AU722932B2

AU722932B2 - Photovoltaic element and method for producing the same

Info

Publication number: AU722932B2
Application number: AU61893/98A
Authority: AU
Inventors: Akio Hasebe; Hirofumi Ichinose; Tsutomu Murakami; Satoshi Shinkura; Yukie Ueno
Original assignee: Canon Inc
Current assignee: Canon Inc
Priority date: 1994-11-04
Filing date: 1998-04-15
Publication date: 2000-08-17
Anticipated expiration: 2015-11-01
Also published as: AU6189398A

Description

i S F Ref: 317790D1

AUSTRALIA

PATENTS ACT 1990 COMPLETE SPECIRCATION FOR A STANDARD PATENT

ORIGINAL

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Name and Address of Applicant: Actual Inventor(s): Canon Kabushlki Kaisha 30-2 Shimomaruko 3 chome Ohta-ku Tokyo 146

JAPAN

Hirofumi Ichinose, Aklo Hasebe, Tsutomu Murakami, Satoshi Shinkura and Yukle Ueno.

Spruson Ferguson, Patent Attorneys Level 33 St Martins Tower, 31 Market Street Sydney, New South Wales, 2000, Australia Photovoltaic Element and Method for Producing the Same

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Address for Service: Invention Title: The following statement is a best method of performing it full description known to me/us:of this invention, including the 5845 Photovoltaic Element and Method for Producing The Same BACKGROUND OF THE INVENTION Field of the Invention The present invention relates to a photovoltaic element for a solar cell, a photo sensor and others, and a method for producing the same.

Related Background Art 1. 0 Solar cells applying photovoltaic elements are expected as an alternative energy source for existing power generation of fired power generation and .hydroelectric power generation solving the problems of these conventional power generation. In particular, 15 various studies have been made on amorphous silicone solar cells, because the cells can be made relatively at low cost and can be produced as the elements that have larger area than solar cells using crystalline solar cell elements. Improvement of the photoelectric conversion efficiency of amorphous silicone solar cells is one of important problems for commercializing the amorphous silicone solar cells. Studies have been made ardently for solving the problems as shown hereunder.

The structure of amorphous silicone solar cell elements is known in which back electrode, semiconductor layer and incident surface electro de are laminated in this order on a conductive substrate such 2 as stainless plate. The incident surface electrode is made, for example, by transparent conductive oxides.

Furthermore, a collector electrode comprising fine metallic wire is placed on the incident surface electrode mentioned above for collecting the generated electricity. The collector electrode mentioned above is provided on the incident surface; consequently it reduces effective generating area of the solar cell.

The area loss is called shadow loss. For this reason, the collector electrode mentioned above is usually made in a fine comb shape. Thus, the shape of the collector electrode normally tends to be fine and long shape, and the selection of material and the design of cross sectional shape are required so as to make the electric resistance small.

o oooo ~An electrode called bus bar electrode is formed on the surface of the collector electrode mentioned above, for collecting the electric current that is collected ooo o by the collector electrode. The bus bar electrode is made from metallic wire that is thicker than the wire of the collector electrode.

Now, the present situation of the research is explained for minimizing shadow loss and loss by electric resistance and for improving the conversion efficiency of solar cell that is constructed as described above.

Materials that have small resistivity such as 3 silver (1.62 x 10- 6 Qcm) or copper (1.72 x 10 6 Qcm) are used for the above mentioned collector electrode to reduce the shadow loss and electric resistance loss.

Vacuum evaporation, plating and screen printing are used as the method to form the collector electrode.

The vacuums evaporation method has problems such as slow sedimentation, low through put, caused by the use of vacuum process, and necessity of masking to form "the linear pattern, and also the masking results in the 10 loss of metal, sediment on the masked portion. The problem in the screen printing is the difficulty forming low resistance electrode.

For example, the resistivity of the lowest resistance of conductive paste is about 4.0 x 10 5 Qcm 15 this is the value one order higher than that of bulky o o [.pure silver, this means resistance of the paste is larger than that of the silver in one order. The following three methods are used to reduce the resistance without area reduction of the collector electrode using such a material.

Increasing the thickness of the electrode. In this case, practically usable upper limit of the thickness is 10 pm to 20 pm. When this thickness of electrode is used to form a long, for example more than 10 cm, collector electrode, it is necessary to make the width of the electrode more than 200 pm in order to keep the electric resistance loss small, and the Aspect ratio -4- (ratio of thickness and width) becomes small value such as 1:10, and the shadow loss becomes larger.

A coated wire for a collector electrode that is made by coating a metallic wire with a conductive particle containing polymer is proposed in USP 4,260,429 and USP 4,283,591. The cross section of the coated wire for collector electrode proposed in the USP 4,260,429 is shown in Fig. 1A. In this figure, reference numeral 101 is a metallic wire, and reference numeral 102 is a coated layer made of the conductive polymer. This invention has a merit that even the long electrode that is made using the copper wire has small electric resistance loss, and the shadow loss is also small because theAspect ratio can be made small value 1:1. The security of the collector electrode proposed in the USP 4,260,429 is that the wire can be fixed by a simple method using conductive adhesive. A method to prevent physical contact between the metallic electrode and Cu 2 S layer is proposed in USP 4,283,591, this method provides prevention of the metallic copper deposition.

However, these proposals have following problems.

0 20 In the case of USP 4,260,429.

A) Following problems were found by a long term exposure- test or by temperature-humidity tests that short circuit between upper electrode and lower electrode is formed in a defective part such as pin hole or short circuit; lower conversion efficiency 0 [R:\LIBE]02746.doc: avc 5 results from the small shunt resistance, tends to get worse yield. Experiments by the present inventors showed that the problem comes from electro-chemical reaction in which the ion component of the above mentioned metallic wire diffuses through the conductive polymer and reach the above mentioned semiconductor element.

B) The electrode disclosed by USP 4,260,429 proposes to get good electro-conductivity between the 10 metallic wire and the semiconductor element, and the •solution of the problem that the occurrence of the trouble by the electro-chemical reaction between the metallic wire and the semiconductor element is not included.

15 C) The electrode disclosed by USP 4,260,429 has a problem that some portion of the electrode may have not enough bonding force. In some occasion, tub of some metallic material almost did not have enough bonding force when the adhesive connection between the solar cell substrate and metallic tub of the collector electrode was required.

D) Not only initial bonding force but constant bonding force between the electrode and the solar cell is required for the solar cell used in open atmosphere in severe condition. The solar cell that used electrode described above had a problem that the series resistance increase and the conversion efficiency 6 decrease caused by the deterioration of the bonding force occurred during the temperature-humidity test and the heat resistance test as the acceleration-test.

E) Some problems of peeling off were observed on the solar cell caused by the lack of initial bonding force between the solar cell substrate and metallic tub, and also by degradation of the bonding force between the cell element, metallic wire and the coating layer, affected by the humidity and temperature.

i0 F) The solar cell was affected easily by the oo humidity because tight covering layer was not formed as the covering film.

G) It is desirable that the covered wire electrode Scan be manufactured in off line and be used from the 15 storage, however, in the case where thermosetting resin was used the above mentioned electrode had a problem that it was difficult to obtain the enough bonding force when it was formed on the solar cell because the cure acceleration of the polymer after the drying up was difficult to control. Furthermore there was no means on the selection of the curing agent to cure the thermosetting resin and relatively long curing time was required.

H) When only thermoplastic resin was used, deformation of the electrode occurred caused by the thermo-hysteresis during the lamination process after the formation of the electrode, and the following 7 problems were observed, line width change, partial peeling and position shift of the electrode.

I) For the solar cell that is used in open atmosphere, it is required that there is no change in the bonding force between the electrode and the solar cell element even if it is used for long term in severe condition. The solar cell that used above mentioned electrode had a problem that series resistance increase and conversion efficiency decrease caused by the 10 deterioration of the bonding force during long time ooo open air exposure test or temperature-humidity test as the acceleration test.

In the case of USP 4,283,591.

A) Although the idea to prevent physical contact 15 between metallic electrode and semiconductor layer was oo disclosed, but the solution of the problem, in which the metallic ion diffuses slowly through the conductive polymer and induces trouble, was not proposed.

B) The electrode proposed by this invention has the possibility that the metallic wire may contacts with the solar cell substrate as the result of breakage of the above mentioned covering layer during the thermal crimp process. The concrete counter measure of this problem is not proposed.

C) The proposal has some limit in the electrode formation because the procedure do not contain drying process and the covered wire can not be stored.

8 In the cases of USP 4,260,429 and USP 4,283,591.

A) Either proposal has the problem that it is difficult to get covering layer of uniform thickness and stable good electric conductivity.

B) Short circuit between upper electrode and lower electrode is formed when the covering layer has pin hole that induces large enough leak current. As the result the shunt resistance decreased, lower conversion a. efficiency is resulted and the yield was decreased.

1 C) The electrode proposed by the invention has the possibility that the metallic wire may contacts with the solar cell substrate, and when it is used outdoors enough effect of migration and shunt closure was not ":'obtained.

In the case of USP 5,084,104.

A) Short circuit between upper electrode and lower ••co electrode is formed when an amorphous silicone solar cell that has defective part such as pin hole or short circuit was used, and lower conversion efficiency is resulted from the small shunt resistance, tends to get worse yield.

B) Series resistance of the electrode that is covered by conductive adhesive increases by thermohysteresis because of the solution or the softening of the electrode caused by the penetration of the paint solvent.

C) The series resistance of the photovoltaic -9element increases and the conversion efficiency decreases when it is tested by open air exposure test or temperature-humidity test as the acceleration test.

SUMMARY OF THE INVENTION An object of the present invention is to provide a coated wire with a collector electrode that has excellent storability, adhesiveness, and resistance to leak due to humidity.

I0 It is desirable to provide a photovoltaic element that has high initial characteristic and long term reliability, using the above mentioned collector electrode, that can avoid short circuit between the upper electrode and lower electrode, can avoid penetration of the paint solvent to the electrode covered by the conductive adhesive, and can prevent the increase of resistance in series.

It is also desirable to provide a manufacturing process that can make the photovoltaic element in a high yield and in stable operation.

According to one aspect of the present invention, there is provided a coated wire with a collector electrode, said coated wire comprising: a metal wire coated with a coating layer of a conductive adhesive and formed to adhere to a photovoltaic element through said coating layer, wherein the coating layer is for preventing a metal ion of said metal wire from migrating into a light incident surface of a photoelectric conversion layer of said photovoltaic element.

[R:\LIBE]02746.doc:avc According to another aspect of the present invention there is provided a coated wire for a collector wire, said coated wire comprising: a metal wire with a coating layer of a conductive adhesive bonded4through said s coating to a photovoltaic element, wherein said coating layer comprises at least two layers.

a [R:\LIBE]02746.doc:avc -11 BRIEF DESCRIPTION OF THE DRAWINGS Figs. 1A and 1B are schematic cross-sectional views illustrating composition of a collector electrode that is provided with a coating layer on the metal wire, according to this disclosure.

Figs. 2A, 2B and 2C are schematic cross-sectional views illustrating composition of a collector electrode having a plurality of coating layers and the fixation condition of the collector electrode on to a substrate.

Fig. 3 is a schematic cross-sectional view illustrating for a wire coat device used for manufacturing a collector electrode of this disclosure.

Figs. 4A, 4B and 4C are schematic cross-sectional views illustrating composition of a solar cell of amorphous silicon type, according to this disclosure.

Fig. 5 is a schematic cross-sectional view illustrating composition of a solar cell of single *oo• [R:LIBE]02746.doc:avc -12crystal silicon type, according to this disclosure.

Fig. 6 is a schematic cross-sectional view illustrating composition of a solar cell of polycrystal silicon type, according to this disclosure.

Fig. 7 is a schematic cross-sectional view illustrating composition of a thin film solar cell of polycrystal silicon type according to this disclosure.

Figs. 8A and 8B are schematic plan views illustrating composition of a solar cell that is an example of the photovoltaic element according to the present invention.

Fig. 9 is a schematic cross-sectional view illustrating composition of a photovoltaic elements module using a collector electrode having two layers coating, according to this disclosure.

Fig. 10 is a schematic cross-sectional view illustrating composition of a photovoltaic elements module using a collector electrode having two or three layers coating, according to this disclosure.

Fig. 11 is a schematic cross-sectional view illustrating composition of a photovoltaic elements module using a collector electrode having three layers coating, according to this disclosure.

25 Fig. 12 is a graph showing the relationship between volume resistivity and conversion efficiency in [R:\LIBE]02746.doc:avc 13 a module of photovoltaic elements according to this disclosure.

Fig. 13 is a schematic plan view illustrating composition of another module of photovoltaic elements using a collector electrode having the coating layer, according to this disclosure.

Fig. 14 is a graph showing the relationship between steaming cycles and series resistance for a module of photovoltaic elements according to this disclosure.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS According to experiments conducted by the inventors, the problem arising in the formation of the 15 existing collecting electrode, during the process 0* following the coating and drying of the wire; in environments where light and moisture are present; was found to be caused by electromotive force being applied to the collecting electrode, thereby diffusing ions 20 from the metal wire to the conductive resin layer.

Also, the problem of shunt with the existing collecting electrode formation was found to be caused by the possibility that the metalwire could contact the o *semiconductor layer or the transparentconductive film, because the conductive resin coating consisted of only one layer. In other words, it is not possible, with the existing collecting electrode, to prevent the metal -14wire from directly contacting the semiconductor layer without the inclusion of conductive resin during the thermocompression bonding process and therefore, it was found that contact of the faulty area and the wire was the cause of the initial decrease' in yield. In addition, we have discovered that, even if such contact was prevented, metal ion diffusion occurred during actual usage, because of minute pores in the conductive resin, as well as the moisture and ion permeability of the resin itself. We have also discovered that the problem of long-term dependability was attributed to the deterioration of conductivity with the conductive resin, caused by oxidation of the metal wire surface (consisting of copper, etc.), which is caused by moisture penetrating during outdoor use, because the polymer used in solar batteries laminated with polymer is not perfectly watertight.

We have also found out that it is problematic that the bridging density of the conductive resin layer could not be controlled regarding the shelf life and adhesive strength of the coated wire for collector electrode. In other words, the problem was that, when curing resin is used in polymers that form the conductive resins of the existing coated wire for collector electrode, the resin would harden after drying, for example during storage, while the use of thermoplastic resin was also a problem because the •fluidity would become too large from the heat history a a [I:\DayLib\LIBE02746a.doc:jls 15 of later processes, because the resin will not bridge.

Furthermore, low resistance copper and aluminum wires used in wiring for electric appliancesare inexpensive and good conductors. Enamel wires, etc.

are made by coating these metal wires with insulating varnish, but generally, it is not easy to coat metal, which are inorganic, with material that contains organic material. In addition, sufficient adhesive S•strength may not be obtained when adhering the wire, through the coating layer, to semiconductors and metals. This is because a special bond does no exist between the organic material in the coating layer and *.the semiconductor or metal material. This problem becomes even more pronounced depending on the metal 15 material and its surface conditions, and we have •go• discovered that almost no adhesive strength can be obtained when they are affected by moisture.

As a result of studies by the inventors of this oooro invention aimed at tackling these problems, we have discovered that good adhesion, offering good storage characteristics with no progressive curing after the heat/drying process, can be achieved without altering the shape of the electrode by using a curing agent, such as block isocyanate, etc. to control the bridging density of the conductive resin layer before and after the process of forming the electrode on the surface of the solar cell.

-16- We were able to create solar batteries of good characteristics by dividing the coating layer into multiple layers, where each layer will be assigned different jobs, such as preventing moisture and ion permeation, and the adhesion of the metal- wire to the semiconductor layer or the transparent electrode.

Also, by creating a coating layer consisting of polymer containing a coupling agent and conductive filler, the surface of the metal was altered in such a way that it will readily adhere to organic material, whereby a good adhesion between the metal and the conductive resin layer containing organic material was achieved based on the knowledge of this invention.

Next, we will describe the constitutive characteristics of the embodiment of this invention, as well as the interactive effects based thereon.

With regard to the coated wire for collector electrode on which a metal wire; coated with a layer consisting of photovoltaic element through the layer of coating, S S we have prevented the metal ions in the metal wire to diffuse into the semiconductor layer of the photovoltaic element. As a result, we were able to prevent the short circuiting of the metal wire and the semiconductor layer of the photovoltaic element, which causes deterioration of the photovoltaic element's exchange efficiency.

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[R:\LBE102746.doc:avc 17 Because the coating layer possesses the property of preventing the diffusion of the metal ions, it becomes possible to prevent the deterioration of the photovoltaic element's exchange efficiency caused by the short circuiting of the metal wire and the semiconductor layer of the photovoltaic element, even if the metal wire is applied with a voltage that is greater than the photovoltaic element's eiectromotive force, regardless of the voltage which is applied on S 10 the metal wire.

.999 Because the conductive adhesive consists of oe conductive particles and polymer, the resistivity of the conductive adhesive can be variably adjusted between 0.1 Qcm and 100 Qcm.

15 The surface of the metal, for example, a eeoc metal wire, is altered in such a way that it is readily bonded to organic material and therefore providing a good adhesion between metals and conductive resin containing organic material, because the conductive adhesive consists of a coupling agent, conductive particles and polymer.

Since one of the following; silane based, titanate based and aluminum based coupling agents; will be chosen as the coupling agent, it is possible to control the interface between dissimilar material. In other words, it will act as a medium between the inorganic material (metal) and the organic material 18 (binder resin included in the conductive resin), to form a strong bond between the two.

Because we have determined the space ratio of the conductive adhesive to be 0.04ml/g or less, at a space radius of 1 pm or less, we are able to avoid short circuits caused by the ionization and migration of silver in the conductive adhesive.

Because the numeric mean molecular weight of o, the polymer ranges from 500 to 50,000, it is possible 10 to prevent diffusion of the metal ions.

Because the gel rate of the polymer ranges from 20% to 100%, it is possible to control deformation and dislocation of the electrode even when heat history is applied after the electrode is formed. As a result, 15 it becomes possible to prevent diffusion of the metal OeO0 ions.

Because the layer of coating consists of two or more layers and the conductive adhesive which makes up all inner coating layers, other than the outermost layer, consist of the polymer, it is possible to assign different tasks; such as prevention of moisture and metal ion permeation, and the adhesion between the metal wire and the semiconductor layer or the transparent electrode; to different layers.

(10) Because the layer of coating consists of two or more layers and conductive adhesive which makes up the outermost layer consists of an uncured 19thermoplastic polymer, the coated wire for collector electrode can be stored, providing sufficient adhesive strength when curing is completed during the formation of the electrode on the photovoltaic element. As a result, we were able to prevent deformation of the electrode that cause changes in line width, partial peeling or positional dislocation of the electrode, caused by heat history during processes, such as lamination following the formation of the coated wire for collector electrode.

(11) Because the conductive adhesive consists of two or more layers and because the softening point of the conductive adhesive making up the layer closest to the electrode is set higher than the maximum temperature of the heat history applied to the photovoltaic element during the manufacturing process, we are able to prevent melting or peeling during the formation of the moisture protection layer, or deformation or peeling during lamination.

(12) Because we have limited the resistivity range of the conductive adhesive to 0.1 Qcm to 100 Qcm, it possesses a preventive function against shunt and we were able to reduce the electric resistance loss to negligible levels.

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20 (13) Because at least one of the following: urethane, phenoxy, epoxy, butyral, phenol and polymide, will be chosen as the polymer, a we are able to choose the desired hardness of the resin from a wide [I:\DayLib\LIBE]02746a.docjIs range. As a result, the metal wire can be coated readily, workability is good, good flexibility is provided and it can be heat cured. As a result, durability is improved.

(14) Because we have selected block isocyanate as the curing agent to be contained in the conductive adhesive, we are able to control the bridging density of the conductive adhesive, before and after the formation of the electrode on the photovoltaic element. As a result, the coated wire for collector electrode is easy to handle and guarantees stability during storage. Furthermore, the process of applying the conductive adhesive to the coated wire for collector electrode can be operated at low costs.

Because the glass transition point of the conductive adhesive was specified to be 100 degrees centigrade or higher, the permeation of paint solvents into the electrode coated with conductive adhesive when compression bonding the electrode coated with conductive adhesive to the cell surface of the photovoltaic element, can be prevented.

(16) Because the average diameter of the primary particles of the conductive particles was limited to a range of 0.02 ptm to 15 gm, they are smaller than the thickness 20 of the coating and the increase in resistivity caused by the contact between particles can be controlled.

(17) Because we have specified the conductive *o S o oo* po *0• [R:\LIBE]02746.doc:avc -21particles to be at least one of the following: graphite, carbon black, In203, TiO 2 SnO 2 ITO, ZnO or a substance that is created by adding to these a dopant consisting of tervalent metal elements, it was possible to make particles with diameters of 0.02 jtm to 15 gm.

(18) The transparent electrode installed on the semiconductor layer of the photovoltaic element and the conductive adhesive were installed in contact with each other. Thus, on the semiconductor layer, a transparent electrode transparent to a light to be absorbed by the semiconductor layer is provided. Accordingly, for the nonmonocrystalline semiconductor having a greater resistivity in a surface direction, an efficiency is improved in particular.

(19) We obtained a photovoltaic element of good initial characteristics and long term dependability which consists of a semiconductor layer consisting of at least one pin junction or pn junction and a collecting electrode installed on the light entry side of the semiconductor layer, we were able to obtain a photovoltaic element, by means of the collecting electrode consists of the above mentioned collecting electrode.

We were able to obtain a photovoltaic element with an excellent 20 collection efficiency and sufficiently low series resistance, because the semiconductor layer had a transparent electrode on the light entry side and the collecting electrode.

