A method of manufacturing solar cells, more in particular thin film solar cells, and solar cells obtained by using such a method.
The present invention relates to a method of manufacturing solar cells, more in particular thin film solar cells, comprising a substrate on which a structure consisting of one ore more layers is provided, which method comprises the steps of: i) placing the substrate into a deposition chamber; ii) placing one or more targets into said deposition chamber for the purpose of depositing on the substrate a layer consisting of a compound of several elements, namely copper-indium-sulphur (CuInS2) or a related compound wherein indium (In) can be replaced entirely or partially for gallium (Ga); iii) generating a sub-atmospheric pressure in said deposition chamber; and iv) irradiating said target(s), using a pulsed laser, in order to form a layer of target material on said substrate. The present invention furthermore relates to solar cells obtained by using the method according to the present invention.
The manufacture of solar cells by means of a pulsed laser is known per se from the article "Laser Ablation Deposition of CuInSe2 Thin Films on Silicon and Fused Silica" by J. Levoska et al , Jpa. J. Appl. Phys. Vol.32 (1993) suppl .32-3, pp.43-44. According to a method described therein, CuInSe2 thin films were deposited by an in situ process on fused silica and single crystal silicon substrates by means of an eCi excimer laser focussed on a polycrystalline target. A temperature of more than 350 °C is required for obtaining a satisfactory crystal quality, whereby it is also stated in said article that the substrate material and orientation had an effect on the structure of the films.
A similar method of manufacturing thin films for solar cells is known from the article "Preparation and properties of laser evaporated CuGa01In09Se2 thin films" by I.V. Bodnar et al, Thin Solid Films 207 (1992) Jan. 30, 54-56. According to the method described therein, CuGa01In09Se2 films having a thickness of 0.3 - 1.5 μ were deposited on a glass substrate, whereby the substrate temperature was 100 - 350 °C, in particular 250 °C, followed by annealing in air at 220 °C for 30 minutes for the purpose of improving the crystal structure thereof.
The manufacture of solar cells by means of a pulsed laser is also known from the article "Photoelectric properties of laser- deposited p-CuInSe2 layers and structures based on them" by Zaretskaya et al, Journal of Applied Spectroscopy, Vol.60, Nos.3-4, 1994. Thus, CuInSe2 films were deposited on glass substrates in an oxygen atmosphere at a temperature of 620 K, preferably 570 - 590 K, by means of a pulsed laser.
The manufacture of solar cells by means of a pulsed laser is furthermore known from the article "Optical transitions in laser- evaporated thin CuInSe2 films" by V.V. Kindyak et al, Thin Solid Films, 240 (1994) 114-115. According to such a method, CuInSe2 films were deposited in a thickness of 0.6 μm on glass substrates at an optimum substrate temperature of 375 °C in a vacuum chamber.
The manufacture of solar cells by means of a pulsed laser is furthermore known from the article "CuInSe2 thin film solar cells by pulsed laser deposition" by H. Dittrich et al , 23 D IEEE Photovoltaic Specialists Conference, May 1993, Louisville, USA, 617-620. Thus, CuInSe2 thin films were deposited on substrates of soda lime glass and Corning 7059 glass, with and without Mo coating, at a substrate temperature of 500 °C, using a pulsed Nd:YAG laser. The manufacture of solar cells by means of a pulsed laser is furthermore known from the article "Pulsed laser deposition and characterization of CuInSe2 thin films for solar cell applications" by R. Schaffler et al , Material Science Forum Vols.173-174 (1995), pp.135-140. The substrates used, in particular glass, were provided with CuInSe2 thin films at a temperature of 520 - 580 °C, using an Nd:YAG laser.
