H
PP +1+ 10oo. ; ,+21 1500,4
, (3) 20004 Each of these was manufactured. Note that the hydrogen gas concentration is 0.
各々の試料に対して同じ条件で第2層目の番層として、
第3図に示す有磁場マイクロ波プラズマCVD装置を用
い、α−SiGa:H膜5を形成した。As the second layer under the same conditions for each sample,
An α-SiGa:H film 5 was formed using a magnetic field microwave plasma CVD apparatus shown in FIG.
成膜ガス導入口16から.5iH48sccmとGgH
4 4 scam、放電ガス導入口15から4 6 s
ec@を流し、マイクロ波周波数2. 54 GHz
,マイクロ波出力100F,放電ガス圧1.6mTor
r,基板温度180℃、放電管13の排気側端部での磁
場強度を875Gの条件でa−SiGg :H膜を形成
した。From the film forming gas inlet 16. 5iH48sccm and GgH
4 4 scan, 4 6 s from discharge gas inlet 15
ec@, microwave frequency 2. 54 GHz
, microwave output 100F, discharge gas pressure 1.6mTor
An a-SiGg:H film was formed under the following conditions: r, substrate temperature of 180° C., and magnetic field strength at the exhaust side end of the discharge tube 13 of 875 G.
次に前記3試料についてル撒微結晶54膜6をH2希釈
10oo ppm .ホスフィン50 pccm ,
SiH4 2 zcarn +成膜温度170℃,反応
圧力600 mT orr の条件で平行平板型τfプ
ラズマCVI)法で放電電力60Wで形成した。Next, for the three samples mentioned above, the microcrystalline 54 film 6 was diluted with H2 to 100 ppm. Phosphine 50 pccm,
The film was formed using a parallel plate type τf plasma CVI) method with a discharge power of 60 W under the conditions of SiH4 2 zcarn + film formation temperature of 170° C. and reaction pressure of 600 mTorr.
ついで、裏面M電極を抵抗加熱蒸着により形成し、太陽
電池を得た。Next, a back M electrode was formed by resistance heating vapor deposition to obtain a solar cell.
α−Si:H膜を(11 1000,4 , +2+
1sooA, (31 2ooo,;の太陽電池を実施
例−1,同−2.同−3とする。α-Si:H film (11 1000,4, +2+
The solar cells of 1sooA, (31 2ooo,;) are referred to as Example-1, Example-2, and Example-3.
水素ガス濃度は9チであるSiH4 25zccm ,
基板温度180℃,反応圧力200 rnTorr ,
rf電力13F(プラズマパワー密度[Loar/,
1)の条件で、保膿膜としてα−Si:H膜4を形成し
た以外は、上記実施例−2と同様にして実施例−4の太
陽電池を作成した。SiH4 with a hydrogen gas concentration of 9 zccm,
Substrate temperature 180℃, reaction pressure 200rnTorr,
rf power 13F (plasma power density [Loar/,
A solar cell of Example 4 was produced in the same manner as Example 2 above, except that the α-Si:H film 4 was formed as a purulent retention film under the conditions of 1).
(比較例の太陽電池の製造)
保膜膜のα一Si:H膜4を形成せず、上記p層α一S
i:H膜3の上に直接i一α−5iGm:H膜5を形成
したことを除いて、他の条件を全く同一として比較例−
1の太陽電池を形成した。(Manufacture of solar cell of comparative example) Without forming the α-Si:H film 4 of the film-holding film, the p-layer α-S
Comparative example under the same conditions except that the i-α-5iGm:H film 5 was directly formed on the i:H film 3.
1 solar cell was formed.
α一Si:H膜4の形成に際し、水素含有量が12チの
ガスを、rf電力16W(プラズマバワー密度が0.
05 F/一)で形成したことを除いて、他の条件を実
施例−2と同一として比較例−2の太陽電池を形成した
。When forming the α-Si:H film 4, a gas with a hydrogen content of 12% was used at an RF power of 16W (plasma power density of 0.5%).
A solar cell of Comparative Example 2 was formed under the same conditions as Example 2 except that it was formed using 05 F/1).
α−Si:H膜4の形成に際し、水素含有量が10%の
ガスを、rf寛力19W(プラズマパワー密度が0.[
l6F/,!) で形成したことを除いて、他の条件を
実施例−2と同一として比較例−3の太陽電池を形成し
た。When forming the α-Si:H film 4, a gas with a hydrogen content of 10% was used at an RF tolerance of 19W (plasma power density of 0.[
l6F/,! ) A solar cell of Comparative Example 3 was formed under the same conditions as Example 2 except for forming the solar cell in Comparative Example 3.
α−Si:H膜4の形成に際し、水素含有量が12%の
ガスを、γft力19W(プラズマパワー密度が0.
06 W/l,t) で形成したことを除いて、他の条
件を実施例−2と同一として比較例−4の太陽電池を形
成した。When forming the α-Si:H film 4, a gas with a hydrogen content of 12% was supplied with a γft force of 19W (plasma power density of 0.