(21) We were able to obtain a photovoltaic element of good initial characteristics and long term dependability, because we have specified at least one of the 2 5 following to be used for the semiconductor layer: monocrystal silicone, polycrystalline S. silicone, thin film polycyrstalline silicone, amorphous silicone, amorphous silicone germanium or amorphous silicone carbon.

(22) Because the semiconductor layer was made into a triple cell, consisting of three layers of cells consisting of pin junction or pn junction, a photovoltaic element of better initial characteristics was obtained.

(23) We obtained the production method of photovoltaic elements with a collecting electrode on the light entry side, that offered good production yield, because [R:\LIBE]02746.doc:avc -22the collecting electrode is adhered to the light entry side of the photovoltaic element with heat and/or pressure.

(24) We were able to obtain a method of producing photovoltaie elements of good initial characteristics and long term dependability, by setting higher the heat applied to the coated wire for the collecting electrode than the dissociation temperature of the block isocyanate, thereby allowing the adhesion and curing of the formed collecting electrode to be completed in a short period of time.

o 0 of *e *t a to a [R:\LIBE]02746.doc:avc -23- We were able to obtain a method of producing photovoltaic elements of long term dependability, which were not affected readily by moisture after-the adhesive formation of the photovoltaic elements, by heating the collecting electrode until the gel rate of the uncured heat curing polymer which forms the coating layer is between 20% to 100%.

The following sections describe the embodiment of this invention.

(Coated wire for collector electrode) Coated wires for collector electrodes, according to this disclosure, are described in Figs. 1A and 1B, and 2A to 2C. The coated wire for collector electrode 100 shown in Fig. 1A is one in which the metal wire 101 is coated with one type of coating layer 102.

The coated wire for collector electrode 200 shown in Fig. 2A is one in which the metal wire 201 is coated with two types of coating layers, namely, first coating layer 202 and S second coating layer 203.

0* 20 It is desirable for the metal wires 101 and 202 composing the coated wire for •collector electrode 100 and 200 to be wire material, for which an industrially stable supply is available. It is also desirable that the material of the metal composing the metal wires 101 and 201, possess a resistivity of 10 4 Qcm or less.

*S0 o•• o oe [R:\LIBE)02746.doc:avc -24- For example, copper, silver, gold, platinum, aluminum, molybdenum and tungsten are suitable for use because of their low electric resistance. Of these, copper, silver and gold are the most desirable for their low electric resistance. The metal wire can also be an alloy of these metals.

If so desired, it is also proper to form thin metal layers 103 and 204, such as those shown in Figs.

lB and 2B, on the surface of the metal wire; for purposes such as corrosion prevention, oxidation prevention, improvement of adhesion with the conductive ~resin and the improvement of electric conductivity.

.*.Candidates for metal layers to be applied to the metal wire surface are precious metals that offer resistance to corrosion, such as silver, palladium, silver and palladium alloy and gold, as well as metals with good ooo• corrosion resistance, such as nickel and tin. Of S" these, gold, silver and tin are not readily affected by moisture, therefore making them suitable for the metal layer. For example, plating and cladding are suitable methods of forming the metal layer on the metal wire surface. It is also possible to create a coating of conductive resin in which the metals are used as fillers and distributed throughout the resin. Though the thickness of the coating will depend on individual preferences, the ideal thickness for metal wires with a circular cross section would be 1% to 10% of its 25 diameter. The ideal resistivity of the metal layer, considering the electric conductivity, effectiveness of corrosion resistance and the thickness of the metal layer, would be 10- 6 Qcm to 100 Qcm.

The cross section of the metal wire can be circular or rectangular and can be chosen depending on preferences. The diameter of the metal wire was designed so that the sum of the electric resistance loss and shadow loss is minimal. In specific terms, a 10 copper wire for enamel wire with a diameter of 25 pm to imm, as indicated in the JIS-C-3203 is suitable for use. It is even more desirable to use diameters of pm to 200 pm to create photovoltaic elements with good photoelectric exchange efficiency. Wires with diameters smaller than 25 pm are prone to breakage, difficult to produce and their power loss is larger.

1* Meanwhile, diameters of 200 pm or more possess larger shadow loss or the surface of the photovoltaic element becomes bumpy, making it necessary to make the filler used on the surface coating layer, such as EVA, thicker.

The metal wire is produced by using a well-known wire drawing machine to mold it into the desired diameter. The wire which has passed through the wire drawing machine is hard, but it will be annealed using a well-known method to meet desired characteristics in stretchability and bendability, and it can be also used -26as a soft wire.

(A coated wire for collector electrode coated with a conductive adhesive consisting of one layer).

An example of "a coated wire for collector electrode coated with a conductive adhesive consisting of one layer" according to this invention is shown in Fig. 1A.

In Fig. 1A, 101 is a metal wire for the electrode and 102 is the coating layer.

The metal wire 101 is the core wire of the collecting electrode, and uses a wire that possesses good conductivity, such as copper wire, silver plated copper wire or silver copper clad wire, in order to reduce power loss. The coating layer 102 is formed from heat curing conductive adhesive or thermoplastic conductive adhesive, and its function is to mechanically and electrically connect the main part of the coated wire for the collecting electrode to the photovoltaic element substrate, through the thermocompression bonding process.

(A coated wire for collector electrode coated with a conductive adhesive consisting of two layers).

An example of "a coated wire for collector electrode coated with a conductive adhesive consisting of two layers" is shown in Fig. 2A.

In Fig. 2A, 201 is a metal wire for the electrode, 202 is the first coating layer and 202 is the second coating layer. The metal wire 201 is the core wire of the coated wire for collector electrode, and uses a wire that offers 0 0 9 [R:\LIBE]02746.doc:avc -27good conductivity, such as copper wire, silver plated copper wire or silver copper clad wire, in order to reduce power loss. The first layer 202 is formed with heat curing conductive adhesive, and protects the electrode metal, and provides mechanical and electrical connection. It also has the function of preventing migration by the electrode metal and controlling the flow of current into defective areas of the photovoltaic element from the coated wire for collector electrode. The second layer 203 is also formed of heat curing conductive adhesive, and its function is to mechanically and electrically connect the main part of the coated wire for collector electrode to the photovoltaic element substrate, through the thermocompression bonding process. And also because it heat cures, it is not readily damaged by paints used in the moisture prevention layer in later processes.

In other words, the first coating layer 202, which is in direct contact with the metal wire 201, is a barrier layer which prevents moisture from reaching the metal wire to prevent corrosion of the metal wire surface, as well as prevent metal ion migration from the metal wire. The second layer 203 is an adhesive layer, which has the functions of adhering the coated wire for collector electrode to the semiconductor layer or transparent electrode and of current collection.

As for polymers included in the conductive 0o 1; 0 0 •oi 0 0o*o *0o 0 *o o *oo° 00* 0 0000 0 [lADayLib\LIBE]02746a.doc:jls 28 adhesive that make up the first layer 202, resins with relatively little permeability are suitable for use among the resins mentioned above. In other words, urethane, epoxy, phenol or heat curing resins created by denaturating these resins are ideal. Also, it is desirable to allow thorough curing after these resins are applied. In addition, it is desirable that the thickness of the first layer be 1 pm to 15 pm, in order .to prevent excessive shadow loss. Thicknesses of under 10 1 pm will make it difficult to create a uniform coating and pin-holes will occur, rendering it insufficient as a barrier. On the other hand, thicknesses of over m are not desirable because they are difficult to peel and shadow loss becomes too great.

As for polymers included in the conductive adhesive that make up the second layer 203, resins with good adhesive properties and good flexibility, in particular are suitable. In other words, urethane, eeme• S"epoxy, phenol or heat curing resins made by denaturating these resins or thermoplastic resins, such as phenoxy, polyamide or polyamideimide would be suitable. In particular, urethane resin is suitable for use because its bridging density is readily adjusted. It is desirable to leave these resins uncured after coating and cured only after the adhesion process is complete. For this reason, block isocyanate is desirable as the polymeric curing agent. This block -29isocyanate has the mechanism of progressively curing when heated above the dissociation temperature.

Therefore, by drying it at temperatures lower than the dissociation temperature, any solvent contained in it can be completely removed, therefore depriving it of its stickiness and tackiness, allowing it to be coiled on a reel for storage. In additional, because curing will not progress unless temperatures exceeding the dissociation temperature of the isocyanate are applied, it will uniformly provide sufficient adhesive strength during the formation of the collecting electrode.

The thickness of the second coating layer will depend on the diameter of the wire. For example, if the diameter of the metal wire is 100 tm, the ideal thickness of the second coating layer would be 5 ptm to 30 -tm; which is a thickness that would have no Is pin-holes, would provide sufficient properties as an adhesive layer and offer no extreme shadow loss.

(A coated wire for collector electrode coated with a conductive adhesive consisting of three layers).

An example of "a coated wire for collector electrode coated with a conductive adhesive consisting of three layers" according to this invention is shown in Fig. 11.

i In Fig. 11, 1101 is the metal wire for the electrode, 1102 is the first coating layer, 1103 is the second coating layer and 1104 is the third coating layer. The metal wire 1101 t 25 is the core wire of the o h oo oeoo• *o o [R:\LIBE02746.doc:avc coated wire for collector electrode, and uses a wire that offers good conductivity, such as copper wire, silver plated copper wire or silver copper clad wire, in order to reduce power loss. The first layer 1102 is formed of heat curing conductive adhesive, and provides electrical connection with the electrode metal. Metallic conductive adhesives would be suitable for the first coating layer 1102, to provide an electrical connection with the electrode metal. The second layer 1103 prevents migration caused by the metal fillers in the metallic conductive adhesive used in the electrode metal and the first coating layer. It also controls the flow of current to defective areas in the photovoltaic element from the io coated wire for collector electrode. The third coating layer 1104 is also formed of heat curing conductive adhesive and its function is to mechanically and electrically connect the main part of the coated wire for collector electrode to the photovoltaic element substrate, through the thermocompression bonding process. And also because it heat cures, it is not readily damaged by paints used in the moisture prevention layer in later Is processes.

(Conductive adhesives and their resistivity) In this invention, the conductive adhesive used to coat the metal wire is made by distributing conductive particles and polymer. The resistivity of the conductive adhesive must be negligible in terms of i 555555 S S [R:\LIBE]02746.do:avc 31 collecting the electric current generated by the photovoltaic element and at the same time, provide adequate resistance to prevent shunt. In specific terms, 0.1 Qcm to 100 Qcm is desirable. When resistance is smaller than 0.1 ocm, the shunt retention function becomes insufficient and when it is greater than 100 Qcm, loss from electric resistance becomes too great.

(Conductive particles) Conductive particles according to this disclosure are pigment which add conductivity. Materials suitable for this purpose are, for example, carbon black, graphite, In 2 0 3 TiO 2 SnO 2 ITO, ZnO and oxide semiconductor material made by adding the appropriate dopant to the material. The diameter of the conductive particles should be smaller than the coating layer to be formed, but if particles are too small the resistance on the contact point of the particles to each other becomes great and making it impossible to 20 obtain the desired resistivity. For these reasons, the suitable average diameter for the conductive particles is 0.02 pm to 15 pm. It is also acceptable to adjust the resistivity and the distribution in the conductive resin by mixing two or more types of conductive *o particles. It is also acceptable to add translucency by using materials, such as ITO, In 2 0 3 TiOz, SnO 2 and ZnO. The usage of ITO produces especially good 32translucency.

The conductive particles and the resin are mixed in suitable ratios to obtain the desired resistivity.

Resistivity will decrease as the amount of conductive particles increase, but the coating layer will loose its stability as the proportion of resin decreases.

And when the polymers are increased, the contact of the conductive particles to each other becomes faulty and will result in high resistance. Therefore, the optimum g. 10 ratio should be determined depending on the polymer and conductive resin used, as well as its desired physical O *0 properties. In specific terms, good resistivity is obtained at volume percentages of the conductive particles ranging from 5% to (Polymer) The suitable resin according to this invention will be one that facilitates coat formation on the metal wire, with good workability, flexibility and weather resistance. Polymers with such characteristics are heat curing resins and thermoplastic resins.

As for heat curing resins, urethane, epoxy, phenol, polyvinyl formal, alkyd resin and resins made by denaturing these materials are examples which are suitable for use. In particular, urethane, epoxy and phenol resins are used as coating material for enamel lines, and are good in terms of flexibility and productivity. They are also suitable as material for -33coated wire for collector electrodes of the photovoltaic element, in terms of weather resistance and adhesion.

As for thermoplastic resins, butyral, phenoxy, polyamide, polyamideimide, melamine, butyral, acryl, styrene, polyester and fluoride are examples of suitable materials. In particular, butyral, phenoxy, polyamide and polyamideimide resins are good materials in terms of flexibility, weather resistance and adhesion, making them suitable for use in coated wires for collector electrodes of photovoltaic elements.

(Coupling agent) In this disclosure, a conductive adhesive consisting of a polymer containing a coupling agent and conductive particles are suitable. The reason why good characteristics are obtained when a conductive adhesion added with a coupling agent is used is described below.

Generally, low resistance copper and aluminum wires used in wiring for electric appliances are inexpensive and good conductors. Enamel wires, etc. are made by coating S. 20 these metal wires with insulating varnish, but generally, it is not easy to coat metal, which are inorganic, with material that contain organic material. In addition, sufficient adhesive strength may not be obtained when adhering (the wire), through the coating layer, to 9 9 Ssemiconductors and metals. This is because a special bond does not exist between the organic material in the coating layer and the f ft** *9*999 f ft f f 9 [R:\LIBE]02746.doc:avc 34semiconductor or metal material. This problem becomes even more pronounced depending on the metal material and its s-rface conditions, and we have discovered that almost no adhesive strength can be obtaine.' when they are affected by moisture.

When the coated wire for collector electrode stated in this invention is used for solar batteries, its coupling agent acts to strengthen the bond between the organic material in the coating layer, with inorganic material, such as the surface of the solar cell substrate or metal tabs of the takeoff electrode. This makes it possible to prevent areas from o0 loosing sufficient adhesive strength. In addition, because the coating layer consists of two or more layers, effectiveness can be improved by determining the type of cApling agents to be used in the inner most side, which is in direct contact with the metal wire, and the outer most layer, which is in direct contact with the solar cell substrate; depending on the material of the metal wire, material of the solar cell substrate, material of the metal tab is and the polymer composing these coating layers. Also, the adhesive strength enhanced by the coupling agents is maintained in high temperatures, high humidity and high temperature/humidity environments, and therefore maintained even when the solar cell is used outdoors. This makes it possible to prevent deterioration of the exchange efficiency caused o* a [I:\DayLib\LI BE]02746a.docjs 35 by the rise in series resistance from the deterioration of adhesive strength between the electrode and the solar cell substrate or metal tab, as well as from peeling.

As the coupling agents used in this disclosure, silane derivative coupling agent, titanate derivative coupling agent and aluminum derivative coupling agent are among those cited. Such a coupling agent consists of a hydrophilic portion which has a mutual function with inorganic material and an organic function group which has a mutual function with organic material. The surface control between foreign materials is the main purpose of the use, particularly its function is based on a covalent bond and in this respect it is different from conventional surface active agents. That is, the coupling agent acts as go-between between a combination of inorganic material (metal) and an organic material (polymer in conductive adhesive) and the two materials are firmly combined. A silane derivative coupling agent is covalently bonded to both the inorganic material and the organic one, however, titanate derivative coupling agent and aluminum derivative coupling sometimes do not form covalent bonds of o" organic material. By changing the polarity and surface energy of the surface of inorganic material, the strength of the bond can be increased. So, it is said that a silane coupling agent is the most effective.

a that a silane coupling agent is the most effective.

36 As silane coupling agents suitable for this invention, the following products are among those cited: y-mercaptoxy propyltrimethoxysilane, y-glycixidpropyltrimethoxysilane, y-(2-aminoethyl) aminopropyltrimethoxysilane, y-(2-aminoethyl) aminopropylmethyldimethoxysilane, aminosilane, y-anilinopropyltrimethoxysilane, vinyltriacetoxysilane, hexamethyldisilane, y-chloropropyltrimethoxysilane.

As titanate coupling agents suitable for the 10 invention, the following products are cited: isopropyltriisostearoyltitanate, tetra(2, .0 2-diallyloxymethyl-l-butyl) bis (di-tridecyl) phosphitetitanate, tetraisopyruvis (dioctylphosphite) titanate, isopropyltri (N-aminoethyl-aminoethyl) titanate, tetraoctyl bis (ditridecylphosphite) titanate, isopropyltris (dioctylpyrophosphanate) titanate, bis (octylpyrophosphate) oxyacetatetitanate.

As an aluminum derivative coupling agent suitable for the invention, acetoalkoxyaluminiumdiisopr6pylate is cited.

When the preceding coupling agent reacts with the surface of inorganic material, there is an optimum amount in order to obtain the optimum properties such as adhesive power. Usually, a coupling agent is mixed with a desirable solvent, adjusted and used. Such solvents are methanol, ethanol, isopropyl alcohol, toluene, benzene, acetone, methyl cellosolve, 37 tetrahydrofuran and water. The solvent which is compatible with each coupling agent is selected and used. If solvent is used at high concentration, the activity of coupling agent would loose. Therefore, low concentration is used, 0.01% 10.0% is usually optimum.

Also, the hydrophilic portion of the preceding coupling agent depends on silane, titanate, and aluminum derivatives; the suitability to the reaction of inorganic material must be considered. On the other hand, the organic function group of coupling agents are amino, epoxy, carboxy, phosphite radicals, etc. The suitability to reaction of organic material with these organic function groups must be considered.

(Mean molecular weight of polymer) In order to prevent diffusion of the preceding metal ion from the preceding metal wire, it is necessary to get good adhesion of the conductive particle with the polymer. For this reason, as said 20 polymer, the polymer of more than 500 and less than i 50,000 figure mean molecular mean weight is desirable.

In this disclosure,in order to form a dense coating film, it is necessary to improve the ;dispersibility between the used polymer and the conductive particles, and to decrease the hole volume *of the formed coating layer. It becomes possible to control the effect of humidity by proper selection and control the effect of humidity by proper selection and 38 combination of polymers having more than 500 and less than 50,000 mean molecular weight and various kinds and diameters of conductive particles. The favorable resins for use are urethane, phenoxy, epoxy, butyral, phenol, polyimide, melamine, alkyd, fluorine polyvinylformal, polyamide, polyamideimide, polyester, acrylic and styrene resins. Especially, urethane, phenoxy, epoxy and phenol resins are widely used industrially for insulation material for enamel wire.

S 10 Good properties in respect to humidity resistance, control of flexibility and productivity can be obtained. Moreover, butyral resin has good dispersibility, polyimide resin has good heat resistance.

(The gel ratio of the polymer) One way to measure the degree of bridging of the polymer is to measure its gel ratio. In other words, when a specimen of the polymer is soaked in solvents, such as xylene, the gel parts that have bridged by gelation will not elute, but the sol parts which have not bridged will. In other words, when bridging is complete, there will be no elution of the sol parts.

Next, when the specimen is removed and the xylene is evaporated, the undissolved gel part, from which the sol part has been removed, will remain. The gel ratio is obtained by measuring the amount of unbridged and eluted zol. The method of calculation is described -39below.

Gel ratio (weight of undissolved part) original weight of specimen] x 100 High gel ratios after the drying process will result in decreased adhesive strength during the formation of the coated wire for collector electrode. In addition, low sol ratios of the conductive resin layer of the coated wire for collector electrode formed by thermocompression, may result in decreased dependability when subjected to moisture.

Therefore by limiting the gel ratio of the polymer layer of the coiluctive resin layer to 0% to 20%, after the adhesive layer has been coated and dried onto the metal wire, its initial adhesion will not be affected during storage. In addition, by keeping the gel ratio of the adhesive layer to 20% to 100%, after the thermocompression formation of the collecting electrode, dependability during usage will also be improved.

(The mixing of the conductive particles and the polymer) i "The mixing of the conductive particles and the polymer" according to this disclosure is conducted at a suitable ratio to obtain the desired resistivity. Resistivity will decrease as the amount of conductive particles increase, but the coating layer will loose its stability as the proportion of resin decreases.

*o 0 4* 00 *00* 0 0 00*000 [I:\DayLib\LI BE1302746a.docJIs 40 And when the polymers are increased, the contact of the conductive particles to each other becomes faulty and resulting in high resistance. Therefore, the Optimum ratio should be determined depending on the polymer and conductive resin to be used, as well as its desired physical properties. In specific terms, good resistivity is obtained at volume percentages of the conductive particles ranging from 5% to The distributing devices used in "the mixing of the conductive particles and the polymer" according to this invention are, for example, regular triple roll mills, ball mills, paint shakers and bead mills. It is acceptable to add distributing agents and coupling agents as desired to improve distribution. It is also acceptable to dilute it with a suitable solvent to adjust the viscosity of the conductive adhesive, during or after distribution.

JO

,(Layer closer to the electrode) "Layer closer to the electrode" according to this 20 disclosure, are those layers which have either one or :-':both of the following functions: to protect the metal e b wire used in the electrode from the surrounding 000* environment or to establish an electrical connection

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with the metal wire. The resistivity of "layer closer 00 0 25 to the electrode" must be such that it does not offer electric resistance when collecting the current Sgenerated by the photovoltaic element and a suitable S generated by the photovoltaic element and a suitable 41 range would be 0.1 Qcm to 100 Qcm. By using heat cured conductive adhesive for this "layer closer to the electrode", solvent resistance and heat resistance during production, as well as dependability during usage is improved.