Such a method of manufacturing solar cells is also known from European patent application No.0581833. According to said method, a glass substrate is placed on a rotatable, generally cylindrical supporting element, which is disposed in a vacuum chamber. The substrate is heated to a temperature of 300 - 600 °C, rotated, and selenium, copper and indium are separately precipitated on the substrate by vapour deposition. During the rotation of the cylindrical supporting element on which the substrate is present, the basic elements selenium, copper and indium are precipitated on the substrate by vapour deposition, whereby the sources of the starting materials copper and indium are passed through the rotating, cylindrical supporting element in axial direction. The location of the source of the starting material selenium is not critical thereby. One drawback of such a method is the fact that the substrate must
be heated to a temperature of at least 300 °C, which rules out the use of thermally instable materials. In addition, the composition of the CuInSe2 layer on the substrate is liable to change, which has an adverse effect on the electric efficiency of the solar cell. Another method of manufacturing solar cells as referred to in the introduction is known from European patent application No. 0 502 148. According to the method described in said European patent application, a CuInSe2 layer is deposited on a metal substrate using electro-deposition technique. First, binary Cu-In layers are electroly- tically deposited in a galvanic bath with a base of sulpha ate, in which Cu and In ions are present and in which the element Se is present in the form of Se-powder, whereby selenium is finely dispersed into the aforesaid binary alloy by dispersion electrolysis. In order to obtain the desired ternary CuInSe2 alloy, the substrate and the layers applied thereto must be subjected to a thermal -chemical reaction. One drawback of this method is the fact that the suspended Se powder in the galvanic bath tends to settle, as a result of which the composition of the CuInSe2 layer on the substrate material will be liable to change. Another drawback is the fact that said method requires two steps, namely the galvanic deposition and the subjection to a heat treatment, so that from an economic point of view this method is not very suitable for mass production.
The object of the present invention is to provide a method which overcomes the aforesaid drawbacks, and wherein the choice of substrate is not critical. In addition to that it is desirable to deposit the layer of copper-indium-sulphur or a related compound as referred to in the introduction in a reproducible, possibly continuous process, wherein any impurities in the starting material do not affect the composition of the layer of copper-indium-sulphur or a related compound as referred to in the introduction, which is to be applied by deposition. The method as referred to in the introduction is according to the present invention characterized in that as the substrate a material which is flexible at ambient temperature and one or more targets selected from the group consisting of Cu, In, S and Ga and/or alloys thereof are used, wherein steps i) - iv) are carried out in a continuous process, wherein a strip of the substrate present on a roll is led into said deposition chamber, the strip is provided with the layer of target material in said deposition chamber, after which the substrate strip
provided with the layer of target material is removed from the depositon chamber.
The deposition of layers on a substrate material by means of a laser is known per se from International patent application 0-93/12537. Accordingto the method described in said international patent application, however, asolarcell is fabricatedwherein the characteristic layers are built up of amorphous germanium or amorphous silicon. A layered structure of solar cells as referred to therein is essentially different from the layered structure for the solar cells obtained by using the method according to the present invention, which solar cells comprise a layer of copper-indium-sulphur or a related compound. Surprisingly, the energy efficiency of a solar cell consisting of a layer of copper-indium-sulphur or a related compound is higher than that of a solar cell which is built up of amorphous germanium or amorphous silicon. Said international patent application moreover does not provide any indication that copper-indium- sulphur or a related compound can be applied to a substrate, in particular a substrate which is flexible at ambient temperature, in a continuous process by means of laser deposition.
In a preferred embodiment of the method of manufacturing solar cells according to the present invention, a Cu-In-S alloy is used as the target in step ii). When such an alloy is used, it is possible to transfer this alloy quantitatively to the substrate in substantially the same composition by means of the pulsed laser. Thus it is possible, by selecting a special target, to reproducibly transfer a desired composition of copper-indium-sulphur or a related compound to the substrate.
In another embodiment of the method according to the present invention, it is preferred to use targets of the individual elements selected from the group consisting of Cu, In, S and Ga, for example Cu, In and S, as individual elements rather than as an alloy of Cu, In and S in step ii), and subsequently deposit a layer of target material on the substrate by means of a pulsed laser. After the substrate has been provided with the individual elements, the aggregate is heated in step v) to the temperature at which an alloy is formed. Said temperature level depends on the elements deposited by means of the pulsed laser and on the alloy to be formed with said elements, and it can be determined in a simple manner by a person skilled in the art by carrying out routine experiments. It should be noted, however, that the temperature which is used in step v) must not lead to decomposition or disturbance of the
substrate. The preferred embodiment discussed above is not limited to the individual application of the elements selected from the group consisting of Cu, In, S and Ga. but it is for example also possible, in the embodiment wherein a CuInS2 layer on the substrate is desired, to irradiate an alloy of Cu and In as a first target, and to irradiate S as a second target, after which the aggregate is heated in step v) for the purpose of forming the intended CuInS2 layer on the substrate.
Experiments have shown that the layer of CuInS2 or a related compound which has been deposited by means of pulsed laser deposition may exhibit so-called micro interspaces, which leads to a reduced light trans ittance and a shorter life, which is undesirable in practice. The presence of such defects can be reduced in that the target also contains impurities such as boron, phosphor or carbon besides the desired elements. The irradiation of the target by means of the pulsed laser is preferably carried out in a hydrogen-containing atmosphere. The laser beam functions to photodissociate H2, as a result of which free radicals and other activated species are formed for the deposition. Furthermore it is desirable to generate a sub-atmospheric pressure in the deposition chamber in order to minimize contamination.