A solar cell of Comparative Example 4 was formed under the same conditions as Example 2 except that the solar cell was formed at 0.06 W/l, t).
(本発明の太陽電池と比較例の太陽電池の性能比較)
上記の本発明と比較例の太陽電池をAM1.5,100
mF/一赤色フィルター下においてI−V%性の測定を
行った。(Performance comparison between the solar cell of the present invention and the solar cell of the comparative example) The solar cells of the present invention and the solar cell of the comparative example were
I-V% measurements were carried out under mF/one red filter.
その結果を第2図に示す。The results are shown in FIG.
第2図は,α−Si:H腺厚1 500 Aである本発
明の実施例−2の太陽電池のI−V特性8を基準に、比
較例−1の太陽電池の7−V特性9を示している。短絡
電流、開放電圧はそれほど差がないが、曲線因子は比較
例(曲線9)で0457に対し、本発明の太陽電池(曲
線8)では0.571と大きく向上しており、曲線因子
が改善されている。Figure 2 shows the 7-V characteristics 9 of the solar cell of Comparative Example 1 based on the IV characteristics 8 of the solar cell of Example 2 of the present invention, which has an α-Si:H gland thickness of 1 500 A. It shows. Although there is not much difference in short circuit current and open circuit voltage, the fill factor is 0.571 in the solar cell of the present invention (curve 8) compared to 0457 in the comparative example (curve 9), which is a significant improvement, indicating that the fill factor has improved. has been done.
このように本発明の太陽電池では、曲線因子が太きいた
め、曲線因子×開放電圧×短絡電流密度で表わされる変
換効率が改善される。As described above, in the solar cell of the present invention, since the fill factor is large, the conversion efficiency expressed by fill factor x open circuit voltage x short circuit current density is improved.
同様にして、本発明のα−Si:H膜厚が10oo.,
;.2000 Aの実施例−1,同−3さらに実施例−
4の太陽電池では、曲線因子0.55以上の良好な特性
のものが得られた。これに対し、比較例−2.同3,同
−4の太陽電池は曲線因子が0.50以下となり、曲線
因子が小さかった。Similarly, the thickness of the α-Si:H film of the present invention was 10 oo. ,
;. 2000 A Example-1, Same-3 and Example-
In the solar cell No. 4, good characteristics with a fill factor of 0.55 or more were obtained. On the other hand, Comparative Example-2. The solar cells No. 3 and No. 4 had a fill factor of 0.50 or less, which was a small fill factor.
本発明のように、下地膜上に保膿膜としてaSi:H膜
を設けることにより、下地膜に損傷がなく、変換効率が
良好な太陽電池を得ることができる。By providing an aSi:H film as a purulent-retaining film on the base film as in the present invention, a solar cell with good conversion efficiency without damage to the base film can be obtained.
特に、長波長光域にまで吸収特性を有するa一S*Gg
:H膜を,下地膜の損傷なしにi層として形成すること
ができるので,アモルファスシリコンゲルマニウムを用
いた太陽電池の効率を大幅に向上できる。In particular, a-S*Gg, which has absorption characteristics even in the long wavelength light range.
Since the :H film can be formed as an i-layer without damaging the underlying film, the efficiency of solar cells using amorphous silicon germanium can be greatly improved.
第1図は,本発明のシリコンゲルマニウムヲ用いたアモ
ルファス太陽電池の構成の一例を示す断面図である。
第2図は、本発明の実施例及び比較例のシリコンゲルマ
ニウムを用いたアモルファス太陽taの1−V特性を示
す図である。
第6図は、太陽電池のλ層α−SiGa:H腺形成に用
いるマイクロ波プラズマCVD装置の一例の構造の概要
を示す図である。
1・・・・・・・・・・・・ガラス基板2・・・・・・
・・・・・・S 30 2展3・・・・・・・・・・・
・pmα−Si:H膜4・・・・・・・・・・・・i−
α−Si:H腺5・・・・・・・・・・・・i−a−S
乙Gm:Hli6・・・・・・・・・・・・ルー微結晶
Sip7・・・・・・・・・・・裏面A1電極8・・・
・・・・・・・・・本発明の実施例により作製した太陽
電池のI−V特性
9・・・・・・・・・・・比較例により作製した太陽電
池のI一V特性
10・・・・・・・・・マグ不トロン
11・・・・・・・・・導波管
12・・・・・・・・・真空室
13・・・・・・・・・放電管
ソレノイドコイル
放電ガス導入日
成膜ガス導入口
基板
試料台
排気口FIG. 1 is a sectional view showing an example of the structure of an amorphous solar cell using silicon germanium of the present invention. FIG. 2 is a diagram showing 1-V characteristics of amorphous solar ta using silicon germanium according to an example of the present invention and a comparative example. FIG. 6 is a diagram schematically showing the structure of an example of a microwave plasma CVD apparatus used for forming a λ layer α-SiGa:H gland in a solar cell. 1......Glass substrate 2...