If so desired, it is acceptable to form the contact layer, of which the main ingredient is metal, as the "layer closer to the electrode". The contact layer has the function of improving the electrical

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1 0 contact between the metal wire and the conductive adhesive. In particular, when copper is used for the electrode metal wire, its surface is subject to oxidation, resulting in high resistance, in which case the contact resistance will increase, should graphite and substances like metal oxides be used for the esi.

conductive particles. Use the contact layer to prevent 9I*S such incidents. Candidates materials for the contact layer are precious metals that offer resistance to ••o corrosion, such as silver, palladium, silver and palladium alloy and gold, as well as metals with good corrosion resistance, such as nickel and tin. When this consists of a conductive adhesive, it is desirable to produce an adhesive with the metal as its filler.

It is also acceptable to form a layer of tin or silver on the metal wire by plating, without using conductive adhesives. Silver clad copper wires are also acceptable.

42 When metal based conductive adhesive is used in the "layer closer to the electrode", it is acceptable to form a barrier layer on top of it that will prevent metal ion migration.

The thickness of the barrier layer will vary depending on the wire diameter and preference. For example, for a wire with a diameter of 100 pm, a thickness of 1 pm to 15 pm would be desirable, to a prevent pin-holes, to provide sufficient function as a 10 barrier and to prevent excessive shadow loss.

ooooo i: *Thicknesses of under 1 pm make it difficult to create a uniform coating and pin-holes will occur, rendering it insufficient as a barrier. On the other hand, thicknesses of over 15 pm are not desirable because 15 they are difficult to peel and shadow loss becomes too great.

(The void ratio of the conductive adhesive) ooo o S•In order to improve its barrier effect against metal ions, the void ratio of the conductive adhesive used in the barrier layer must be 0.04 ml/g or smaller, for a void radius of 1 pm or smaller.

Void radii of over 1 pm or more exist only very rarely for regular adhesives containing pigment. And when voids larger than this do exist, the mechanical strength of the conductive adhesive deteriorates after curing. Also, void ratios exceeding 0.04 ml/g will allow water to penetrate, which will degrade the bond 43 between the conductive particles and the polymer in the conductive adhesive, resulting in greater resistance or metal ion migration.

(The glass transition point of the conductive adhesive) According to this disclosure, it is desirable that the glass transition point of the conductive adhesive after curing is 100 'C or higher. This will give it characteristics to sufficiently withstand the heat history during over-coating after the formation of the coating, as well as during the top coat agent and lamination processes.

(The method of coating the conductive adhesive) Regular coating methods used for enamel wires can be suitably used as "the method of coating the conductive adhesive" in this disclosure. In specific terms, the conductive adhesive will be diluted to an appropriate viscosity, after which it will be coated onto the metal wire using a roll coater etc., after 0: which it will be passed through dies or felt to form 0 0e 20 the desired thickness and finally dried and cured using infrared heating, etc.

ooooFig. 3 is a type diagram describing a suitable ••go coating device. In Fig. 3, 301 is the delivery reel, oooo 302 is the metal wire, 303 is the cleaning tank, 304 is 0 0 the coater, 305 is the die, 306 is the drying oven, 307 0 is the film thickness gauge, 308 is the tension 0 controller, 309 is the aligned winding motor, 310 is 44 the take-up reel and 311 is the temperature regulator.

The delivery reel 301 is the bobbin to which the metal wire before coat formation is wound. The cleaning tank 303 is used only when required. This tank is filled with solvents, such as acetone, MEK and IPA, and is used to clean the surface of the metal wire 302 of any dirt. The coater 304 is a device which is used to apply the conductive adhesive to metal wire 302.

.The coater 304 contains a certain amount of conductive 10 adhesive to be applied and can be equipped with a eoo solvent adding mechanism for adjusting viscosity, a conductive adhesive replenishing mechanism or a filter Smechanism if desired. The die 305 is a device which controls the thickness of the applied conductive 15 adhesive to the desired thickness. As for the die 305, .r commercially available die for enamel coats are suitable for use, but felt may be used if desired. The drying oven 306 is used to remove solvent from the applied conductive adhesive and to dry it. It is also used for curing and if desired, these can be hot air driers or infrared driers. The film thickness gauge 307 is used to measure and manage the thickness of the applied conductive adhesive, and a commercially available outer diameter gauge is suitable for this purpose. It is also acceptable to use the information obtained through the film thickness gauge to conduct feedback controls, such as for delivery speed and 45 viscosity of the conductive adhesive. The tension controller 308 maintains a constant tension, to prevent sag or forces exceeding the yielding point to be applied to the metal wire 302. The aligned winding motor 309 is a device that controls the spacing of the wire while the wire is being wound to the take-up reel 310. The take-up reel 310 is rotated at the desired speed, by a motor which is not shown in the figure.

The temperature regulator is a device which maintains 10 the temperature in the drying oven 306 at the set value. Well-known methods, such as slidack, on/off control and PID can be used if desired.

Fig. 3 shows a vertically oriented device, but the direction of travel of the metal wire 302 can be either 15 vertical or horizontal and can be determined based on preference.

When applying multiple coats of conductive adhesive, (the wire) may be taken up by the bobbin after each coating, but it may also be taken up by the bobbin after multiple coatings are complete. Fig. 3 shows the coating of one wire, but multiple wires may be coated simultaneously.

The metal wire, onto which conductive adhesive has been coated, is to be stored wound to the bobbin, to be unwound for use when forming the collecting electrode for the photovoltaic element.

(Photovoltaic element) -46- Solar batteries configured as shown in Figs. 4A to 4C through Figs. 8A and 8B are examples of photovoltaic elements.

Shown in Figs. 4A to 4C is a typical cross section of an amorphous silicone based solar cell, which receives light from the surface opposite the substrate. In this figure, 401 is the substrate, 402 is the lower electrode, 403, 413 and 423 are the n-type semiconductor layers, 404, 414 and 424 are i-type semiconductor layers, 405, 415 and 425 are p-type semiconductor layers, 406 is the upper electrode consisting of a transparent conductive film and 407 is the grid electrode where a coated wire for collector electrode is used.

Fig. 5 shows a cross section of a monocrystal silicone solar cell. 501 is the semiconductor layer consisting of the silicone wafer substrate, 502 is the semiconductor layer which forms a pn junction with the semiconductor layer 501, 503 is the rear face electrode, 504 is the collecting electrode and 505 is the low reflection coating.

Fig. 6 shows the cross section of a polycrystalline silicone solar cell, 601 is a semiconductor layer consisting of a silicon wafer substrate, 602 is a semiconductor layer which forms a pn junction with semiconductor layer 601, 603 is the rear face electrode, 604 is the collecting electrode and 605 is the low reflection coating.

*a o o ooo• *oo oooo p:\DayLib\L1BE]02746a.docs -47- Fig. 7 shows the cross section of a thin film polycrystalline silicon solar cell, 701 is the substrate, 702 is the polycrystalized semiconductor layer, 703 is the semiconductor layer which forms a pn junction with semiconductor layer 702, 704 is. the rear face electrode, 705 is the collecting electrode and 706 is the low reflection coating.

Figs. 8A and 8B show the solar cells shown in Figs. 4A to 4C through 7, from the light entry side. 801 is the substrate, 802 is the positive electrode, 803 is the negative electrode and 804 is the collecting electrode.

The structure of the "photovoltaic element" in this invention, istdesirable to consist of, for example, a semiconductor layer which contributes to electricity generation, a transparent conductive layer installed on the light entry side of the semiconductor layer, a coated wire for collector electrode consisting of the metal wire and conductive adhesive on the transparent electrode and a rear face electrode installed on the side opposite of light entry of the semiconductor layer.

The semiconductor layer is required to have a structure which possesses semiconductor junctions, such as pn junction, pin junction or Schottky splicing, etc.

Materials suitable for this purpose are, for example, semiconductors in the group IV, such as crystalline pI:\DayLib\LBE]02746a.docs 48 silicon, polycrystalline silicone and amorphous silicon, semiconductors in the group II-VI, such as Cds and CdTe, or semiconductors in the group III-V-, such as GaAs.

In the photovoltaic element of this invention, the collecting electrode is positioned on the light entry side of the semiconductor layer, positioned in a parallel configuration, with appropriate spacing. The electrode in this invention is particularly suitable for the formation of photovoltaic elements with large areas. For example, when producing a 30 cm x 30 cm photovoltaic element, collecting electrodes can be formed by placing electrodes, consisting of metal wires cm in length and conductive adhesive, on the semiconductor layer at specified intervals.

Furthermore, for the purpose of sending electric currents from the collecting electrode to one terminal, a bus bar electrode of relatively large capacity is to e be formed.

20 The rear face electrode of the photovoltaic *element stated in this disclosure is one that is installed on the rear face of the semiconductor layer, the metal of which is formed, for example, by screen printing or deposition. The type of metal used, should be chosen from one that offers good ohmic contact with the semiconductor.

When the semiconductor layer is made of a thin When the semiconductor layer is made of a thin 49 film consisting of monocrystal semiconductors containing amorphous silicon, microcrystal silicon or polycrystalline silicon based substances, it will need a subsidiary substrate. Both insulative and conductive substrates may be used for the subsidiary substrate.

Substrates of metals, such as stainless steel or aluminum are suitable for use and these also function as the rear face electrode. When insulative substrates, such as glass, polymer and ceramics, etc.

10 are used, metals such as chrome, aluminum or silver are to be depositioned to create the rear face electrode.

The lower electrode 402 is an electrode on one side to retrieve the power generated in the semiconductor layers 403, 404, 405, 413, 414, 415, 423, 424 and 425, and is required to possess a work function that will create an ohmic contact with semiconductor layer 403.

Materials used are, for example, metals or alloys, and transparent conductive oxides (TCO), such as Al, Ag, Pt, Au, Ni, Ti, Mo, W, Fe, V, Cr, Cu, nichrome, SnO 2 In 2 0 3 ZnO or ITO, etc. It is desirable that the surface of the lower electrode is smooth, but it may be textured if it is a cause of irregular reflection of light. Also, if substrate 401 is conductive, there is no need for a lower electrode 402. The lower electrode may be formed with well-known methods, such as plating, depositioning or spattering.

Not only are single structure with n-layer 403, i-layer 404 and p-layer 405 as one set suitable for the amorphous silicone semiconductor layer, but so are double or triple structure consisting of two-or three sets of pin or pn junctions. Materials such as a-Si, a-SiGe and a-Sic, or the so called group IV and group IV alloy-type amorphous semiconductors, are suitable in particular, for the semiconductor material used for the i-layers 404, 414 and 424. Methods such as depositioning, spattering, high-frequency plasma CVD, 10 microplasma CVC, ECR, heat CVD, and LPCVD methods, for example, can be used for the film formation of the amorphous semiconductor layer if desired. Transparent conductive film 406 is required when the sheet resistance is high, such as is the case with amorphous 15 silicone. And because it is positioned on the light entry side, it is required to be transparent.

Materials such as SnO 2 In 2 0 3 ZnO, CdO, CdSNO 4 and ITO, for example are suitable for the transparent conductive film 406.

As for monocrystal silicone solar cell 500 and polycrystalline silicon solar cell 600, a subsidiary substrate is not installed and the monocrystal wafer 501 and polycrystalline wafer 601 act as the substrates. The monocrystal wafer 501 is made by cutting, etc. an Si ingot which is pulled up with the CZ method. The polycrystalline wafer 601 is formed by cutting an Si ingot obtained with the cast method or by 51 obtaining a polycrystal in sheet form using the ribbon method. For example, the vapor phase diffusion method using POC 13, the coat diffusion method using Ti02 SiO 2 or P 2 0 5 or the ion placing method which dopes it directly in ions is used to make semiconductor layers 502 and 602. The rear face electrodes 503 and 603 are made by forming metal films with deposition or spattering, or by screen printing of silver paste. The low reflection coating 504 and 604 are formed to prevent the loss of efficiency, caused by light reflecting off of the solar cell surface. Suitable materials are, for example, SiO 2 Ta 2 0 5 and The thin film polycrystal 700 is formed by growing Si polycrystal thin film 702 on substrate 701 made of alumina or graphite, etc. And in some cases, a particle diameter enlargement process is conducted, after which this is used as a substrate once again, onto which the base layer is formed, on top of which the surface layer 703 is formed using the epitaxial 20 growth process. Low cost substrates, such as metal Si may be used for substrate 701.

The second electrode consisting of the coated wire for collector electrode is positioned on the light entry side of the semiconductor layer. It is desirable that they be positioned in appropriate intervals, so .'oeo that the sum of the loss caused by the electric resistance of current collecting and shadow loss is -52 mimimam. For example, if sheet resistance is approximately 100 ohms/L, the desired intervals of the coated wire for collector electrodes would be about 5 mm. Also, optimization by narrowing pitch for thin diameter wires and widening pitch for thicker diameter wires will offer optimum efficiency.

The electrode in this disclosure is particularly suitable for the formation of solar cells with large areas. For example, when producing a 30 cm x 30 cm solar cell, collecting electrodes can be formed by placing electrodes of this disclosure, on the semiconductor layer at specified intervals. Furthermore, for the purpose of sending electric currents from the collecting electrode to one terminal, a tab may be positioned as the collector.

A solar cell produced in this manner is encapsulated using a well-known process, for better weather resistance and to maintain its mechanical strength, and is modularized for outdoor use. In specific terms, with regard to the materials used for encapsulation, EVA (ethylene vinyl acetate), etc. is suitable for the adhesive layer. It is also acceptable to impregnate EVA in clay glass, etc. to improve mechanical strength. In addition, a fluoride resin is laminated as a surface protectant to improve moisture and scratch resistance. Suitable materials are for example, a polymer oftetrafluoroethylene (TFE), a

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[I:\DayLib\LBE]02746a.doc:jls -53 copolymer (ETFE) of tetrafluoroethylene and ethylene, polyvinyl fluoride and polychloro fluoroethylene (CTFE), etc. It is also acceptable to improve their weather resistance by adding ultraviolet ray absorbers to the resin. As for the method of laminating these resins with the solar cell substrate, heating and compression in a vacuum, using a commercially available device, such as vacuum laminator, for example, can be used.

Fig. 9 is a typical cross section showing an example of the photovoltaic element.

In Fig. 9, 901 is the subsidiary substrate, 902 is the rear face electrode, 903 is the p-type semiconductor layer, 904 is the i-type semiconductor layer, 905 is the n-type semiconductor layer, 906 is the collecting electrode.

Fig. 10 is a type diagram of a photovoltaic element module 100, using a "coated wire for collector electrode coated with conductive adhesive consisting of two layers (hereinafter abbreviated as: two-layer coated collecting electrode)" of this disclosure. In Fig. 10, 1001 is the photovoltaic element substrate, 1002 is the positive electrode, 1003 is the negative electrode and 1004 is the two-layer coated collecting electrode of this disclosure. Photovoltaic element substrate 1001 is made by forming films of p, i and n semiconductor and transparent conductive layers on the stainless steel o U

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ego* *eeo* *a eoc 1r:\DayLib\LBE]02746a.doc:jls 54 substrate, using the CVD or spattering process. The positive electrode 1002 is an electrode which is used to retrieve the current collected by the collecting electrode and materials suitable for this are, for example, copper or silver plated coppef which offer good conductance. The negative electrode 1003 is an electrode which is used to retrieve current from the stainless steel substrate and the material suitable for this would also be copper. The two-layer coated collecting electrode 1004 has the function of collecting the current generated by the photovoltaic element substrate. The two-layer coated collecting electrode 1004 is mechanically and electrically connected to the photovoltaic element substrate and the positive electrode by means of the thermocompression process.

In terms of the method by which the metal wire is positioned as the collecting electrode on the photovoltaic element; for example, when more than one wires are to be positioned on the surface of the photovoltaic element surface; optimum efficiency can be is obtained with optimization procedures, namely narrowing the pitch for thin wires and widening the pitch for thicker wires.

As for the method of adhesion, the outer most layer of the coated wire for collector electrode must not be cured during application on the wire and only be dried of the 00* go *o 0 00**00 00 00 0 0 0 0 [I:\Day Lib\LI BE]02746a.doc:j Is solvent. And heated when adhering to achieve adhesion and curing.

(Production method) s One method of production of the photovoltaic element of this disclosure is, for example the production method of photovoltaic cells described below.

It is desirable to adhere the coated wire for collector electrode to the semiconductor or the transparent electrode of the light entry side with heat and/or pressure.

The desirable heating temperature would be the softening point of the adhesive layer and the conductive resin of the second layer, which will form the adhesive layer. It is desirable that only the adhesive layer and the second layer will be softened to make the coated wire for collector electrode adhere to the solar cell, without softening the first layer to maintain the initial film thickness. Also, if block isocyanate is used as the curing agent for the conductive resin, it is desirable to apply temperatures exceeding the dissociation temperature of isocyanate, so that curing will occur during the adhesion process.

The desirable pressure will be such that the adhesive layer and said second layer will undergo moderate deformation, but must also be lower than any pressure that will destroy the solar cell. In specific terms, 0.1 kg to 1.0 kg/cm 2 would be suitable for solar *ee• *999** [i:\DayLib\LIBE]02746a.doc:jls 56 cells with thin films, such as amorphous silicon.

If the adhesive layer and the second layer, which will form the adhesive layer, are of the hot-melt type, the desirable adhesive method would be to soften them and adhering them to the solar cell. Suitable pressure may be applied during adhering. If the second layer is thermoplastic, it will soften with heat. For heat curing resins, it is acceptable to dry the solvent, leaving the resins uncured during the application process to the wire for them to be heat cured during adhesion.

Also, the coated wire for collector electrode of this disclosure and the photovoltaic elements using the coated wire for collector electrode and their production method are entirely applicable to the photovoltaic elements other than the solar cell.

Is (Curing agents to be included in the conductive adhesive) One of the problems of production is that, in order to produce coated wire electrodes off-line and to facilitate storage until the formation of electrodes, it is difficult to control accelerated hardening of the resins, after the resin has been coated and dried on the metal wire. By using block isocyanate as the curing agent, only the solvent contained in the resin is dried during and after the coating drying process, and by heating it at a Soconstant temperature, the block 0 o 6o. I so* bees ooe* S

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S

[I:\DayLib\LIBEI02746a.doc:jls -57agent dissociates, allowing active isocyanate radicals to react with the resin to achieve hardening. In other words, whereas it has been very difficult to control accelerated hardening with other curing agents, such problems are solved by using block isocyanate as the curing agent.

(The glass transition point of the conductive 9* adhesives) 9 9 ooso ,o Another production related problem was, that it is 10 convenient for handling if the metal wires are wound to a bobbin, etc. after the resin has been coated, however, the tackiness of the coated wires themselves I. made it difficult to unwind them from the bobbin and in some cases where tackiness was strong, the coating 15 would peel off. This occurs when the glass transition point of the coating layer resin is low. By using resins with glass transition points of over 0 the o:0 effects of tackiness reduction can be felt, but better results are obtained when the glass transition temperature is over 100 Also, by mixing polymers with different glass transition points, it becomes possible to form coating layers with superior properties in terms of flexibility, adhesion and reduced tackiness. Preferable combinations are urethane resin and phenoxy resin, etc.

(The average particle diameter of primary particle of conductive particles) 58 To obtain stably a coating layer with uniform film thickness and good conductivity, the dispersibility of conductive particles into resin becomes important as well as the selection of high polymer. Although the diameter of a conductive particle should be formed smaller than the thickness of conductive coating layer, too small diameter increases resistance at the surface of particles where they contact each other, making it impossible to obtain the desired resistivity. When the 10 conductive particles are dispersed into the resin, ooo o agglomerated particles exist; such as primary particles which are systematically agglomerated crystallites, ~secondary particles which consist of primary particles agglomerating with particles' surface charge or van der Waals force or with other force. If the dispersibility *oeo is poor, agglomerated particles of a high order would .exist to cause not only ununiform film thickness but .:Soo: also unstable conductivity. This invention has solved the problem by making the average diameter of primary particles of conductive particles in the coating layer bigger than 0.02 pm and smaller than 15 pm, the sizes which prevent formation of agglomerated particles of a higher order. As the method to measure particles' agglomerating state in dispersion and particles' diameter (generally called 'grading'), there are the laser diffraction method, the light-particle correlation method, the light scattering method etc.

59 The suitable conductive particles for the coating layer are graphite, In 2 0 3 SnO 2 TiO 2 ITO, ZnO, and oxide semiconductor materials made from the materials by adding suitable dopants. The conductive particles and the polymer are mixed at a suitable ratio to obtain the desired resistivity. Although increased conductive particles reduce resistivity, they decrease the ratio of resin resulting in poor stability as coating film.

g Therefore, a suitable ratio should be properly selected *0 "r 10 considering what kind of high polymer and conductive *particles will be used and what physical property value is desired for the film. Going into detail, around volume percent to 95 volume percent of conductive .u i. particles give good resistivity. When the conductive 15 particles and polymer are mixed, ordinary dispersing of•, eo methods, such as a three-roll-mill or a paint shaker ~etc., can be used. During or after the dispersion, the conductive paint can be diluted with a suitable solvent to adjust viscosity.

(The thickness of coating layer composed of conductive adhesive) A problem during and after the formation of electrodes on a photovoltaic element is forming of pinholes which causes leakage current to defective parts reducing the characteristics of the photovoltaic element. However, this problem is solved by forming coated layers precisely and forming coating layers with 60 sufficient thickness. The thickness of the coating layer varies with the diameter of the metal wire or characteristics desired. For example, when the metal wire is 100 pm in diameter, to have sufficient function as a barrier layer against leakage current, at the same time not to cause extreme shadow loss, the suitable thickness is between 1 pm and 30 pm. Another problem I is, while forming of electrodes, metal wires touch the oo o solar cell substrate to cause shunt. The solution to 1 0 this problem is to form more than 2 of coating layers, and to harden completely the innermost layer of the coating layer while coating. In this way, metal wires are prevented from direct contact with the solar cell substrate during the compression process. The o r 15 problems, such as migration etc., which occur when a oo• photovoltaic element is used outdoors, can be solved by separating functions into layers; by preparing more than 2 layers of coating layers to share the functions such as current collecting, shunt prevention, migration prevention, electrode fixing, etc.