With the method according to the present invention, a material which is flexible at ambient temperature, in particular a thermoplastic plastic material, in particular polyimide. polyethylene terephthalate or PEN, is used as the substrate. Polymers of this kind are readily available on an industrial scale and they bond excellently to the layers to be applied. The use of a flexible substrate provides a very wide range of applications of the solar cells obtained with the present method. The flexible substrate material can be used on all kinds of surfaces, irrespective of their shapes and dimensions. In addition, the substrate material can be simply processed into substrate materials of smaller dimensions, so that there are no limitations to their use for generating electricity. It is also possible, however, to use a metal as the substrate, whereby the thickness of the metal is such that the substrate will be flexible at ambient temperature. A preferred material is steel, whereby a thickness of less than 3 mm is required. Another preferred substrate is copper, which conducts electricity very well, whereby the thickness of the copper must be less than 3 mm in order to ensure the flexibility
thereof. The substrate generally comprises a layer of Mo which is applied thereto, which may or may not be done by means of laser deposition.
Experiments have shown that an improved bond between the substrate and the layer of target material deposited thereon is obtained if the substrate is heated before step iv) is carried out. The temperature of the substrate is not critical, but it must be selected so that the substrate is not adversely affected, for example as a result of decomposition or cracking.
The output of the laser is adjusted so that the desired energy density on the target surface is obtained, preferably approximately 3 - 6 joule/cm2. The energy density must not be too low, because evaporation must take place from the target surface in order to obtain a desired thickness of the layer of target material on the substrate. On the other hand, the energy density must not be too high either, because this would cause the target material to deposit on the substrate in the form of large particles, which would result in a very rough microstructure on the substrate, which leads to poor electric conductivity.
In a preferred embodiment of the method of manufacturing solar cells according to the present invention, it is preferred to use a laser pulse frequency of about 12 - 50 Hz. If the laser pulse frequency is too low, the build-up of the layer of target material on the substrate will take place slowly. If on the other hand the laser pulse frequency is too high, this will have a negative influence on the evaporation process which takes place on the irradiated target, which will result in an irregular structure of the layer which is being formed on the substrate.
Steps i) - iv). and possibly step v), are carried out in a continuous process, wherein a strip of a substrate present on a roll is led into the deposition chamber. The strip is then provided with the layer of target material in a continuous process, after which the substrate strip provided with the layer of target material is removed from the deposition chamber, and. in the embodiment which comprises step v), is furthermore heated and possibly wound into a roll again. Preferably, the substrate strip provided with the layer of target material is provided with a so-called window layer, viz. a transparent layer of electrically conductive oxide, preferably ZnO. Other preferred oxides are indium tin oxide (ITO). gallium indium oxide (Galn03), Ti02 and TaOx. When indium tin oxide, for example, is to be applied by means of laser deposition, it is desirable to use a sintered mixture of ln203 and Sn02 as the target. Gallium
indium oxide exhibits a better transmittance over the entire wave length spectrum than indium tin oxide, so that the former is preferred.
In certain embodiments it is preferred to use zinc oxide doped with an element from the group III B (Ga, Al , B or In) of the Periodic System as the electrically conductive oxide. In particular aluminium doped zinc oxide exhibits great thermal stability, and the average transmittance in the visible part of the spectrum is higher than 90$. A suitable target is ZnO doped with 2 % by weight of A1203. If smooth surfaces are required, it is preferred to use gallium doped zinc oxide, whereby the average transmittance in the visible spectrum is 82$, however. A suitable target is ZnO doped with 7 % by weight of Ga203.
The deposition of such an oxide layer preferably takes place by irradiation of an oxide target with a pulsed laser. After the layer of CuInS2 or a related compound as referred to in the introduction has been deposited, a buffer layer of CdS is usually applied, after which the transparent layer of electrically conductive oxide, in particular ZnO is applied. The deposition of such a buffer layer preferably takes place by means of a pulsed laser. In certain embodiments it is desirable to use CuS as the buffer layer. A CuS buffer layer provides a better bond to a Cu-containing layer of CuInS2 deposited by laser deposition or to a layer of a related compound than does a CdS buffer layer. After the layer of an electrically conductive oxide has been deposited, an anti-reflective upper layer, in particular a layer of MgF2. may be applied on top of said layer, preferably by means of a pulsed laser. Other materials which can be suitably used for the anti -reflective layer are Ti02 and silicium nitrides.