・・・・・・S 30 2 Exhibition 3・・・・・・・・・・・・
・pmα-Si:H film 4・・・・・・・・・・・・i-
α-Si:H gland 5・・・・・・・・・i-a-S
Otsu Gm: Hli6......Lou microcrystal Sip7......Back side A1 electrode 8...
......I-V characteristics of the solar cells produced according to the examples of the present invention 9...........I-V characteristics of the solar cells produced according to the comparative examples 10.・・・・・・・・・Magnetron 11・・・・・・Waveguide 12・・・・・・Vacuum chamber 13・・・・・・Discharge tube solenoid coil Discharge gas introduction Daily film gas inlet Substrate sample stage exhaust port
Claims (1)
いたpin型アモルファスシリコン太陽電池において、 p層とアモルファスシリコンゲルマニウム膜との間に、
少なくとも1層の水素ガス耐性のある保護膜を有するこ
とを特徴とするアモルファスシリコン太陽電池。 2、少なくともp層、i層、n層および基板からなるア
モルファスシリコン太陽電池において、i層が少なくと
も、アモルファスシリコンゲルマニウム膜と、水素ガス
耐性のある保護膜とからなり、 前記保護膜が前記アモルファスシリコンゲルマニウム膜
より基板側にあることを特徴とするpin型アモルファ
スシリコン太陽電池。 3、前記保護膜がアモルファスシリコン膜であることを
特徴とする請求項1または2記載のpin型アモルファ
スシリコン太陽電池。 4、アモルファスシリコンゲルマニウムを用いたpin
型アモルファスシリコン太陽電池の製造方法において、 i層の形成にあたり、プラズマパワー密度が0.05W
/cm^3以下で、水素含有量10%以下のガスをプラ
ズマ分解することにより、p層上にアモルファスシリコ
ン膜を成膜した後、 前記アモルファスシリコン膜上にアモルファスシリコン
ゲルマニウム膜を形成したことを特徴とするpin型ア
モルファスシリコン太陽電池の製造方法。[Claims] 1. In a pin-type amorphous silicon solar cell using amorphous silicon germanium as the i-layer, between the p-layer and the amorphous silicon germanium film,
An amorphous silicon solar cell characterized by having at least one protective film resistant to hydrogen gas. 2. In an amorphous silicon solar cell comprising at least a p-layer, an i-layer, an n-layer, and a substrate, the i-layer comprises at least an amorphous silicon germanium film and a protective film resistant to hydrogen gas, and the protective film is made of the amorphous silicon. A pin-type amorphous silicon solar cell characterized by being located closer to the substrate than the germanium film. 3. The pin type amorphous silicon solar cell according to claim 1 or 2, wherein the protective film is an amorphous silicon film. 4. Pin using amorphous silicon germanium
In the method for manufacturing type amorphous silicon solar cells, when forming the i-layer, the plasma power density is 0.05W.
/cm^3 or less and an amorphous silicon film is formed on the p layer by plasma decomposition of a gas with a hydrogen content of 10% or less, and then an amorphous silicon germanium film is formed on the amorphous silicon film. A method for manufacturing a pin-type amorphous silicon solar cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2008231A JP2644901B2 (en) | 1990-01-19 | 1990-01-19 | Method for manufacturing pin type amorphous silicon solar cell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2008231A JP2644901B2 (en) | 1990-01-19 | 1990-01-19 | Method for manufacturing pin type amorphous silicon solar cell |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH03214676A true JPH03214676A (en) | 1991-09-19 |
| JP2644901B2 JP2644901B2 (en) | 1997-08-25 |
Family
ID=11687388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2008231A Expired - Fee Related JP2644901B2 (en) | 1990-01-19 | 1990-01-19 | Method for manufacturing pin type amorphous silicon solar cell |
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| Country | Link |
|---|---|
| JP (1) | JP2644901B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002083984A (en) * | 2000-09-08 | 2002-03-22 | National Institute Of Advanced Industrial & Technology | Solar cell and method of manufacturing the same |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59107574A (en) * | 1982-12-13 | 1984-06-21 | Agency Of Ind Science & Technol | Manufacturing method for amorphous silicon solar cells |
| JPS6249672A (en) * | 1985-08-29 | 1987-03-04 | Sumitomo Electric Ind Ltd | Amorphous photovoltaic device |
| JPS6461907A (en) * | 1987-09-02 | 1989-03-08 | Hitachi Ltd | Formation of amorphous semiconductor alloy |
-
1990
- 1990-01-19 JP JP2008231A patent/JP2644901B2/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59107574A (en) * | 1982-12-13 | 1984-06-21 | Agency Of Ind Science & Technol | Manufacturing method for amorphous silicon solar cells |
| JPS6249672A (en) * | 1985-08-29 | 1987-03-04 | Sumitomo Electric Ind Ltd | Amorphous photovoltaic device |
| JPS6461907A (en) * | 1987-09-02 | 1989-03-08 | Hitachi Ltd | Formation of amorphous semiconductor alloy |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002083984A (en) * | 2000-09-08 | 2002-03-22 | National Institute Of Advanced Industrial & Technology | Solar cell and method of manufacturing the same |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2644901B2 (en) | 1997-08-25 |
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