Fig. 2A shows the sectional plan of an electrode with conductive coating layer on. Fig. 2C shows the sectional plan of the part where the electrode is fixed on a photovoltaic element substrate through the coating layer. In Fig. 2A and Fig. 2C, 201 is the metal wire, 202 is the primary coating layer which is directly coated on the metal wire, 203 is the secondary coating 61 layer which forms the outermost layer, 205 is the coating layer (the whole) corposed of conductive adhesive, and 206 is the photovoltaic element substrate. Coating of conductive coating layers is desired to be made cocentrically. As the method to coat the conductive resin on the metal wire, the ordinary spreading method of insulating coating film, the method used for enameled wire, can be suitably used. Going into detail, the conductive resin is 1 0 diluted with a solvent to obtain suitable viscosity, then coats the metal wire with a roll coater, etc. The coated wire is passed through the dice to form a desired thickness, and is put in a furnace for drying the solvent and heat curing.

(Components of photovoltaic element) 0, In the following part, the components of photovoltaic element will be explained S. using Fig. 4A, Fig. 4C, and Fig. 13. Fig 4A shows an amorphous silicon solar cell which has single cell structure with the light incidence on the other side of the substrate. Fig. 4C shows an amorphous.silicon solar cell which has a triple structure of the solar cell in Fig. 4A. Fig. 13 shows the solar cells when looked at from the side of light incoming side shown in Figs. 4A and 4C. Grid electrodes of about 30 cm long are seen formed.

Although no illustrations are shown, it goes 62 without saying that the composition according to the invention's idea can be applied to amorphous silicon solar cells which are accumulated on a transparent insulated substrate, and also to monocrystalline and thin-film polycrystalline solar cells.

In Fig. 4A, 401 shows the subsidiary substrate, 402 shows the lower electrode, 403, 404, and 405 respectively show the semiconductor layer which form c o pin-junction, 406 shows the upper electrode of 10 transparent conductive film, and 407 shows the grid electrode using coated wire of collector electrode.

In Fig. 4C, 403, 404, and 405 show the semiconductor layers which form the first pin-junction, 413, 414, and 415 show the semiconductor layers which form the second pin-junction, 423, 424, and 425 show *the semiconductor layers which form the third pin-junction.

0*0. In Fig. 13, 1301 shows the metal tab, 1302 shows the output port of anode, and 1303 shows the output port of cathode.

0 (Substrate)

S

The substrate 401 according to this disclosure is a membrane which mechanically supports semiconductor layers 403, 404 and 405 which are a thin film solar cell such as non-crystaline silicone. It is also used as an electrode in some cases. The substrate 401 has a required heat resistance to the heat temperature for 63 forming film of semiconductor layers 403, 404 and 405.

However, both the one having the electroconductive property and the one having an electro insulating property can be used. As electroconductive material, such metals as Fe, Ni, Cr, Al, Mo, Au, Nb, Ta, V, Ti, Pt, Pb and Ti are used; these alloys, for example, brass and stainless steel thin plate and its complex, carbon sheet and zinc plated steel plate are among those that can be used. As electro insulating S 10 material, film or sheet of heat resistant resin such as polyester, polyethylene, polycarbonate, cellulose acetate, polypropylene, polyvinylchloride, polyvinylidenechloride, polystyrene, polyamide, polyimide and epoxy resin are used. Or the compound with the resin and glass fiber, carbon fiber, boron fiber, metal fiber are among those also cited. And on the surface of the thin metallic plate and resin sheet, a coating treatment with foreign material metal thin film and/or insulating thin film of Si02, Si 3

N

4 A1 2 0 3 AlN, etc., is carried out by a sputtering, vapor deposition and plating method. Glass and ceramic are also cited.

(Lower electrode) According tothis disclosure,the lower electrode 402 is one electrode to take out the electric power generated at semiconductor layers 403, 404, and 405.

It is required to have such a work function as to form 64 an ohmic contact to the semiconductor layer 403. As its materials, for example, Al, Ag, Pt, Au, Ni, Ti, Mo, W, Fe, V, Cr, Cu, stainless steel, brass, nichrome, SnO 2 In 2 0 3 ZnO, ITO, etc. are used as simple metallic substances or as their alloys or as transparent conductive oxides (TCO), etc. Although the surface of the lower electrode 402 is desirable to be smooth, the surface can be textured to cause diffused reflection of light. When the substrate 401 is conductive, tTie lower 10 electrode 402 is not necessarily to be prepared.

The methods to prepare the lower electrode are plating, deposition, spattering etc. As the methods to prepare the upper electrode, there are the ohmic-resistance heating deposition method, the electron beam heating deposition method, the spattering method, the spraying method etc. to choose the desired.

(Semiconductor layer) According tothis disclosure,the named semiconductor layers are amorphous silicon, polycrystalline silicon, monocrystalline silicon, etc..

0 In an amorphous silicon solar cell, the semiconductor materials to compose i-layer 404 are; a-Si:H, a-Si:F, a-Si:H:F, a-SiGe:H, a-SiGe:F, a-SiGe:H:F, a-SiC:H, a-SiC:F, a-SiC:H:F, etc. The named are, what is called, IV group and the IV group's alloy-amorphous semiconductor. The semiconductor materials to compose p-layer 405 or n-layer 403 are obtained from the 65 semiconductor materials for the i-layer 404 by doping valence electron control agent. As the materials for valence electron control agent to obtain p-type semiconductor, the compounds of elements in group III of the periodic table are used. Elements in group III are B, Al, Ga, and In. As the valence electron control agent to obtain n-type semiconductor, the compounds of elements in group V of the periodic table are used.

0 0 S* The elements in group V are P, N, As, and Sb. S: 10 The methods to form films of amorphous silicon semiconductor layers can be chosen whatever desired from the well known methods such as the deposition :method, the spattering method, the RF plasma CVD method, the microwave plasma CVD method, the ECR method, the thermal CVD method, the LPCVD method, etc.

0o0* Industrially, the RF plasma CVD method is favorably used, in which the material gas is decomposed with RF plasma and accumulated on the substrate. However, the RF plasma CVD method has problems such as the low yield in the material gas decomposition (about 10 and the slow accumulating speed (about 0.1 nm/sec. to 1 nm/sec.). The microwave plasma CVD method is attracting attention as an improved method for these problems. As the reactor to do the film formation, well known devices, such as the Batch reactor or a continuous film formation device, etc., can be used whatever desired. The solar cell can also be 66 used for, what is called, tandem cell or triple cell, in which more than two semiconductor splices are laminated in order to obtain better spectral sensitivity and higher voltage.

(Upper electrode) According tothis disclbsurethe upper electrode 406 is the electrode to take out electromotive force generated at the semiconductor layers 403,- 404, and 405. It makes the pair to the lower electrode 402.

The upper electrode 406 is necessary for semiconductors with high sheet resistivity, such as amorphous silicon.

Because crystalline solar cells have low sheet 0 4, resistivity, they do not necessarily need the upper electrode. The upper electrode 406 is positioned on the light incoming side and it needs to be transparent, and it is also called the transparent electrode. The upper electrode 406 is desirable to have more than of transmissivity for effective absorption of light from the sun and daylight fluorescent lamps etc. into semiconductor layers. Electrically, the upper electrode 406 is desirable to have a sheet resistivity value of less than 100 0/0 to let the electric current generated with light flow horizontally to the semiconductor layers. Materials with these characteristics are the metal oxides of SnO 2. In2031 ZnO, CdO, CdSn04, ITO, etc.

(Grid electrode) -67- The grid electrode 407 consists of the metal wire 201, as shown in Fig. 2A, and the conductive coating layer 205. The conductive coating layer 205 needs to have resistivity value which is low enough not to reduce the efficiency of photovoltaic element and at the same time high enough to prevent shunt. That is, it does not act as resistance to the electric current generated by solar cells, but works as resistance to prevent serious leakage when any defect is around. The suitable resistivity value for the conductive coating layer 205 depends on the design of the grid, and on the photovoltaic element's electric current value and the scale of defect at is operating point. The desirable resistivity value is 0.1 100 Qcm. When shunt occurs in this range, the value becomes sufficient resistance, and at the same time, this value is almost negligible-t the electric current generated at the photovoltaic element. The grid electrode 407 is positioned on the light incoming surface side of the photovoltaic element 400 (shown in Fig. 4A). As the grid's arrangement, the parallel arrangement with suitable intervals is recommendable.

15 The coated wires for collector electrodes are particularly suitable for forming a solar cell with large area. For example, when solar cell of 30 cm 2 is built, all needed is to install the coated wires for collector electrodes of 30 cm long parallel on the semiconductor layer with prescribed intervals. Furthermore, because 0 *0* •oo• [j:\DayLib\LIBE]02746a.doc:js -68the electrode is composed to reduce the current leakage caused by shunt or leaks, it is suitable for amorphous silicon solar cells. However, such composition is, of course, applicable to other types of solar cells than amorphous silicon type; to the solar cell of monocrystalline, polycrystalline, or of other semiconductors than silicon, or of Shottky splicing type.

(Tab) 10 According to this disclosure, the tab 501 is the collector which collects the *w S flowing current at the grid electrode 407 to one end. As the materials forfhe collector, °metals like Cu, Ag, Pt, and alloys of these metals are usable. The desirable shapes are *0 sheets, tapes, or foils to be glued with adhesive agents.

0 (The method to form the collecting electrode on the photovoltaic element) According to this disclosure, as "the method to form the collecting electrode on the photovoltaic element", the following method is illustrated as how to build solar cells.

0 o.o 20 The coated wires for collector electrodes are desirable to be glued on the light incoming side of the semiconductor layer or on the surface of the transparent conductive film, using heat, pressure, or both.

The favourable heating temperature is to higher o o II:\DayLib\LIIBE]02746a.doc:jls 69 than the softening point of the outermost coating layer, which is to become the glueing layer, and of the high polymer which forms the coating layer. When the conductive resin's hardening agent is composed of block isocyanates, it is desirable to keep the temperature higher than the block isocyanate's dissociation temperature, then let the resin cause heat curing while glueing process.

The favorable pressure should be high enough to 10 suitably transform the glueing layer, the outermost layer of the coating layer, but should be lower than the pressure which keeps the solar cell without [damaging. Going into detail, for example, for a film-type solar cell, such as amorphous silicon, a pressure of 0.1 kg/cm 2 to 1.0 kg/cm 2 will be suitable.

As the glueing method, when the glueing layer, the outermost layer of the coating layer, is hot-melt-type, it is desirable to be glued to the solar cell by softening with heat. While glueing, a suitable pressure can be applied.

(Encapsulation) The solar cell made by the abovementioned method is modularized by well-known encapsulation in order to improve weather resistance and mechanical strength. As encapsulation material, adhesive layer is concerned, EVA (ethylene vinyl acetate) is favorably used from the point of adhesive property to solar cell, weather 70 resistance and buffer effect. In order to improve further moisture resistance and anti scratching property, a fluorine resin is laminated as a surface protecting layer. For example, 4 fluoro ethylene copolymer TFE (Du Pont TEFLON), copolymer of 4 fluoroethylene and ethylene ETFE (Du Pont TEFZEL), polyvinyl fluoride (Du Pont TEDLER), polyvinyl fluoride (Du Pont TEDLER), polychlorofluoroethylene CTFEC Daikin

S.

Industries Neoflon) are cited. Weather resistance can e* S 1 0 also be improved by adding well-known UV absorber.

As the method for encapsulation, for example, it 6"00"5 is desirable to use well known:devices such as the 0* S: vacuum laminater, for thermocompression bonding of the solar cell substrate and the resin film in a vacuum.

(Embodiment) [The following is the detailed and embodied explanation of "the collecting electrode, the photovoltaic element with the coated wires for collector electrodes, and their building process". However, this 20 invention shall not be limited by these embodiments.

S

5 Firstly, in Embodiments 1 40 and Examples for Comparisons 1 2, a detailed discussion is given on "the case when conductive adhesive is composed of conductive particles and high polymer".

Secondary, in Embodiments 41 46 and Examples for Comparisons 3 4, a detailed discussion is given on "the case when the coating layer is composed of at -71 least more than 2 layers, and at least the conductive adhesive, which forms the outermost layer of the coating layers, is composed of not yet hardened but heat curing high polymer".

Furthermore, in Embodiments 47 55 and Examples for Comparisons 5 6, a detailed discussion is given on "the case when the conductive adhesive contains coupling agent".

Concerning Embodiments 1 40 and Examples for Comparisons 1 2, the following information is collected and shown in Tables 9 -16; the formativebonditions of the coated wire for collector electrode, the solar cell structure, and the characteristic evaluation results of solar cells.

15 (Embodiment 1) In this embodiment, an explanation is given on the case when a coated wire for collector electrode is composed of Cu wire, carbon black, and urethane.

20 As Fig. la shows, the coated wire for collector electrode 100 of this disclosure was formed as follows. As the metal wire 101, copper wire of 100 rm in diameter was used.

The carbon paste, to form conductive adhesive for the coating layer 102, was 25 prepared as follows. First, a mixed solvent of ethyl acetate 2.5 g and IPA 2.5 g was placed in a shake bottle for dispersion. Next, 22.0 g of urethane resin, the main ingredient, was added into the shake bottle, and all was mixed [:\DayLib\LIBE]02746a.doc:js 72 thoroughly with the ball mill. The number average molecular weight of urethane resin was 3000. Then, 1.1 g of block isocyanate, as a hardening agent, and g of glass beads, for dispersion, were added to the solution. Then, as conductive particles, 2.5 g of carbon black of 0.05 pm in average primary particle diameter was added to the solution.

The shake bottle containing the materials was placed in a paint shaker, of Toyo Seiki Co., for hours for dispersion. Then glass beads for dispersion were removed from the prepared paste. The average particle diameter of the paste was measured to be about 1 Pm. The results of using the beads mill instead of a paint shaker were almost the same.

The paste was hardened at 160°C for 30 minutes, •the standard hardening condition of the hardening agent. Its volume resistivity was measured to be 0.6 Scm to prove being low enough.

A

The void ratio of the paste was measured by a mercury Polosimeter to be 0.01 ml/g. Then, carbon black was removed from the paste and only resin was hardened to form a sheet. Its gel ratio was measured ,to be approximately 100 The coating layer 102 was formed as follows, using a vertical wire-coating machine 300 shown in Fig. 3.

First, the delivery reel 301 was set with a reel which is wound with metal wire 307. Next, the metal S- 73 wire was stretched toward the take-up reel 310. Then, the paste was poured into the coater.

The coating speed was 40 m/min, and the residence time was 2 seconds. The drying furnace 306 was set at 120 0 C. The coating was done 5 times. The dice, the one for enamel coating, were used in a variety of diameters, from 110 pm to 200 pm in order. Under this condition, the paste was preserved, with solvent evaporated and in unhardened state. The thickness of 9 10 the coating layer 102 was 20 pm on average. Variations in the film thickness after coating were within ±0.5 pm per 100 m.

As an embodiment of this invention, an amorphous solar cell 400 was built. It had the layer composition 15 shown in Fig. 4C and pin-junction-type triple structure with grid electrodes of 30 cm long.

First, an SUS 430 BA substrate 401 was thoroughly degreased and washed, then was placed in a DC spattering device (not illustrated) to accumulate 450 nm of Ag followed by 1000 nm of ZnO. Thus the lower electrode 402 was formed. The substrate was taken out and placed in a microwave plasma CVD film formation device (not illustrated) to form in order of silicon layer as the n-layer 403, silicon-germanium layer as the i-layer 404, and silicon layer as the p-layer 405.

Thus the bottom layer was formed. Then, in the same way, the middle layer was formed in order of silicon 74 layer as the n-layer 413, silicon-germanium layer as the i-layer 414, and silicon layer as the p-layer 415.

The top layer of the silicon layer was formed in order of the n-layer 423, the i-layer 424, and the p-layer.

Thus, the semiconductor layer was accumulated. Then, it was placed in the spattering device (not illustrated) to form 70 nm of ITO film, the transparent conductive film 406, which also has low reflectance function. Then, the solar cell substrate 401 was 10 trimmed into the size of 30 x 30 cm with an effective area of 900 cm 2 by removing unnecessary part of transparent conductive film, using etching paste, whose main ingredient is ferric chloride, and a printer on the market.

15 Then, out of the effective area, the anode 802 and the cathode 803, both of hard copper, were prepared.

As the collecting electrode 805, the coated wire 100 was stretched between the both anode 802 at 6 mm intervals and to be within the effective area, then was fixed with an ultraviolet-ray hardening adhesive.

The fixed said coating wire 100 was bonded by thermocompression, using a heating device (not illustrated), to form the collecting electrode 804 on the cell surface of the solar cell substrate 401 and on the anode 802. Thus, a triple-cell of 30 x 30 cm, shown in Fig. 8A, was built. The heating condition was; at 200°C, for 45 seconds, and at the pressure of 1 75 kg/cm 2 The encapsulation of this sample was done as follows. On the top and bottom of the solar cell substrate 801, plane glass and EVA were laminated, and fluorine-contained resin film ETFE (Tefzel of Du Pont) was laminated further on the top and bottom of it.

Then, the substrate was placed in a vacuum laminater and laminated at 150°C for 60 minutes.

In the same method, 50 solar cell modules were r 10 built.

.The initial characteristics of the obtained sample '0 were measured as follows. First, the voltage/current characteristics were measured in the dark state. The shunt resistivity was measured at the slope near the home position to be 200 kcm 2 to 500 kfcm 2 favorable results. Next, the solar cell characteristics were measured, using pseudo solar light source (hereafter 0 2 called simulator) with quantity of light of 100 mW/cm 2 by the AM 1.5 global sunlight spectrum. The obtained conversion efficiency was 9.6 0.02 showing favorable characteristics with little variations. The series resistivity was 32.0 Ocm 2 on average, also a favorable value. The yield rate of normal I-V curve was favorable 94 The reliability test was given to these samples in conformity with the Japanese Industrial Standards C 8917; the environmental testing method for crystalline 76 solar cell modules, and the hygrothermal cycle test A 2 provided by the endurance testing method.

The samples were placed in a thermo-hygrostat, which can control temperatures and humidity, and repeated 20 times of cycle tests varied between -40 0 C and +85°C (with relative humidity Then, the samples, which completed the cycle test, were measured their solar cell characteristics in the same way as the initial characteristics were, using the simulator. Its conversion efficiency was lower 2% on average than the initial value, showing no occurrence of meaningful deterioration.

The results of this embodiment show that a solar cell, with collecting electrodes S.of the metal wire coated with the invented conductive adhesive, has favourable characteristics and high reliability.

00••0 i (Example for Comparison) In this example, as a conventional example, an explanation is given on the case when the coated wire for collector electrode consists of Cu wire with fluorine-contained D 20 resin paste containing carbon.

For comparison, the conventional coated wire for collector electrode 100 was built in the same way as in Embodiment 1, in Fig. la, with the following exceptions.

25 The paste, used for the coating layer 102 of the coated wire for collector electrode 100 in Fig. 1A, was a EI:\DayLib\LI BE]02746a.doc:jls 77 fluorine-contained resin paste (Electrodag +502 SS of Acheson Colloid), similar to the one mentioned in the U. S. Patent No. 4,260,429.

The wire was coated in the same way as in Embodiment 1. The thickness of the coating layer 102 was 20 pm on average, and the deflection of film thickness in 100 meter long was over ±1.0 pm after coating.

The paste was hardened at 120°C for 5 minutes, the 10 standard hardening condition for the hardening agent.

The volume resistivity was measured to be 0.1 Qcm 2 a too, low enough value. The hole volume of this conductive adhesive was 0.05 ml/g. Then, like in Embodiment 1, solar cell modules were built, using this wire as 15 collection electrodes.

The initial characteristics of the obtained sample were measured in the similar method to Embodiment 1.

First, the shunt resistivity was measured to be 4 kQcm 2 300 kQcm2, showing a wide variation. Next, the conversion efficiency was obtained to be 9.0 ±1.2 varying widely. The series resistivity of normal 1 1 V curve was obtained to be 32.1 Qcm 2 on average, a favorable value. The initial yield rate of normal I V curve was as low as 64 The reliability test was done to this sample similarly to Embodiment 1. The tested sample was measured its solar cell characteristics with the 78simulator similarly to the initial characteristics. The result was on average 11% lower than the- initial conversion efficiency, showing the occurrence of meaningful deterioration. The series resistivity was measured to have risen to 62 Qcm 2 on average.

This indicated that the rise of the series resistivity caused the deterioration of the conversion efficiency.

It is supposed that the outside humidity entered into the device to raise the interfacial resistivity in the contacting part of the paste in the adhesive interface of coating to layer and transparent conductive film surface.

.e eq This result showed that the solar cell using the invented coated wire for collector electrodes have a good initial yield rate and favorable reliability.

"7 .a 15 (Embodiment 2)

S

In this example, an explanation is given on the case when the coated wire for collector electrode consists of Cu wire, ITO, and butyral.

20 In this case, the same process was used to build coated wires for collector electrodes as in Embodiment 1, except that, for the invented coated wire for collector electrode 100 according to this disclosure shown in Fig. 1A, butyral resin (Slec BL S of Sekisui Chemical Co., Ltd.) was used as the main ingredient high polymer to form conductive adhesive, and that ITO powder (HYX of Sumitomo Metal Mining Co., Ltd.) 25 of 0.05 pm in the average primary particle [:\DayLib\LIE102746a.docs:jls -79diameter was used as conductive particles.

The above-described paste was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener and then was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measured value was 1.2 Qcm 2 Further, transmittance of light was measured using a spectroscope and its transmittance was satisfactory because the measured value was 90% per 400 nm. The volume of a hole of this conductive adhesive agent was 0.02 ml/g and the ratio of gel was 20%. The average S* molecular weight of polymeric resin was fifty thousand.

Wire was coated as the first embodiment to form a coated wire for collector electrode 100. Fifty solar battery modules were produced using the coated wire for 15 collector electrode 100 by the:same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained ses •because its conversion efficiency was 9.7% 0.05%, its shunt resistance was 250 to 300 so*# 20 KQ cm 2 its series resistance was 32.5 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 94%.

The reliability test of these samples was [I:\DayLib\LIBE]02746a.docjs performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and its measured conversion efficiency was lower 2% S on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector electrode according to this disclosure has excellent characteristics and high reliability.

S-

(Embodiment 3) 0 Referring to this embodiment, the case that a coated wire for collector electrode 15 comprises Ag wire, urethane and SnO 2 will be described.

In this embodiment, a coated wire for collector electrode 100 according to this disclosure shown in Fig. 1A is produced as the first embodiment except that a metallic wwire 101 is formed by silver, and SnO 2 powder manufactured by Mitsui Mining and Smelting Co., Ltd. of which average primary particle diameter is 0.2 mrn is used as a conductive particle forming a coated layer 102.

The above-described past was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener Sand then, was measured in its volume resistivity and it as verified that its volume and then, was measured in its volume resistivity, and it was verified that its volume li:\DayLib\LIB E]02746a.doc:jls -81 resistivity was low enough because the measured value was 1.0 Q cm 2 Wire was coated as the first embodiment to form a coated wire for collector electrode 100. Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 9.1% 0.06%, its shunt resistance was 250 to 400 10 kQ cm 2 its series resistance was 32.9 0 cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

S**

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test 15 was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.5% on average than the initial conversion efficiency, however, no significant deterioration occurred.

(Embodiment 4) [I:\DayLib\LIBE]02746a.docjls 82- Referring to this embodiment, the case that a coated wire for collector electrode comprises Au wire, polyamide and In 2 03 will be described.

In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1A is produced as the first embodiment except that a metallic wire 101 is formed by gold, polyamide resin manufactured by Mitsubishi Chemical Industries Ltd. is used as polymeric resin which mainly constitutes paste forming a coated layer 102, and In 2 0 3 o •manufactured by Sumitomo Metal Mining Co., Ltd. of which average primary particle 10o diameter is 0.05 is used as a conductive particle.

0 The above-described paste was hardened at the temperature of 160 0 C for thirty 4 go minutes which were the standard hardening condition of the above-described hardener *000 and then, was measured in its volume resistivity, and it was verified that is volume S 15 resistivity was low enough because the measured value was 1.5 Q cm 2 The volume of a hole of this conductive adhesive was 0.04 1/g and average molecular weight of polymeric resin was ten thousand.

Wire was coated as the first embodiment to form a coated wire for collector electrode 100. Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample [I:\DayLib\LIBE]02746a.doc:jls -83 were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 9.2% 0.01%, its shunt resistance was 400 to 500 kO cm 2 its series resistance was 32.3 0 cmri 2 on average.

S The yield rate of samples of which I-V curve was normal was satisfactory because it was The reliability test of these samples was performed by the same method as that in o. •the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2% on average than the initial conversian efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for 5i collector electrode has excellent characteristics and high reliability.

(Embodiment Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver clad, urethane and carbon black will be described.

In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1B is produced as the first embodiment except that a silver-clad copper wire 100 ptm in diameter produced by forming a i:\DayLib\LBE02746a.docjs -84silver-clad metal layer 103 2 pm thick on a copper wire 101 to enhance adhesion and electrical connection with a conductive adhesive is used.

Paste for forming a conductive adhesive for a coated layer 102 is produced as follows: First, mixed solution comprising ethyl acetate 2.5 g and IPA 2.5 g as a solvent is put in a shaker for dispersion. Next, urethane resin 22.0 g which is main material is added in the above-described shaker and is 10 sufficiently stirred with a ball mill. Next, as a hardener, block isocyanate 1.1 g and glass beads for dispersion 10 g are added in the above-described solution. Next, carbon black 2.5 g of which average primary particle diameter is 0.05 pm as a conductive particle is added in the above-described solution.

The shaker in which the above-described materials were put is dispersed with a paint shaker manufactured by Toyo Precision Mechanical Equipment for ten hours.

Then, the glass beads for dispersion are removed from produced paste. The average particle diameter of the paste was measured and the measured value was approximately 1 pm. The similar result was also obtained if a bead mill was used in place of a paint shaker.

The above-described paste was hardened at the temperature of 160 °C for thirty minutes which were the standard hardening condition of the above-described 85 hardener and then, was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measured value was 0.6 Q cm 2 Next, a coated layer 403 is formed using a vertical-type wire coating machine 400 shown in Fig. 4 as described below.

A layer 102 was coated on a silver-clad layer 103 as the first embodiment to form a coated wire for collector electrode 100. Fifty solar battery modules were produced 10 using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained 0 15 because its conversion efficiency was 9.7% 0.03%, its shunt resistance was 300 to 400 kQ cm 2 its series resistance was 31.5 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was oThe reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 1.5% on average than the initial conversion efficiency, however, no 0 [I:\DayLib\LIBE02746a.docj 86 significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector electrode has excellent characteristics and high reliability.

(Embodiment 6) Referring to this embodiment, the case that a coated wire for collector electrode •10 comprises Cu wire, silver clad, phenoxy and ZnO will be described.

In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1B is S* produced as the fifth embodiment except that phenoxy resin manufactured by PKHH Tomoe Industries is used as polymeric resin which mainly constitutes paste forming a S 15 coated layer 102 and ZnO powder manufactured by Mitsui Mining and Smelting Co. Ltd.

of which average primary particle diameter is 0.1 mu is used as a conductive particle.

The above-described paste was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener S 20 and then, was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measured value was 1.3 Q cm 2 The volume of a hole of this conductive adhesive was 0.01 ml/g and the ratio of gel was 100%. The average molecular weight of polymeric resin was [I:\DayLib\LBE]02746a.doc:js 87twenty-five thousand.

Wire was coated as the fifth embodiment to form a coated wire for collector electrode 100. Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained S to because its conversion efficiency was 9.6% 0.02%, its shunt resistance was 310 to 390 kO cm 2 its series resistance was 32.4 Q cm 2 on average. The yield rates~f samples of which I-V curve was normal was satisfactory because it was 94%.

The reliability test of these samples was performed by the same method as that in .S 15 the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2% on average than the initial conversion efficiency, however, no significant deterioration occurred.

S 20 The result of this embodiment shows a solar battery using a coated wire for collector electrode has excellent characteristics and high reliability.

S (Embodiment 7) S 25 Referring to this embodiment, the case that a [L\DayLib\LIBE02746adocjIs -88 coated wire for collector electrode comprises Cu wire, silver clad, phenoxy and ZnO Al will be described.

s In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1B is produced as the fifth embodiment except that ZnO powder produced by adding aluminum to ZnO as dopant so as to lower contact resistance of a conductive particle is used.

0 i The above-described paste was hardened at the temperature of 160 0 C for thirty S lo minutes which were the standard hardening condition of the above-described hardener S and then, was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measured value was 0.9 0 cm 2 0 Wire was coated as the fifth embodiment to form a coated wire for collector 15 electrode 100. Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

\The initial characteristics of the obtained sample were measured by the same o method as that in the first embodiment and satisfactory characteristics could be obtained S 20 because its conversion efficiency was 9.6% 0.09%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 31.5 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

The reliability test of these samples was 6 ([ADayLib\LIBE]02746a.docjs 89performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was -lower 2% on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for 0 collector electrode has excellent characteristics and high reliability.

(Embodiment 8) Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver plating, urethane and Ti02 will be described.

In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1B is produced as the fifth embodiment except that a metallic layer 103 on a copper wire 101 is changed from silver clad according to the fifth embodiment to silver plating and TiO 2 manufactured by Ishihara Sangyo Kaisha of which average primary particle diameter is S 20 0.2 pm is used as a conductive particle.

The above-described paste was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener S* and then, was measured in its volume S [I:\DayLib\LBE]02746a.docjs resistivity, and it was verified that its volume resistivity was low enough because the measured value was 1.1 Q cm 2 Wire was coated as the fifth embodiment to form a coated wire for collector electrode 100.

Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same ito method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 9.5% 0.01%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 31.6 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

So: 15 The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator is in measurement of initial values, and the conversion efficiency was lower 2.3% on average than the initial conversion efficiency, however, no significant deterioration occurred.

S .o The result of this embodiment shows a solar battery using a coated wire for collector electrode has excellent characteristics and high reliability.

(i:\DayLib\LI BE]02746a.doc:j s -91 (Embodiment 9) Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, tin plating, polyamide and graphite will be described.

In this embodiment, a coated wire for collector electrode 100 shown in Fig. 1B is produced as the fifth embodiment except that a metallic layer 103 on a copper wire 101 is Se* changed from silver clad according to the fifth embodiment to tin plating, and polyamide 10 imide resin manufactured by Mitsubishi Chemical Industries Ltd. is used as polymeric resin which mainly constitutes paste and a conductive particle is changed to graphite manufactured by Tokai Carbon.

The above-described paste was hardened at the temperature of 180 0 C for thirty 15 minutes which were the standard hardening condition of the above-described hardener and then, was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measurbd value was 2.0 cm 2 The volume of a hole of this conductive adhesive was 0.01 ml/g and the average molecular weight of polymeric resin was twenty-five thousand.

f [:\DayLib\L1BEI02746a.doc:jIs -92- The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 9.3% 0.09%, its shunt resistance was 400 to 500 s kQ cm 2 its series resistance was 33.6 0 cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 94%.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test S. 10 was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.9% on average than the initial conversion efficiency, however, no significant deterioration occurred.

0 •0 S *The result of this embodiment shows a solar battery using a coated wire for 15 collector electrode according to the invention has excellent characteristics and high reliability.

(Embodiment Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver paste, urethane and carbon black will be described.

In this embodiment, a coated wire for collector electrode 100 according to the Sinvention shown in Fig. 1B is produced as the fifth embodiment except that a metallic 25 layer [r:\DayLib\LIBE]02746a.doc:jls 93 103 on a copper wire 101 is changed from silver clad according to the fifth embodiment to silver paste, 5007 manufactured by Du Pont.

For paste used for the above-described metallic layer 103, paste in which a silver particle is dispersed in epoxy resin is used.

The above-described paste was hardened at the temperature of 150 °C for thirty minutes which were the standard hardening condition of the above-described a 10 hardener and then, was measured in its volume resistivity, and it was verified that its volume 9**9*9 resistivity was low enough because the measured value was 5 x 10- 5 Q cm 2 .9 Next, a metallic layer 302 comprising the abovedescribed silver paste which is coated on a Cu wire sequentially from the innermost layer by the same method as that in the first embodiment is constituted as follows: First, a reel on which a Cu wire 302 is wound is set on a delivery reel 301 and the above-described Cu wire is stretched to a take-up reel 310. Next, the above-described silver paste 5007 is injected into a coater.

The take-up speed of Cu wire shall be 40 m/min., the hardening time 2 sec., the temperature of a drying furnace 200 °C and the diameter of the used die for enamel coating 160 pm. The above-described conditions 94 on which paste 5007 applied on wire is hardened are determined based upon the result of experiments. The thickness of formed metallic layer 103 was 5 pm on average and fluctuation of the thickness of film when wire 100 m long was coated was within ±0.2 pm.

Next, a carbon paste-coated layer 102 comprising urethane resin was formed by the same method as that in the fifth embodiment.

The thickness of the coated layer 102 was 20 pm on

S.

10 average and fluctuation of the thickness of film when a •wire 100 m long was coated was within ±1 pm.

Next, fifty solar battery modules using this wire as a coated wire for collector electrode which were constituted as in the first embodiment and shown in Fig. 8A were 15 produced.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment. First, the shunt resistance was checked and a satisfactory value could be obtained because the 20 measured value was 150 to 200 kQ cm 2 Next, the characteristics of the above-described solar battery were measured, and it was verified that such solar battery had satisfactory characteristics and such characteristics varied little because its conversion efficiency was 9.2% 0.05% and its series resistance was 31.8 0 cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it 95 was 88%.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.1% on average 0 than the initial conversion efficiency, however, no o 0 significant deterioration occurred.

10 Next, a test in which low illuminance of light was irradiated to such solar battery module under the environment where the temperature was +85 °C and the relative humidity was 85% so as to check possibility of migration of silver because silver is used for a 15 coated wire for collector electrode was continued for 100 hours.

e* Next, the shunt resistance of such sample after the above-described test was finished was measured by the same method as that in the first embodiment, as a result, the measured value was 130 to 160 kQ cm 2 and no 20 significant deterioration occurred.

o The result of this embodiment shows a solar battery using a metallic wire on which a conductive adhesive is coated according to this disclosure as a coated wire for a collector electrode has excellent characteristics and high reliability.

(Embodiment 11) In this embodiment, an amorphous solar battery 400 96 is produced according to the following procedure by the same method as that in the first embodiment except that it is constituted as a single type which is constituted only by a Si layer shown in Fig. 4A and radio-frequency (RF) plasma CVD is used for forming a semiconductor layer.

First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device 0 not shown, Ag is deposited until the film is 400 nm 10 thick, then ZnO is deposited until the film is 400 nm Sthick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a RF plasma CVD film forming system not shown, and a siliconsemiconductor layer is formed in the 15 order of n layer 403, i-layer 404 and p-layer 405.

Then, the substrate is put in a resistance heating deposition system not shown and In 2 0 3 film is formed as transparent conductive film 506 provided with a function also with anti-reflection effect. Next, fifty 20 solar battery modules were produced using the abovedescribed coated wire for a collector electrode 100 by the same method as that in the first embodiment. At this time, the above-described coated wire 100 was used at intervals of 5.5 mm.

The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be 97 obtained because its conversion efficiency was 5.2% 0.05%, its shunt resistance was 150 to 320 ko cm 2 its series resistance was 9.5 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was The reliability test of these samples was performed by the same method as that in the first 00 embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured 10 using a simulator as in measurement of initial values, 00 and the conversion efficiency was lower 2.4% on average than the initial conversion efficiency, however, no 0000 significant deterioration occurred.

The result of this embodiment shows a solar 15 battery using a collecting electrode according to this **000 disclosure has excellent characteristics and high reliability.

(Embodiment 12) s In this embodiment, an amorphous solar battery 400 0 20 is produced according to the following procedure by the same method as that in the first embodiment except that it is constituted as a double type which is constituted by two Si layers shown in Fig. 4B and RF plasma CVD is used for forming a semiconductor layer.

First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device not shown, Ag is deposited until the film is 400 nm 98 thick, then ZnO is deposited until the film is 400 nm thick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a RF plasma CVD film forming system not shown, and the bottom layer of a silicon layer is formed in the order of n layer 403, i-layer 404 and p-layer 405.

Next, similarly, the top layer of a silicon layer is sequentially formed in the order of n layer 413, i-layer 414 and p-layer 415, and as a result, a silicon semiconductor layer is deposited. Then, the substrate is put in a resistance heating deposition system not shown and In 2 0 3 film is formed as transparent conductive film 406 provided with a function also with antireflection effect.

15 Next, fifty solar battery modules were produced oo"o. using the above-described coated wire for collector electrode 100 by the same method as that in the first embodiment.

At this time, the above-described coated wire 100 was used at intervals of 5.5 mm.

20 The initial characteristics of the obtained sample *e were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 7.5% 0.01%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 23.1 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 94%.

99 The reliability test of these samples was performed by the same methodas that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 1.9% on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a soJar 10 battery using a coated wire for collector electrode according to this disclosure has excellent characteristics and high reliability.

(Embodiment 13) In this embodiment, an amorphous solar battery 400 15 is produced according to the following procedure by the same method as that in the first embodiment except that Se:' it is constituted as a double type which is constituted by Si and SiGe layers shown in Fig. 6, RF plasma CVD is used for forming a semiconductor layer, and a silicon 20 germanium semiconductor layer is used for i-layer of e the bottom layer.

First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device not shown, Ag is deposited until the film is 400 nm thick, then ZnO is deposited until the film is 400 nm thick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is 100 put in a microwave plasma CVD film forming system not shown, and the bottom layer is formed in the order of a silicon layer for n layer 403, a silicon germanium layer for i-layer 404 and a silicon layer for p-layer 405. Next, similarly, the top layer of a silicon layer is sequentially formed in the order of n layer 413, i-layer 414 and p-layer 415, and as a result, a silicon semiconductor layer is deposited. Then, the substrate is put in a resistance heating deposition system not 10 shown and In 2

O

3 film is formed as transparent conductive film 406 provided with a function also with antireflection effect.

Next, fifty solar battery modules were produced using the above-described coated wire for collector electrode 6* 15 100 by the same method as that in the first embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the first 20 embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 7.7% 0.02%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 20 0 cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

The reliability test of these samples was performed by the same method as that in the first 101 embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.0% on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar 0 battery using acoated wire for collector electrode according *0 SO to this disclosure has excellent characteristics and high 10 reliability.

*050e0 (Embodiment 14) 00 0 0:0 In this embodiment, an amorphous solar battery 400 is produced according to the following procedure by the same method as that in the first embodiment except that 15 it is constituted as a triple type which is constituted by SiC, Si and SiGe layers shown in Fig. 4C, RF plasma CVD is used for forming a semiconductor layer, and a silicon germanium semiconductor layer is used for •i-layer of the bottom layer.

00 00 20 First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device not shown, Ag is deposited until the film is 400 nm thick, then ZnO is deposited until the film is 400 nm thick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a microwave plasma CVD film forming system not shown, and the bottom layer is formed in the order of a 102 silicon layer for n layer 403, a silicon germanium layer for i-layer 404 and a silicon layer for p-layer 405. Next, similarly, the middle layer of a silicon layer is sequentially formed in the order of n layer 413, i-layer 414 and p-layer 415, further the top layer is formed in the order of a silicon layer for n layer 423, a silicon-C layer for i-layer 404 and a silicon layer for p-layer 405, and as a result, a semiconductor layer is deposited. Then, the substrate is put in a 10 resistance heating deposition system not shown and In 2 0 3 •film is formed as transparent conductive film 406 oprovided with a function also with anti-reflection :effect.

Next, fifty solar battery modules were produced using the above-described wire coating for collector 060 electrode 100 by the same method as that in the first embodiment.

•0 .0 The initial characteristics of the obtained sample were measured by the same method as that in the first embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 9.5% 0.06%, its shunt resistance was 260 to 330 kQ cm 2 its series resistance was 33.7 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of 103 the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.4% onaverage than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector electrode according to this disclosure has excellent characteristics and high 06 reliability.

10 (Embodiment 0 In this embodiment, a monocrystalline solar battery 500 is produced according to the following procedure by the same method as that in the first embodiment except that it is constituted by a monocrystalline solar battery (monocrystalline Si) shown in Fig. First, a silicon monocrystal of which valence electron is controlled by Czochralski process so that it is p type is produced, the monocrystal is sliced, 20 and a silicon wafer 500 approximately 300 pm thick is .0 produced. Further, a n'-type layer 501 is formed in a diffusion process by applying P 2 0 5 on the abovedescribed wafer. Next, silver paste is printed on the rear side of p-layer 500 by a screen printing machine not shown, heated and burnt, and as a result, the lower electrode 502 is formed. Next, the above-described coated wire for collector electrode 100 used in the first embodiment 104 is formed on n*-type layer 501 on the side of light irradiated face by the above-described method. Then, SiO 2 film 504 is formed as anti-reflection film by a sputtering process. Next, fifty solar battery modules shown in Fig. 8B by the same method as that in the first embodiment were produced. At this time, the above-described coated wire 100 was used at intervals of 8.5 mm.

The initial characteristics of the obtained sample 10 were measured by the same method as that in the first embodiment and satisfactory characteristics could be 0o o obtained because its conversion efficiency was 15.8%

S.

S: 0.09%, its shunt resistance was 500 to 760 kQ cm 2 its series resistance was 2.8 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 98%.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next,- the solar battery characteristics of 20 the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 1.9% on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this.embodiment shows a solar battery using a coated wire for collector electrode according p to this disclosure has excellent characteristics and high 105 reliability.

(Embodiment 16) In this embodiment, a polycrystalline solar battery 600 is produced according to the following procedure by the same method as that in the first embodiment except that it is constituted by a polycrystalline solar battery (polycrystalline Si) shown in Fig. 6.

First, a polycrystalline ingot is produced by a 10 casting process, the polycrystal is sliced, and n-type layer 601 is formed on the obtained polycrystalline silicon wafer 600 in a diffusion process by applying

P

2 0 5 on the above-described wafer. Next, silver paste is printed on the rear side of p-layer 600 by a screen printing machine not shown, heated and burnt, and as a result, the lower electrode 602 is formed. Next, the above-described coated wire for collector electrode 100 used in the first embodiment is formed on n'-type layer 601 on the side of light irradiated face by the above-described method. Then, SiO 2 film 604 is formed as anti- 0 reflection film by a sputtering process. Next, fifty solar battery modules shown in Fig. 8B by the same method as that in the first embodiment were produced.

At this time, the above-described coated wire 100 was used at intervals of 8 mm.

The initial characteristics of the obtained sample were measured by the same method as that in the first 106 embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 13.8% 0.01%, its shunt resistance was 450 to 650 kQ cm 2 its series resistance was 2.6 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 94%.

The reliability test of these samples was performed by the same method as that in the fir;t 1. embodiment. Next, the solar battery characteristics of 10 the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2% on average than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar 0000 battery using a wire coating for collector electrode according to this disclosure has excellent characteristics and high *0 %00 reliability.

(Embodiment 17) 20 In this embodiment, a thin-film polycrystalline 0 solar battery 600 is produced according to the following procedure by the same method as that in the first embodiment except that it is constituted by a thin-film polycrystalline solar battery (thin-film polycrystalline Si) shown in Fig. 7.

First, a metallic Si substrate 701 sufficiently degreased and cleaned is put in a microwave plasma CVD 107 film forming system not shown so as to form n layer 702. Next, this substrate is put in a heating furnace not shown so as to polycrystallize n layer 702. Then, the substrate is put in a microwave plasma CVD film forming system not shown so as to form p-layer 703.

Further, the substrate is put in a sputtering device not shown and ITO film is formed as transparent conductive film 704 provided with a function also with anti-reflection effect. Next, a collecting electrode 10 705 is formed on the above-described transparent conductive film 704 by the same method as that in the a.

first embodiment and fifty solar battery modules shown in Fig. 8B were produced.

The initial characteristics of the obtained sample 15 were measured by the same method as that in the first ee. embodiment and satisfactory characteristics could be obtained because its conversion efficiency was 12.5% 0.01%, its shunt resistance was 400 to 510 kQ cm 2 its series resistance -was 20 Q cm 2 on average. The yield rate of samples of which I-V curve was normal was satisfactory because it was 92%.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.1% on average 108 than the initial conversion efficiency, however, no significant deterioration occurred.

(Embodiment 18) This embodiment is different from the first embodiment in that resistivity of a conductive adhesive O e 10 is varied within the range of 0.005 to 200 0 cm. For a

S.

S

method for varying resistivity of a conductive adhesive, mixing ratio (in weight) of polymeric resin and a conductive particle in conductive coating material was varied to any of 5:95, 10:90, 20:80, 80:20, 90:10, 95:5.

This embodiment is similar to the first embodiment *eee in other ways.

SC

0.e Ten triple cells shown in Fig. 4C were produced according to the same procedure as that in the first 20 embodiment except that these conductive adhesives were used and similarly evaluated. Table 1 shows the result.

109 [Table 1] 9 *t Resistivity (Q cm) 0.005 0.01 1 100 200 Initial status Transformation efficiency(%) 8.2 9.6 9.6 9.4 Series resistance(O cm 2 31.4 31.4 31.8 32.3 39.8 Shunt resistance(kn cm 2 4.9 25.9 250 320 350 Status after confidence test Transformation efficiency(%) 7.2 9.5 9.5 9.3 7.3 Series resistance(O cm 2 31.3 31.6 31.9 32.6 50.3 Shunt resistance(ko cm 2 2.3 25.9 251 325 350 Table 1 shows that initial shunting can be controlled by setting the resistivity of a coated layer 102 to 0.01 0 cm or more and more stable conversion efficiency can be obtained. Table 1 also shows that series resistance can be reduced by setting the resistivity to 100 Q cm or less and higher conversion efficiency can be obtained. Table 1 further shows that increase of series resistance and lowering of conversion efficiency after a reliability test can be reduced and a solar battery using a collecting electrode according to the invention has high reliability.

(Embodiment 19) This embodiment is different from the first embodiment in that the heating pressure-bonding temperature of a conductive adhesive is varied in the 110 range of 50 to 300 For temperature for heating and pressure-bonding a coated wire for collector electrode 100, measurement was performed at four different temperature of 100, 160, 200 and 250 Used block isocyanate is similar to that in the first embodiment and its dissociative temperature is 150 *C.

In other ways this embodiment is similar to the first embodiment.

S* Ten triple cells shown in Fig. 4 were produced and similarly evaluated according to the same procedure as that in the first embodiment except that heating pressure-bonding temperature was set as their temperature. Table 2 shows the result.

[Table 2] egos 0 0O

C

Heating pressure- 100 160 200 250 bonding temperature

C)

Initial status Transformation efficiency(%) 6.3 9.0 9.6 9.6 Series resistance(Q cm

T

51.3 31.4 31.3 31.2 Shunt resistance(kQ cm 2 57.3 253 352 390 Status after confidence test Transformation efficiency(%) 3.1 8.7 9.6 9.6 Series resistance(Q cm 2 121 36.5 31.3 31.2 Shunt resistance(ko cm 2 56.8 254 356 389 111 Table 2 shows that series resistance can be reduced by setting heating pressure-bonding temperature to the dissociative temperature or higher of coated layer resin and higher conversion efficiency can be obtained. The table 2 also shows increase of series resistance after a reliability test and lowering of conversion efficiency can be reduced and a solar battery using a collecting electrode according to this S" disclosure has high reliability.

(Embodiment a 4, :This embodiment is different from the first 0 embodiment in that the heating pressure-bonding time of Sa conductive adhesive is, varied in the range of 10 to seconds. For heating pressure-bonding time of a coated wire for collector electrode 100, four different time of 0 45 and 60 seconds was set. To check the hardening *o •leo factor of a conductive adhesive under such a condition, an amount eluted into a solvent before and after immersion was measured and as a result, the ratio of 20 gel was 15%, 80% and 100% respectively. Used block

S

isocyanate is similar to that in the first embodiment 0 and its dissociative temperature is 150 °C.

In other ways this embodiment is similar to the first embodiment.

Ten triple cells shown in Figs 4A to 4C were produced and similarly evaluated according to the same procedure as that in the first embodiment except that 112

S

0S 0O @6 0O

S

6 0 0 6** for heating pressure-bonding temperature, the abovedescribed temperature was set. Table 3 shows the result.

[Table 3] Heating contact bonding 10 20 45 time(sec.) Initial status Transformation 6.9 8.5 9.5 9.6 efficiency(%) Series 43.5 36.2 31.4 31.2 resistance(O cm 2 Shunt 25.1 96.3 265 312 resistance(ko cm 2 Status after confidence test Transformation efficiency(%) 5.2 8.0 9.5 9.6 Series resistance(O cm 2 58.3 40.2 31.5 31.3 Shunt resistance(kQ cm 2 20.3 96.5 264 315 Table 3 shows that series resistance can be reduced and higher conversion efficiency can be obtained by adjusting heating pressure-bonding time and setting the ratio of gel of coated layer resin to or more. The table 3 also shows increase of series resistance after a reliability test and lowering of conversion efficiency can be reduced and a solar battery using a collecting electrode according to this disclosure has high reliability.

(Embodiment 21) 0 0 @00S 00 6 6 113- In this embodiment, the amount of a hardener applied to a conductive adhesive was measured. The ratio in weight of urethane resin mainly used for a coated layer of a coated wire for collector electrode 100 and block isocyanate used for a hardener was changed to 100:1, 50:1, 20:1 and 10:1. At this time, the ratio of gel of a conductive adhesive was 15%, 85% and 100% respectively. Used block isocyanate is similar to that in the first embodiment and its dissociative temperature is 150 0

C.

In other ways this embodiment is similar to the first embodiment.

Ten triple cells shown in Figs. 4A to 4C were produced and evaluad according to the same procedure as that in the first embodiment. Table 4 shows the result.

S6 S S 0 S pI:\DayLib\LIBE]02746a.doc:jls 114 [Table 4] 0 00 0 0 0 00 0 0 *0 a 00 00 0 0 a 0

S

seem 00 C0 a 00 *e 0

S

Ratio of resin/hardener 100:1 50:1 20:1 10:1 Initial status Transformation efficiency(%) 7.8 8.7 9.7 9.6 Series resistance(O cm 2 39.9 33.8 31.0 31.7 Shunt resistance(kQ cm 2 15.3 165 369 374 Status after confidence test Transformation efficiency(%) 6.1 8.4 9.7 9.6 Series resistance(" cm 2 51.2 38.9 31.1 31.9 Shunt resistance(ko cm 2 14.2 172 368 372 Table 4 shows that series resistance can be reduced and higher conversion efficiency can be obtained by adjusting an amount of a hardener and setting the ratio of gel of coated layer resin to or more. Table 4 also shows that increase of series resistance and lowering of conversion efficiency after a reliability test can be reduced and the table 3 also shows increase of series resistance after a reliability test and lowering of conversion efficiency can be reduced and a solar battery using a collecting electrode according to this disclosure has high reliability.

(Embodiment 22) Referring to this embodiment, the case that a 115 coated wire for collector electrode comprises Cu wire, carbon black, urethane will be described.

In this embodiment, a coated wire for collector electrode 200 shown in Fig. 2A is produced according to the follow procedure.

For metallic wire 201, a copper wire 100 pm in diameter is used.

Carbon paste No. 1 for forming a conductive 0adhesive for the first layer 202 is produced according 10 to the following procedure. First, mixed solution comprising BCA 2.5 g and xylene 2.5 g as a solvent is 00000" put in a shaker for dispersion. Next, urethane resin 22.0 g which is main material is added in theiabovedescribed shaker and is sufficiently stirred with a ball mill. Next, as a hardener, block isocyanate 1.1 g and glass beads for dispersion 10 g are added in the above-described solution.

Next, carbon black 2.5 g of which average primary particle diameter-is 0.05 pm as a conductive particle 20 is added in the above-described solution.

The shaker in which the above-described materials are put is dispersed with a paint shaker manufactured by Toyo Precision Mechanical Equipment for ten hours.

Then, the glass beads for dispersion are removed from produced paste. The average particle diameter of the paste was measured and the measured value was approximately 1 pm. The similar result was also 116 obtained if a bead mill was used in place of a paint shaker.

The above-described paste No. 1 was hardened at the temperature of 160 °C for thirty minutes which were the standard hardening condition of the above-described hardener and then, was measured in its volume resistivity, and it was verified that its volume resistivity was low enough because the measured value was 1.0 Q cm 2 The volume of a hole of this conductive 10 adhesive was 0.01 ml/g and the ratio of gel was 100%.

The average molecular weight of polymeric resin was one thousand.

Next, carbon paste No. 2 for forming a conductive adhesive the second layer 203 is produced according to the following procedure. First, for a solvent, cyclohexanone 2.5 g is put in a shaker for dispersion.

Next, urethane resin 22.0 g which is main material and phenoxy resin 2.0 g are added in the above- S"described shaker and are sufficiently stirred with a ball mill. Next, as a hardener, block isocyanate 1.1 g and glass beads for dispersion 10 g are added in the above-described solution. Next, carbon black 2.5 g of which average primary particle diameter is 0.05 pm as a conductive particle is added in the above-described solution. This is dispersed by the same method as that in the case of paste No. i.

The above-described paste No. 2 was hardened at 117 the temperature of 160 °C for thirty minutes which were the standard hardening condition of the above-described hardener, then the volume resistivity of it was measured, and it was verified that it was low enough because the measured value was 0.5 Q cm.

Next, the first layer 202 and the second layer 203 are sequentially formed in the order described above using a vertical type of wire coater 300 shown in.Fig.

3 as follows: 10 First, a reel on which a metallic wire 307 is wound is set on a delivery reel 301 and the abovedescribed metallic wire is stretched to a take-up reel 310. Next, the above-described paste No. 1 is injected into a coater.

The take-up speed of metallic wire was 40 m/min., the residence time was 2 sec., the temperature of a drying furnace 306 was 350 °C and the metallic wire was coated five times. A die for enamel coating 110 to 200 pm in diameter was sequentially used. Paste No. 1 was sufficiently hardened on the above-described conditions, and adhesion and resistance to a solvent of paste were satisfactory. The thickness of the first layer 202 was 5 pm on average and fluctuation of the thickness of film when wire 100 m long was coated was within ±1 pm.

Next, the second layer 203 comprising paste No. 2 is formed by the same method as described above except 118 the described below.

A reel 310 on which the wire on which the abovedescribed first layer 202 was coated is wound is set on a delivery reel 301 and the above-described wire is stretched to a take-up reel 310. Next, the abovedescribed carbon paste No. 2 is injected into a coater.

The take-up speed of the wire was 40 m/min., the drying time was 2 sec., the temperature of a drying -furnace 306 was 120 °C and the wire was coated five i1' 10 times. A die for enamel coating 150 to 200 pm in diameter was used. Paste No. 2 applied on the abovedescribed wire was in a condition not hardened yet in which its solvent was volatilized. The thickness of the second layer 203 was 20 pm on average and fluctuation of the thickness of film when the wire 100 m long was coated was within ±0.5 pm.

Next, in an embodiment according to the invention, a pin-junction triple amorphous solar battery 400 with constitution of layers shown in Figs. 4A to 4C provided with a grid electrode 30 cm in grid length is produced.

First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device not shown, Ag is deposited until the film is 400 nm thick, then ZnO is deposited until the film is 400 nm thick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a microwave plasma CVD film forming system not 119 shown, and the bottom layer is formed in the order of a silicon layer for n layer 403, a silicon germanium layer for i-layer 404 and a silicon layer for p-layer 405. Next, similarly, the middle layer is sequentially formed in the order of a silicon layer for n layer 413, a silicon germanium layer for i-layer 414 and a silicon layer for p-layer 415, further the top layer of a silicon layer is formed in the order of n layer 423, ilayer 424 and p-layer, and as a result, a semiconductor 10 layer is deposited. Then, the semiconductor layer is S* put in a resistance heating deposition system not shown and ITO film is formed as transparent conductive film 506 provided with a function also with anti-reflection effect. Next, unnecessary transparent conductive film is removed using etching paste which mainly comprises ferric chloride and a printing machine on the market so that the solar battery substrate 401 is 30 x 30 cm in size and effective area of the cell is 900 cm 2 Next, hard copper positive electrode 802 and negative electrode 803 are provided outside the effective area, as a collecting electrode 804 the above-described coated wire 100 is stretched between positive electrodes 802 at intervals of 7 mm so that the wire is contained in the effective area and is fixed using an ultraviolet hardening adhesive.

Next, the above-described collecting electrode 804 is heated and crimped using a heater not shown so as to 120 stick the collecting electrode on the cell face of the solar battery substrate 401 and as a result, a triple cell 30 x 30 in size shown in Fig. 8A is produced. The collecting electrode is heated at the temperature of 200 °C for 45 seconds under pressure of 1 kg/cm 2 Next, this sample is encapsulated according to the following procedure. Kroehnkite glass and EVA are laminated on the upper and rear surfaces of the solar battery substrate 801, further fluororesin film ETFE is 10 laminated on the upper and rear surfaces, the substrate is put in a vacuum laminater and is left at the temperature of 150 °C for an hour for lamination.

Fifty solar battery modules were produced by the same method.

The initial characteristics of the obtained sample were measured according to the following procedure.

First, volt-ampere characteristic of the sample in an off state was measured, its shunt resistance on an inclination in the vicinity of the origin was 200 to 500 kQ cm 2 and it was a satisfactory value. Next, the solar battery characteristics were measured using a pseudo solar light source (hereinafter called a simulator) with a solar spectrum of AM 1.5 global and quantity of light of 100 mW/cm 2 and its conversion efficiency was satisfactory and there was little dispersion because the measured value was 9.6% 0.02%.

Its series resistance was 32.0 0 cm 2 on average and 121 satisfactory. The yield rate of samples of which I-V curve was normal was 98% and satisfactory.

The reliability test of these samples was performed by the same method as that in the first embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2% on average than the initial conversion efficiency, however, no *99*.

10 significant deterioration occurred.

'9 9.

go" Further, to check moisture resistance and a leakage factor of these samples, a reliability test was performed as follows: First, a sample was put in a eooconstant temperature and humidity oven with a window through which light could be transmitted which could control temperature and humidity, and was left at the 9.999 temperature of +85 °C and relative humidity of When the temperature and humidity in it was sufficiently balanced, quantity of light of 100 mW/cm 2 with a solar spectrum of AM 1.5 global was irradiated by a simulator installed outside the window.

Next, the solar battery characteristics of a sample after a reliability test was finished were measured using a simulator as in measurement of initial values and its conversion efficiency was lower 2% on average than its initial conversion efficiency, however, no significant deterioration occurred.

122- The result of this embodiment shows a solar battery using a metallic wire on which a conductive adhesive according to this disclosure is coated as a coated wire for a collector electrode has excellent characteristics and high reliability.

(Comparative Embodiment 2) Referring to this comparative embodiment, the case that a coated wire for a collector electrode comprises Cu wire, Ag and polyester will be described.

For comparison, paste 5007 including a silver particle manufacture by Du Pont Swas coated on wire to form a coated wire for a collector electrode 100. The volume of a hole of this conductive adhesive was 0.1 ml/g. Fifty solar battery modules were produced using the coated wire for collector electrode 100 by the same method as that in s1 the first embodiment.

The initial characteristics of the obtained sample were measured, its conversion efficiency was 7.5% fluctuation of the values was large. Its shunt resistance was 1.8 k cm 2 on average and fluctuation of the values was large. Its series resistance was 20 32.0 0 cm 2 on average. The yield rate of samples of which I-V curve was normal was low because it was 54%.

Samples of which shunt resistance were normal were selected of these samples and a reliability test of moisture resistance and leakage was performed by the same ooo.: 25 method as that in the twenty-second embodiment.

S

[i:\DayLib\LBE02746a.docjs 123- Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, its conversion efficiency was lower 20% than its initial conversion efficiency and its shunt resistance was smaller than a half of its initial shunt resistance value.

(Embodiment 23) Referring to this embodiment, the case that a coated wire for a collector electrode comprises Cu wire, carbon black and epoxy, and carbon black and butyral will be described.

"This embodiment is similar to the twenty-second embodiment except that epoxy Sresin manufactured by Epicoat Petrochemical Shell Epoxy is used as polymeric resin o 15 which mainly constitutes paste No. 1 for forming a conductive adhesive for a coated wire for collector electrode 200 shown in Fig. 2A, and butyryl resin manufactured by Eslec BL-S Sekisui Chemical is used as polymeric resin which mainly constitutes paste No. 2.

The volume of a hole of this paste No. 1 was 0.01 ml/g and the ratio of gel was 20 100%. The average molecular weight of polymeric resin wasone thousand.

The above-described paste No. 1 was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described

S

Ii:\DayLib\LIBE]02746a.docjs 124hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 2.1 Q cm.

Wire was coated as in the twenty-second embodiment to form a coated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire for collector electrode 200 by the same method as that in the twenty-second embodiment.

The initial characteristics of the obtained sample were measured by the same 0o method as that in the first embodiment, its conversion efficiency was 9.4% 0.06%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 32.2 Q cn- on average, Sand satisfactory characteristics could be obtained. The yield rate of samples of which I-V Scurve was normal was 96% and satisfactory. A reliability test of these samples was Sperformed as in the twenty-second embodiment. Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2.6% on average than its initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for 44 20 collector electrode according to this disclosure has satisfactory characteristics and high reliability.

*00 0

S

0 •000*b p:\DayLib\LIBE]02746a.docjs 125 (Embodiment 24) Referring to this embodiment, the case that a coated wire for collector electrode comprises Ag wire, carbon black and urethane, and ITO and urethane will be described.

This embodiment is similar to the twenty-second embodiment except that a silver wire is used as a metallic wire 201 for a coated wire for a collector electrode 200 shown in Fig. 2A, and ITO power manufactured by HYX Sumitomo Metal Mining of which average primary particle diameter is 0.05 pm is used as a conductive particle of paste No.

2 for forming a conductive adhesive.

S

•The above-described paste No. 2 was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described is1 hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 1.0 Q cm.

Wire was coated as in the twenty-second embodiment to form a coated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire 20 for collector electrode 200 by the same method as that in the twenty-second embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 9.5% 0.07%, its shunt resistance was 300 to 500 kQ cm 2 its *0005 2S [I :\DayLib\LIBEI02746a.docj Is 126 series resistance was 32.5 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 94% and satisfactory.

A reliability test of these samples was performed as in the twenty-second embodiment. Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2.3% on average than its initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for o collector electrode has satisfactory characteristics and high reliability.

(Embodiment 0 00 Referring to this embodiment, the case that a coated wire for collector electrode comprises Ag wire, graphite and urethane, and SnO 2 and urethane will be described.

20 This embodiment is similar to the twenty-second embodiment except that a gold wire is used as a metallic wire 201 for a coated wire for collector electrode 200 shown in Fig. 2A, graphite power manufactured by Tokai Carbon of which average primary particle diameter is 0.05 [tm is used as a conductive particle of past No. 1 for forming a conductive 0 [i:\DayLib'LIBE102746a.docjjls 127adhesive, and SnO2, power manufactured by Mitsui Mining and Smelting Co., Ltd. of which average primary particle diameter is 0.2 im is used as a conductive particle of paste No. 2.

The above-described paste No. 1 was hardened at the temperature of 180 0 C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 1.8 Q cm.

The above-described paste No. 2 was hardened at the temperaturez-f 160 OC for thirty minutes which were the standard hardening condition of the above-described S* hardener, then its volume resistivity was measured, and it was verified that its volume S •resistivity was low enough because the measured value was 1.4 Q cm.

Wire was coated as in the first embodiment to form a coated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire for collector electrode 200 by the same method as that in the twenty-second embodiment.

0* 20 The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 9.3% S0.01%, its shunt resistance was 230 to 420 kQ cm 2 its series resistance was 33.0 Q cm 2 on average, and satisfactory characteristics could be obtained. The 0 [I:\DayLib\LIB E]02746a.doc:jls 128yield rates of samples of which I-V curve was normal was 96% and satisfactory.

A reliability test of these samples was performed as in the twenty-second S embodiment. Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2.1% on average than its initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector electrode according to this embodiment has satisfactory characteristics and high S reliability.

(Embodiment 26) 00 Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver clad, carbon black and urethane will be described.

This embodiment is similar to the twenty-second embodiment except that a silver 20 clad copper wire 100 pm in diameter produced by forming a silver clad metallic layer 203 0*0* having the thickness of 2 pm on a copper wire 201 is used for a coated wire for collector electrode 200 shown in Fig. 2A so as to enhance adhesion to a conductive adhesive and conductivity. Wire was coated as in the first embodiment to form a coated wire for collector electrode 200. Further, fifty solar battery S *0 0 [I:\DayLib\LIBE]02746a.doc:jIs 129modules were produced using the collecting electrode 100 by the same method as that in the twenty-second embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 9.7% 0.02%, its shunt resistance was 400 to 500 kQ cm 2 its series resistance was 31.8 0 cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 98% and satisfactory.

A reliability test of these samples was preformed as in the tWventy-second embodiment. Next, the solar battery characteristics of a sample after the test was finished 0 were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2% on average than its initial conversion efficiency, however, no significant deterioration occurred.

0 The result of this embodiment shows a solar battery using a coated wire for collector electrode has satisfactory characteristics and high reliability.

20 (Embodiment 27) Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver clad, ZnO and urethane, and In 2 0 3 and urethane will be [:\DayLib\LIBE]0274 130described.

This embodiment is similar to the twenty-second embodiment except that for a coated wire for collector electrode 200 shown in Fig. 2A, a silver clad copper wire is used, ZnO power manufactured by Mitsui Mining and Smelting Co., Ltd. of which average primary particle diameter is 0.1 pm is used as a conductive particle of paste No. 1 for forming a conductive adhesive, and In 2 0 3 powder manufactured by Sumitomo Metal Mining Co., Ltd. of which average primary particle diameter is 0.05pm is used as a conductive particle of paste No. 2.

The above-described paste No. 1 was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 1.4 0 cm The above-described paste No. 2 was hardened at the temperature of 160 0 C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume 20 resistivity was low enough because the measured value was 0.7 0 cm.

Wire was coated as in the twenty-second embodiment to form a coated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire for collector (:\Dav Lib\LIBE]02746a.doc.jls 131 electrode 200 by the same method as that in the twentysecond embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 9.6% 0.03%, its shunt resistance was 320 to 390 kQ cm 2 its series resistance was 32.1 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 10 96% and satisfactory.

S.

:A reliability test of these samples was performed as in the twenty-second embodiment. Next, the solar :battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2% on average than its initial .00O conversion efficiency, however, no significant deterioration occurred.

s The result of this embodiment shows a solar 20 battery using a coated wire for collector electrode has satisfactory characteristics and high reliability.

(Embodiment 28) Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver plating, carbon black and phenol, and carbon black and polyamide will be described.

132 This embodiment is similar to the twenty-second embodiment except that for a coated wire for collector electrode 200 shown in Fig. 2A, a silver-plated wire 100 pm in diameter produced by plating silver clad with silver is used as a metallic layer 203, phenol resin manufactured by Dainippon and Chemicals, Inc. is used as main material for polymeric resin of paste No. 1 for forming a conductive adhesive, 00 and polyamide resin manufactured by Mitsubishi Kasei S: o 10 Corporation is used as main material for polymeric resin of paste No. 2. The volume of a hole of this paste No. 1 was 0.01 ml/g and the ratio of gel was 100%. The average molecular weight of polymeric resin was one thousand.

The above-described paste No. 1 was hardened at 00. the temperature of 160 °C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low 20 enough because the measured value was 1.5 0 cm.

The above-described paste No. 2 was hardened at the temperature of 160 OC for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 0.8 0 cm.

Wire was coated as in the first embodiment to form 133 acoated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire for collector electrode 200 by the same method as that in the twentysecond embodiment.

The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 9.3% 0.01%, its shunt resistance was 400 to 500 ko cm 2 its series resistance was 32.7 0 cm 2 on average, and 10 satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 96% and satisfactory.

A reliability test of these samples was performed *0 as in the twenty-second embodiment. Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion 0000 efficiency was lower 2.8% on average than its initial conversion efficiency, however, no significant S 20 deterioration occurred.

The result of this embodiment shows a solar Sbattery using a coated wire for collector electrode has satisfactory characteristics and high reliability.

(Embodiment 29) Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, tin plating, 134 ZnO 2 +Al, carbon black and urethane, and TiO 2 and urethane will be described.

This embodiment is similar to the twenty-second embodiment except that for a coated wire for collector electrode 200 according to the invention shown in Fig. 2A, a tin-plated copper wire 100 pm in diameter produced by plating silver clad with tin is used as a metallic layer 203, ZnO 2 powder of which primary particle diameter is 0.05 pm produced by adding aluminum to ZnO 2 10 as dopant so as to reduce contact resistance is used as a conductive particle of paste No. 1 for forming a conductive adhesive, and Ti02 powder of which average primary particle diameter is 0.05 pm is used as a see* conductive particle of paste No. 2. The volume of a hole of this paste No. 1 was 0.01 ml/g and the ratio of gel was 100%. The average molecular weight of S.C polymeric resin was one thousand.

The above-described paste No. 1 was hardened at the temperature of 160 'C for thirty minutes which were 20 the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 0.9 0 cm.

The above-described paste No. 2 was hardened at the temperature of 160 'C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and 135 it was verified that its volume resistivity was low enough because the measured value was 1.5 Q cm.

The initial characteristics of the obtained sample were measured by the same method as that in the twenty- S* 10 second embodiment, its conversion efficiency was 9.4% 00* se.e 0.01%, its shunt resistance was 360 to 430 kQ cm 2 its S* series resistance was 32.6 Q cm 2 on average, and 00*-0; satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 94% and satisfactory.

A reliability test of these samples was performed as in the twenty-second embodiment. Next, the solar 0".:04 battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2.1% on average than its initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector electrode according to this disclosure has satisfactory characteristics and high reliability.

136 (Embodiment Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, gold plating, carbon black and phenoxy, and carbon black and polyamide will be described.

This embodiment is similar to the twenty-second embodiment except that for a coated wire for collector electrode 200 according to the invention shown in Fig. 2A, a goldplated copper wire 100 pm in diameter produce by 10 plating silver clad with gold is used as a metallic S*0* layer 203, phenoxy resin manufactured by Tomoe S- Industries is used as main material for .a polymeric 0* resin of paste No. 1 for forming a conductive adhesive, and polyamide imide resin manufactured by Mitsubishi Kasei Corporation is used as a main material for polymeric resin of paste No. 2.

The above-described paste No. 1 was hardened at the temperature of 160 'C for thirty minutes which were the standard hardening condition of the above-described too hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low enough because the measured value was 1.0 0 cm.

The above-described paste No. 2 was hardened at the temperature of 180 °C for thirty minutes which were the standard hardening condition of the above-described hardener, then its volume resistivity was measured, and it was verified that its volume resistivity was low 137 enough because the measured value was 2.0 Q cm.

Wire was coated as in the first embodiment to form a coated wire for collector electrode 200. Fifty solar battery modules were produced using the coated wire for collector electrode 200 by the same method as that in the twenty-second embodiment The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 9.5% 10 0.05%, its shunt resistance was 240 to 350 k2 cm 2 its series resistance was 34.1 Q cm 2 on average, and satisfactory characteristics could be obtained. The 0 yield rate of samples of which I-V curve was normal was *0 96% and satisfactory.

A reliability test of these samples was performed as in the twenty-second embodiment. Next, the solar "00" battery characteristics of a sample after the test was ,finished were measured using a simulator as in 00.

measurement of initial values, and its conversion efficiency was lower 3.0% on average than its initial conversion efficiency, however, no significant deterioration occurred.

(Embodiment 31) 138 Referring to this embodiment, the case that a coated wire for collector electrode comprises Cu wire, silver paste, and urethane and carbon black will be described.

This embodiment is similar to the twenty-sixth embodiment except that in a coated wire for collector electrode 200 according to the invention shown in Fig. 2A, material for a metallic layer 203 on a copper wire 201 is changed from silver clad according to the twenty-sixth embodiment to silver paste 5007 manufactured by Du Pont.

Paste used for the above-described metallic layer 205 is produced by dispersing silver particles in epoxy resin. A metallic layer 203 is coated as in the tenth embodiment. Next, S the first layer 202 and the second layer 203 are coated in the order described above to form a coated wire for collector electrode. Fifty solar battery modules are produced using the coated wire for collector electrode 200 by the same method as that in the twenty-sixth embodiment.

o i The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 9.5% 0.08%, its shunt resistance was 190 to 300 kQ cm 2 its series resistance was 32.0 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples 20 of which I-V curve was normal was 94% and satisfactory.

0* A reliability test of these samples was performed 0

S

[I:\DayLib\LIBE]02746a.doc:js 139 as in the twenty-second embodiment. Next, the solar battery characteristics of a sample after the test was finished were measured using a simulator as in measurement of initial values, and its conversion efficiency was lower 2.4% on average than its initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar battery using a coated wire for collector elect-rode 1 0 according to the invention has satisfactory characteristics and high reliability.

(Embodiment 32) In this embodiment, a single-type amorphous solar battery 400 constituted only by a Si layer shown in Fig. 4A is produced according to the following procedure by the same method as that in twenty-sixth embodiment except that radio-frequency (RF) plasma CVD is used for forming a semiconductor layer.

First, SUS430BA substrate 401 sufficiently 20 degreased and cleaned is put in a DC sputtering device *not shown, Ag is deposited until the film is 400 nm thick, then ZnO is deposited until the film is 400 nm thick so. as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a RF plasma CVD film forming system not shown, and a silicon semiconductor layer is formed in the order of n layer 403, i-layer 404 and p-layer 405.

140 Then, the substrate is put in the sputtering device not shown and In 2 0 3 film is formed as transparent conductive film 406 provided with a function also with anti-reflection effect.

Next, fifty solar battery modules were produced using the above-described coated wire for collector electrode 100 by the same method as that in the twenty-sixth embodiment.

At this time, the above-described coated wire 200 was used at intervals of 5.5 mm. The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 5.2% 0.05%, its shunt resistance was 150 to 320 kQ cm 2 its series resistance was 9.5 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 92% and satisfactory.

000 A reliability test of these samples was performed by the same method as that in the twenty-second embodiment. Next, the solar battery characteristics of the samples 15 after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.4% on average than the initial o000 conversion efficiency, however, no significant deterioration occurred.

0 The result of this embodiment shows a solar battery using a coated wire for 20 collector electrode according to this disclosure has excellent characteristics and high *6 [i:\DayLib\LIBE]02746a.docj Is 141 reliability.

(Embodiment 33) In this embodiment, a double-type amorphous solar battery 400 constituted by a Si layer and a Si layer shown in Fig. 4A is produced according to the following procedure by the same method as that in twenty-sixth embodiment except that radio-frequency (RF) plasma CVD is used for forming a semiconductor layer.

First, SUS430BA substrate 401 sufficiently degreased and cleaned is put in a DC sputtering device *not shown, Ag is deposited until the film is 400 nm thick, then ZnO is deposited until the film is 400 nm thick so as to form the lower electrode 402. The substrate is taken out of the sputtering device and is put in a RF plasma CVD film forming system not shown, and the bottom layer of a silicon layer is formed in the order of n layer 403, i-layer 404 and p-layer 405.

*O*

Next, similarly the top layer of a silicon layer is sequentially formed in the order of n layer 413, 20 i-layer 414 and p-layer 415 so as to deposit a silicon semiconductor layer. Then, the substrate is put in a resistance heating deposition system not shown and In 2

O,

film is formed as transparent conductive film 406 provided with a function also with anti-reflection effect.

Next, fifty solar battery modules were produced using the above-described a coated wire for collector electrode 100 by 142 the same method as that in the first embodiment. At this time, the above-described coated wire 200 was used at intervals of 6 mm.

The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 7.5% 0.08%, its shunt resistance was 400 to 500 ko cm 2 its series resistance was 23.1 Q cm 2 on average, and satisfactory characteristics could be obtained. The ,e 10 yield rate of samples of which I-V curve was normal was 0 Sso 96% and satisfactory.

A reliability test of these samples was performed *0 0 by the same method as that in the twenty-second embodiment. Next, the solar battery characteristics of 0 00 15 the samples after the test was finished were measured S. using a simulator as in measurement of initial values, and the conversion efficiency was lower 1.9% on average than the initial conversion efficiency, however, no significant deterioration occurred.

20 The result of this embodiment shows a solar battery using a coated wire for collector electrode according to this disclosure having excellent characteristics and high reliability.

(Embodiment 34) In this embodiment, a monocrystalline solar battery 500 is produced according to the following procedure by the same method as that in the twenty- 143 sixth embodiment except that it is constituted by a monocrystalline solar battery (monocrystalline Si) shown in Fig. First, a silicon monocrystal of which valence electron is controlled by CZ process so that it is p type is produced, the monocrystal is sliced, and a silicon wafer 500 approximately 300 pm thick is produced. Further, a n4-type layer 501 is. formed in a diffusion process by applying P 2 0, on the above- S10 described wafer. Next, silver paste is printed on the 66 rear side of p-layer 500 by a screen printing machine not shown, heated and burnt, and as a result, the lower electrode 502 is formed. Next, the above-described a coated wire for collector electrode 100 used in the first 15 embodiment is formed on n'-type layer 501 on the side of light f* ft irradiated face by the above-described .method. Then, SiO, film 504 is formed as anti-reflection film by a sputtering process. Next, fifty solar battery modules by the same method as that in the twenty-sixth 20 embodiment were produced. At this time, the abovedescribed coated wire 200 was used at intervals of mm.

The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 15.8% 0.01%, its shunt resistance was 500 to 760 kQ cm 2 its series resistance was 2.8 Q cm 2 on average, and 144 satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 98% and satisfactory.

A reliability test of these samples was performed by the same method as that in the twenty-second embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 1.9% on average e 10 than the initial conversion efficiency, however, no significant deterioration occurred.

The result of this embodiment shows a solar 0 battery using a coated wire for collector electrode 200 according to this disclosure has excellent characteristics 15 and high reliability.

(Embodiment In this embodiment, a polycrystalline solar *o battery 600 is produced according to the following procedure by the same method as that in the twentysixth embodiment except that it is constituted by a polycrystalline solar battery (polycrystalline Si) shown in Fig. 6.

First, a polycrystalline ingot is produced by a casting process, the polycrystal is sliced, and n*-type layer 601 is formed on the obtained polycrystalline silicon wafer 600 in a diffusion process by applying

P

2 0 5 on the above-described wafer. Next, silver paste 145 is printed on the rear side of p-layer 600 by a screen printing machine not shown, heated and burnt, and as a result, the lower electrode 602 is formed. Next, the above-described coated wire for collector electrode 200 used in the twenty-sixth embodiment is formed on n+-type layer 601 on the side of light irradiated face by the above-described method.

Then, SiO 2 film 604 is formed as anti-reflection film by a sputtering process. Next, fifty solar battery modules were produced by the same method as that in the first embodiment.

At this time, the above-described coated wire 200 was used at intervals of 8.0 mm.

The initial characteristics of the obtained sample were measured by the same method as that in the twenty-second embodiment, its conversion efficiency was 13.8% 0.05%, its shunt resistance was 450 to 650 kQ cm 2 its series resistance was 2.6 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 96% and satisfactory.

A reliability test of these samples was performed by the same method as that in the twenty-second embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured using a simulator as in measurement of initial values, and the conversion efficiency was lower 2% on average than the initial conversion 20 efficiency, however, no ooo [I:\DayLib\LIB E]02746a.doc:jls 146 significant deterioration occurred.

(Embodiment 36) In this embodiment, a thin film polycrystalline solar battery 700 is produced according to the following procedure by the same method as that in 10 twenty-sixth embodiment except that a solar battery is 0* constituted by a thin film polycrystalline solar 6 battery (thin film polycrystalline Si) shown in Fig. 7.

First, a metallic Si substrate 701 sufficiently degreased and cleaned is put in a microwave plasma CVD film forming system not shown to form n layer 702.

DiDO Next, the substrate is put in a heating furnace not shown and polycrystalline n layer 702. Next, the substrate is put in a microwave plasma CVD film forming system not shown to form p-layer 703. Further, it is 20 put in a sputtering device not shown and ITO film is formed as transparent conductive film 704 provided with a function also with anti-reflection effect. Next, a grid 705 is formed on the above-described transparent conductive film 704 by the same method as that in the twenty-sixth embodiment, and fifty solar battery modules are produced. The yield rate of samples of which I-V curve was normal was 94% and satisfactory.

147 The initial characteristics of the obtained sample were measured by the same method as that in the twentysecond embodiment, its conversion efficiency was 15.5% 0.01%, its shunt resistance was 400 to 510 k92 cm 2 its series resistance was 4.5 Q cm 2 on average, and satisfactory characteristics could be obtained. The yield rate of samples of which I-V curve was normal was 94% and satisfactory.

A reliability test of these samples was performed 10 by the same method as that in the twenty-second embodiment. Next, the solar battery characteristics of the samples after the test was finished were measured i* using a simulator as in measurement of initial values, and the conversion efficiency was lower 2.1% on average than the initial conversion efficiency, however, no o. significant deterioration occurred.

The result of this embodiment shows a solar 9S battery using a coated wire for collector electrode according to this disclosure has excellent characteristics 0 and high reliability.

(Embodiment 37) This embodiment is different from the twenty-sixth embodiment in that resistivity of a conductive adhesive is varied within the range of 0.005 to 200 0 cm. For a method for varying resistivity of a conductive adhesive, mixing ratio (in weight) of polymeric resin and a conductive particle in conductive coating 148 a a a.

a (a a a..

material was varied to any of 5:95, 10:90, 20:80, 80:20, 90:10, 95:5.

This embodiment is similar to the twenty-sixth embodiment in other ways.

Ten triple cells shown in Fig. 4C were produced according to the same procedure as that in the twentysixth embodiment except that these conductive adhesives were used and similarly evaluated. Table 5 shows the result.

[Table Resistivity (Q cm) 0.005 0.01 1 100 200 Initial status Transformation efficiency(%) 8.2 9.6 9.6 9.4 Series resistance(2 cm 2 31.4 31.4 31.8 32.3 39.8 Shunt resistance(k cm 2 4.9 25.9 250 320 350 Status after confidence test Transformation efficiency(%) 7.2 9.5 9.5 9.3 7.3 Series resistance( cm 2 31.3 31.6 31.9 32.6 50.3 Shunt resistance(ko cm 2 2.3 25.9 251 325 350 Table 5 shows that initial shunting can be controlled by setting the resistivity of a coated layer 203 to 0.01 0 cm or more and more stable conversion efficiency can be obtained. Table 5 also shows that series resistance can be reduced by setting the resistivity to 100 Q cm or less and higher conversion 149 efficiency can be obtained. Table 5 further shows that increase of series resistance and lowering of conversion efficiency after a reliability test can be reduced and a solar battery using a collecting electrode according to this disclosure has high reliability.

(Embodiment 38) This embodiment is different from the first 0• •embodiment in that the heating pressure-bonding 0-) temperature of a conductive adhesive is varied in the range of 50 to 300 For temperature for heating and pressure-bonding a coated wire for collector electrode 200, measurement was performed at four different temperature of 100, 160, 200 and 250 Used block isocyanate is 15 similar to that in the first embodiment and its 0 dissociative temperature is 150 °C.

In other ways this embodiment is similar to the twenty-sixth embodiment.

Ten triple cells shown in Figs. 4A to 4C were 00 20 produced and similarly evaluated according to the same procedure as that in the twenty-sixth embodiment except that heating pressure-bonding temperature was set as their temperature. Table 6 shows the result.

150 [Table 6] *r 0 6 0 *660 0 6S *6 0 06 6 0006 0 *6 Heating pressure- 100 150 200 250 bonding temperature Initial status Transformation efficiency(%) 7.3 9.0 9.6 9.6 Series resistance(o cm 2 41.3 31.4 31.3 31.2 Shunt resistance(ko cm 2 57.3 253 352 390 Status after confidence test Transformation efficiency(%) 6.1 8.7 9.6 9.6 Series resistance(O cm 2 53.3 36.5 31.3 31.2 Shunt resistance(kQ cm 2 56.8 254 356 389 6006 0 6006 0606 6 0 @6 @0 0 600 0 006006 0 00 00 *r 0

S

Table 6 shows that series resistance can be reduced by setting heating pressure-bonding temperature to the dissociative temperature or higher of coated layer resin and higher conversion efficiency can be obtained. The table 6 also shows increase of series resistance and lowering of conversion efficiency after a reliability test can be reduced and a solar battery using a collecting electrode according to this disclosure has high reliability.

(Embodiment 39) This embodiment is different from the twenty-sixth embodiment in that the heating pressure-bonding time of -151 a conductive adhesive is varied in the range of 10 to 60 seconds. For heating pressurebonding time of a coated wire for collector electrode 200, four different time of 10, 20, and 60 seconds was set. To check the hardening factor of a conductive adhesive under such a condition, an amount eluted into a solvent before and after immersion was measured and as a result, the ratio of gel was 15%, 80% and 100% respectively.

Used block isocyanate is similar to that in the first embodiment and its dissociative temperature is 150 0

C.

In other ways this embodiment is similar to the twenty-sixth embodiment.

Except that the temperatures for heating pressure-bonding are these temperatures, ten pieces of a triple cell in Fig. 7 are made in the same procedure as for Embodiment 26 and the same evaluation is performed. The result is shown in Table 7.

*see *555 00 [i:\DayLib\LIBE]02746a.doc:jIs 152 [Table 7] ir. Cr.

-S

S.

9.

9 (a S 5.9.

(9 9 .9 Heating contact bonding 10 30 45 time(sec.) Initial status Transformation efficiency(%) 6.9 8.5 9.5 9.6 Series resistance(Q cm 2 43.5 36.2 31.4 31.2 Shunt resistance(kQ cm 2 25.1 96.3 265 .312 Status after confidence test Transformation efficiency(%) 5.2 8.0 9.5 9.6 Series resistance(o cm 2 58.3 40.2 31.5 31.3 Shunt resistance(ko cm 2 20.3 96.5 264 315 As apparent from Table 7, higher transformation efficiency can be obtained due to reduction of the series resistance caused by the heating pressurebonding temperature higher than the dissociation temperature of coating-layer resin. In addition, .it is also clear that higher reliability is secured because of less increase of the series resistance and less decrease of the transformation efficiency after the confidence test.

(Embodiment In this embodiment, the amount of a curing agent for conductive bonding material is examined. In other words, a variety of ratio is applied to the weight ratio of urethane resin used as chief agent for a coat 153 es 0s 6 0 6e i 0 5

S.

5

S

layer of the coated wire for current collector electrode 200 to be blocked isocyanate used as a curing agent, such as 100:1, 50:1, 20:1, and 10:1. The gel separation percentage of the conductive bonding material is 5, 15, 85, and 100 under the above conditions. Dissociation temperature of the actually-used blocked isocyanate is 150 oC in the same way as for Embodiment 1.

Other conditions are the same as for Embodiment 26.

Ten pieces of triple cell shown in Figs. 4A to 4C are madeand the same evaluation as for Embodiment 26 is performed. The evaluation result is shown in Table 8.

[Table 8] Resin-curing agent ratio 100:1 50:1 20:1 10:1 Initial status Transformation efficiency(%) 7.8 9.2 9.7 9.6 Series resistance(Q cm 2 39.9 33.8 31.0 31.7 Shunt resistance(kQ cm 2 19.3 185 389 394 Status after confidence test Transformation efficiency(%) 6.1 8.4 9.7 9.6 Series resistance(o cm 2 51.2 38.9 31.1 31.9 Shunt resistance(kQ cm 2 14.9 177 378 382

OS'S

0

S

0O

S

0 0e 0 154 As apparent from Table 8, higher transformation efficiency can be obtained since the series resistance is decreased by the heating pressure-bonding temperature higher than the dissociation temperature of the blocked isocyanate which is a curing agent contained in the conductive bonding material. In addition, it is also clear that higher reliability is secured because of less increase of the series resistance and less decrease of the transformation 10 efficiency after the confidence test.

*fr es a ft 4 I ,•oo 155 TABLE 9 3*

V

*4* S

S

V S

S.

OS

S

*n Embodiment Comparison Embodiment Embodiment Embodiment 1 1 2 3 4 Wire material Copper Copper Copper Silver Gold Wire surface None None None None None First layer filler None None None None None First layer resin None None None None None First layer crosslink- None None None None None ing density First layer curing agent None None None None None First layer solvent None None None None None First layer film gauge None None None None None (um) First layer specific resistance None None None None None (Q cm) Second layer filler Carbon Carbon ITO SnOz 1n 2 0 3 Second layer resin Urethane Fluorine Butyral Urethane Polyamide Second layer curing agent B.I B.I B.I B.I Second layer Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPA acetate IPA acetate IPA acetate IPA acetate IPA Second layer 2 2 film gauge 20 20 20 20 Second layer specific 0.6 0.1 1.2 5.0 resistance Temperature /time during 200/45s 200/20M 200/45s 2 00/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS Type of solar Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ battery SiGe SiGe SiGe SiGe SiGe Type of confidence HF HF HF HF HF test Initial yield 94 64 94 92 Efficiency before test 9.6±0.02 9.0±1.2 9.7±0.05 9.1±0.06 9.2±0.01 Efficiency after test -11% -2% Rs before test (Q cm 2 32.0 32.1 32.5 32.9 32.3 Rs after test(kQ cm 2 No change 62 No change No change No change RshDk before test 200-300 4-300 200-300 250-400 400- 500 RshDk after test No change No change No change No change No change

S

156 S. Se

S

5 0 5 0 *005

S

TABLE Embodiment Embodiment Embodiment Embodiment Embodiment Embodiment 6 7 8 9 Wire material Copper Copper Copper Copper Copper Copper Wire. Silver Silver Silver Silver Tin Silver surface cladding cladding cladding plating plating pasting First layer filler None None None None None None First layer resin None None None None None None resin First layer crosslink- None None None None None None ing density First layer curing agent None None None None None None First layer solvent None None None None None None First layer film gauge None None None None None None (pm) First layer specific resistance None None None None None None (Q cm) Second layer filler Carbon ZnO 2 ZnO 2 +AI TiO 2 Graphite Carbon Second layer Polyamideresin l Urethane Butyral Phenoxy Urethane Polyamide Urethane resin imide Second layer curing agent B.I B.I B.I B.I B.I B.I curing agent Second layer Ethyl Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPA acetate IPA acetate IPA acetate IPA acetate IPA acetate IPA Second layer film gauge 20 20 20 20 20 film gauge Second layer specific 0.6 1.3 0.9 1.1 2.0 0.6 resistance Temperature /time during 200/45s 200/45s 200/45s 200/45s 200/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS SUS Type of solar Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ battery SiGe SiGe SiGe SiGe SiGe SiGe Type of confidence HF HF HF HF HF HF test Initial yield 96 94 92 92 94 88 Efficiency before test 9.7±0.03 9.6±0.02 9.6±0.08 9.5±0.01 9.3±0.09 9.2±0.08 Efficiency after test -2.1% after test Rs before test 2 31.4 31.7 31.5 31.6 33.6 31.8 test (Q cm 2 Rs after testk cm 2 No change No change No change No change No change No change test(k cm RshDk efore test 300-400 310-390 400-500 320-380 400-500 150-200 before test RshDk after test No change No change No change No change No change No change 157 0S @0 0 60 00 0 00 0 *0 S S 00 S @0 US 0

S

0000 00 S. 0 TABLE 11 Embodiment Embodiment Embodiment Embodiment Embodiment Embodiment 1 11 12 13 14 Wire material Copper Copper Copper Copper Copper Copper Wire surface None None None None None None First layer filler None None None None None None First layer resin None None None None None None First layer crosslink- None None None None None None ing density First layer curing agent None None None None None None curing agent First layer solvent None None None None None None First layer film gauge None None None None None None (um) First layer specific resistance None None None None None None (Q cm) Second layer filler Carbon Carbon Carbon Carbon Carbon Carbon Second layer resin Urethane Urethane Urethane Urethane Urethane Urethane Second layer curing agent B.I B.I B.I B.I B.I B.I curing agent Second layer Ethyl Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPAacetate IPAacetate IPAacetate IPAacetate IPA acetate IPA Second layer 20 2 film gauge 20 20 20 20 20 Second layer specific 0.6 0.6 0.6 0.6 0.6 0.6 resistance Temperature /time during 200/45s 200/45s 200/45s 200/45s 200/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS Wafer Typeof solar Si/SiGe/ SiC/Si/ Singlebattery SiGe Si single Si/Si Si/SiGe SiGe crystal Si Type of confidence HF HF HF HF HF HF test Initial yield 94 90 94 92 92 98 Efficiency before test 9.6 5.2±0.05 7.5±0.01 7.7±0.02 9.5±0.06 15.8 Efficiency after test -1.9% Rs before test 32.0 9.5 23.1 21.1 33.7 2.8 test Q cm 2 Rs after test(Q cm 2 No change No change No change No change No change No change RshDk before test 200-300 150-320 400-500 250-310 260-330 500-760 RshDk after test No change No change No change No change No change No change .00.

00. 0 5 158

S.

S. TABLE 12 Embodiment mbodiment Embbodiment Eodiment Embodiment Embodiment 16 17 18 19 20 21 Wire material Copper Copper Copper Copper Copper Copper Wire surface None None None None None None First layer filler None None None None None None First layer resin None None None None None None resin First layer crosslink- None None None None None None ing density First layer curing agent None None None None None None First layer solvent None None None None None None First layer film gauge None None None None None None (Pm) First layer specific resistance None None None None None None (Q cm) Second layer filler Carbon Carbon Carbon Carbon Carbon Carbon Second layer resind l Urethane Urethane Urethane Urethane Urethane Urethane resin Second layer curing agent BI B.I B.I B.I B.I B.I Second layer Ethyl Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPA acetate IPA acetate IPA acetate IPA acetate IPAacetate IPA Second layer 20 20 film gauge 20 20 20 20 20 Second layer specific 0.6 0.6 0.005-200 0.6 0.6 0.6 resistance Temperature /time during 200/45s 2 0 0/45s 200/45s Tempera- Time range 200/45s bonding ture range Substrate Wafer Metal Si SUS SUS SUS- SUS Type of solar Poly- Thin-film battery crysta- poly Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ battery crysta- poly-_ lline Si crystal SiGe SiGe SiGe SiGe Type of confidence HF HF HF HF HF HF test Initial yield 96 92 Efficiency before test 13.8% 12.5% Efficiency after test Rs before 2.6 test (Q cm) 2 6 4 Rs after test (Q cm 2 No change No change RshDK before test 450-650 400-510 RshDk after test No change No change S S 159 TABLE 13 Embodiment Comparison Emodiment bodimen t Embodiment Em mnt 22 2 23 24 Wire material Copper Copper Copper Silver Gold Wire surface None None None None None First layer filler Carbon None Carbon Carbon Graphite First layer resin Urethane None Epoxy Urethane Urethane First layer curing agent B.I None B.I B.I B.I curing agent First layer solvent BCA. xylene None BCA. xylene BCA. xylene BCA. xylene First layer film gauge 5 None 5 5 (pm) First layer specific resistance 1.0 None 2.1 1.0 1.8 (Q cm) Second layer filler Carbon Silver Carbon ITO Sn0 2 Second layer resin Urethane Polyester Urethane Urethane Urethane Second layer curing agent B.I B.I B.I B.I curing agent Second layer Cyclo- Cyclo- Cyclo- Cyclosolvent hexanone Carbitol hexanone hexanone hexanone Second layer film gauge 20 20 20 20 Second layer specific 0.5 0.5 0.5 1.0 1.4 resistance Temperature /time during 2 0 0/45s 150/30m 200/45s 200/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS Type of solar Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ battery SiGe SiGe SiGe SiGe SiGe Type of confidence HF/HHL HHL HF/HHL HF/HHL HF/HHL test Initial yield 98 54 96 94 96 Efficiency before test 9.6±0.02 7.5±1.8 9.4±0.06 9.5±0.07 9.3±0.01 Efficiency after test -20% -2.1% Rs before test cm) 32.0 32.0 32.2 32.5 33.0 test (Q cm

Z

Rs after test (Q cm 2 No change No change No change No change No change RshDk before test 200-500 1.8 400-500 300-500 230-420 RshDk after test No change 0.8 No change No change No change 160 TABLE 14 a Embodiment Embodiment Embodiment Embodiment Embodiment Embodiment 26 27 28 29 30 31 Wire material Copper Copper Copper Copper Copper Copper Wire Silver Silver Silver Tin Gold Silver surface cladding cladding plating plating plating pasting First layer filler Carbon ZnO Carbon ZnO2 +A1 Carbon Carbon First layer resin Urethane Urethane Phenol Urethane Phenoxy Urethane First layer B.I B.I B.I B.I B.I B.I curing agent First layer solvent BCA. xylene BCA. xylene BCA. xylene BCA. xylene BCA. xylene BCA. xylene First layer film gauge 5 5 5 5 5 (pm) First layer specific resistance 1.0 1.4 1.5 0.9 1.0 (Q cm) Second layer filler Carbon In 2 0 3 Carbon TiO 2 Carbon Carbon filler Second layer Polyamideresin l Urethane Urethane Polyamide Urethane mide Urethane resin imide Second layer curing agent .I B.I B.I B.I B.I B.I curing agent Second layer Cyclo- Cyclo- Cyclo- Cyclo- Cyclo- Cyclosolvent hexanone hexanone hexanone hexanone hexanone hexanone Second layer lm ga20 20 20 20 20 film gauge Second layer specific 0.5 0.7 0.8 1.5 2.0 resistance Temperature /time during 200/45s 200/45s 200/455 200/45s 200/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS SUS Typeof solar Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ battery SiGe SiGe SiGe SiGe SiGe SiGe Type of confidence HF/HHL HF/HHL HF/HHL HF/HHL HF/HHL HF/HHL test Initial yield 98 96 96 94 96 94 Efficiency before test 9.7±0.02 9.6±0.01 9.3±0.01 9.4±0.01 9.5±0.05 9.4±0.08 Efficiency after test -2.4% Rs before s 31.8 32.1 32.7 32.6 34.1 32.0 test (Q cm 2 Rs after Sc 2 No change No change No change No change No change No change test (9 cm RshDk before test 400-500 320-390 400-500 360-430 240-350 190-300 RshDk after test No change No change No change No change No change No change 161 TABLE *0 Embodiment Embodiment Embodiment Embodiment Embodiment 26 32 33 34 Wire material Copper Copper Copper Copper Copper Wire Silver Silver Silver Silver Silver surface clading clading clading -clading clading First layer filler Carbon Carbon Carbon Carbon Carbon First layer First layer Urethane Urethane Urethane Urethane Urethane First layer curing agent B.I B.I B.I B.I B.I curing agent First layer Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPA acetate IPA acetate IPA acetate IPA acetate IPA First layer film gauge 5 5 5 5 (pm) First layer specific resistance 1.0 1.0 1.0 1.0 (Q cm) Second layer filler Carbon Carbon Carbon Carbon carbon Second layerer resin Urethane Urethane Urethane Urethane Urethane Second layer curing agent B.I B.I B.I B.I B.I Second layer Cyclo- Cyclo- Cyclo- Cyclo- Cyclosolvent hexanone hexanone hexanone hexanone hexanone Second layer film gauge 20 20 20 20 Second layer specific 0.5 0.5 0.5 0.5 resistance Temperature /time during 200/45s 200/45s 200/45s 200/45s 200/45s bonding Substrate SUS SUS SUS SUS SUS Poly- Type of solar Si/SiGe/ Si single Si/Si Single- crystabattery SiGe crystal Si lline Si Type of confidence HF/HHL HF/HHL HF/HHL HF/HHL HF/HHL test Initial yield 98 92 96 98 96 Efficiency before test 9.7±0.02 5.2±0.05 7.5±0.08 15.8±0.01 13.8±0.05 Efficiency after test -19% -2% Rs before test cm 2 31.8 9.5 23.1 2.8 2.6 Rs after s( 2 No change No change No change No change No change test cm RshDk before test 400-500 150-320 400-500 500-760 450-650 RshDk after test No change No change No change No change No change 162 TABLE 16 *5

S

nt EmbodimeEmbodiment Embodiment Embodiment Embodiment 36 37 38 39 Wire material Copper Copper Copper Copper Copper Wire Silver Silver Silver Silver Silver surface cladding cladding cladding cladding cladding First layer filler Carbon Carbon Carbon Carbon Carbon First layer resin Urethane Urethane Urethane Urethane Urethane First layer curing agent B.I B.I B.I B.I B.I First layer Ethyl Ethyl Ethyl Ethyl Ethyl solvent acetate IPA acetate IPAacetate IPAacetate IPA acetate IPA First layer film gauge 5 5 5 5 (Pm) First layer specific resistance 1.0 1.0 1.0 1.0 (Q cm) Second layer filler Carbon Carbon Carbon Carbon Carbon Second layer resin Urethane Urethane Urethane Urethane Urethane resin Second layer curing agent B.I B.I B.I B.I B.I curing agent Second layer Cyclo- Cyclo- Cyclo- Cyclo- Cyclosolvent hexanone hexanone hexanone hexanone hexanone Second layer Silm gauge 20 20 20 20 film gauge Second layer Amount of specific 0.5 0.005-200 curing resistance agent Temperature /time during 200/45s 200/45s Tempera- Time range 200/45s bonding ture range Substrate SUS SUS SUS SUS SUS Type of solar Thin-film Si/SiGe/ Si/SiGe/ Si/SiGe/ Si/SiGe/ polybattery crystal SiGe SiGe SiGe SiGe Type of confidence HF/HHL HF/HHL HF/HHL HF/HHL HF/HHL test Initial yield 94 Efficiency before test 12.5±0.01 Efficiency after test -2.1% Rs before test (Q cm 2 4 Rs after test(Q cm 2 No change RshDk before test 400-510 RshDk after test .No change 163

S

0055

S

0O 5.

S.

O

S

06000 (Embodiment 41) In this embodiment, a photovoltaic element is made, having coated wires for current collector electrodes to which heat-hardening conductive bonding material is applied, and its performance is confirmed in the procedure described below.

The following describes a method of preparing paste No. 4 for forming the heat-hardening conductive bonding material constituting the coat layer of the 10 coated wires for current collector electrodes.

Mixed solvent containing 17.4 g of butyl carbitol acetate and 11.6 g of methyl ethyl ketone were taken into a shaker for dispersion as solvent.

Butyral resin BL-S manufactured by Sekisui Chemical Co., Ltd. used as chief agent of binder was added by 8.9 g to the solvent in the shaker and it was stirred with a ball mill until it was sufficiently dissolved.

As a curing agent, 1.40 c of blocked isocyanate B- 815N manufacturedby Takeda Chemical Industries, Ltd.

and 15 g of glass beads for dispersion were added to said solvent.

As conductive grains, 5.1 g of Conductex 975 beads manufactured by Colombian Carbon, Ltd. were added to said solvent and it was placed statically until the conductive grains were settle- out sufficiently in said solvent.

Dispersion was made for the shaker containing the woos 0 000

S

0 b0 i 00 00 h S

S

164 above materials for 12 hours by using a paint shaker manufactured by Toyo Seiki Seisakuzyo, Ltd. The time was obtained through an experiment for finding a lapse of time in which volume resistivity of the paste No. 4 was decreased to the lowest level.

Afterwards, glass beads for dispersion were removed from the paste No. 4. The paste No. 4 was cured under the standard curing conditions on said curing agent, 160 OC of the temperature and 30 min. of the time and 10 its volume resistivity was measured. As a result of Sthe measurement, 0.8 Qcm was obtained, by which it could be confirmed that the resistivity was sufficiently low.

By using a longitudinal type of a wire coater 300 shown in Fig. 3, silver-cladded copper wire having a diameter of 100 pm was coated with the paste No. 4.

For a die 605 for enamel coating used for wire coating, was used a PVF die manufactured by Osaka Diamond, Ltd.

As for a drying oven 606, two IR ovens SS-09 (infrared ovens) manufactured by Sakaguchi Dennetsu, Ltd. were placed in a longitudinal direction and assembled at the position opposite to each other so as to be used. An atmospheric temperature in the drying oven was set to a desired level by an operation with a temperature controller 311. In pulling up the Cu wire, a servo motor (not shown) was used for controlling a pulling-up speed. An orientation roll driving gear 309 were -165 placed in a side of a wire roller reel. Additionally, an LS-3100/3034 film-thickness measuring apparatus 307 manufactured by Keyence, Ltd. was placed at an outlet of the drying oven to measure a thickness of the coat of the conductive bonding material and then it was measured.

The following describes conditions on forming said paste No. 4 as a first coat layer 202.

The wire rolling speed is 8.9 mm/s, the curing 10 time is 60 sec., the temperature in the drying oven is 280 and a bore diameter of the die used for enamel coating is 180 pm. The conditions were obtained through an experiment for finding a status in which curing reaction of the paste No. 4 progressed enough S" 15 without any falling off of the paste No. 4.

Concretely, it was confirmed by ultrasonic cleaning of the coated wire for 30 sec. with methyl ethyl ketone to .ee check that any conductive bonding material made of the Ce paste No. 4 would-not fall off. The conductive bonding material made of the paste No. 4 applied to the silvercladded copper wire existed in a cured status with progressed crosslinking. The thickness of the first coat layer 202 was 11 pm at an average and a deflection of the thickness of the coat was within a range of ±1 pm as a result of the coating in 100 m length.

The following describes forming conditions on a second coat layer 203 to which said heat-hardening 166 conductive bonding material (paste No. 4) is applied and a method of fabricating the coated wires for current collector electrodes used for the photovoltaic element.

The wire rolling speed is 8.9 mm/s, the drying time is 60 sec., the temperature in the drying oven is 120 0 C, and a bore diameter of the die used for enamel coating is 200 rm. The conditions were obtained through an experiment for finding a status in which the temperature was lower than the dissociation temperature of blocked isocyanate without any tack of the conductive bonding material No. 1 applied to said wire but with 1io sufficient adhesion to the wire. The conductive bonding material made of the paste No. 4 applied to said wire existed in a thermoplastic status with the solvent votltilized. The thickness of a coat layer 303 is 8 tm at an average and a deflection of the thickness of the coat was within a range of ±1.5 p.m as a result of the coating in 100 m length.

The following describes a:process of fabricating ten photovoltaic element modules.

Fig. 10 illustrates a photovoltaic element module having coated wires for current collector electrodes 1004 created in said method. A substrate 1001 which was 20 used had a pin-typed double cell coated with CVD on an SUS substrate combined with a minus electrode. In addition, a transparent conductive coat made of In203.

piADayLib\LIBE]02746a.docjs 167was formed as a plus electrode in the incident side of light.

The substrate 1001 has an effective area of 30 x 30 cm- Patterns are printed on the substrate by using etching paste containing ferric chloride as chief ingredient, a commercial printer, and a printing plate for etching and undesired portions of transparent conductive coat was removed.

Next, a plus electrode 1002 of hard copper and a minus electrode 1003 10 were set outside the effective area, and said coated wires for current collector electrodes 1004 were expanded between the both plus electrodes 202 so that they wae within the effective area at 7-mm intervals and they were fixed temporarily with ultraviolet curing adhesive outside the plus electrode, in other words, outside the effective area.

Afterwards, said coated wires for current collector electrodes 1004 were contact-bonded with heating on a cell surface of the substrate 1001. It was performed under the conditions of 1 kg/cm 2 pressure and heating conditions based on a profile such as increasing the temperature up to 200 0 C in 60 min. in a ramp state and then cooling them in 20 min. The heating conditions were obtained through an experiment with 20 measuring adhesivity of the coated wires for current collector electrodes to the cell surface of the photovoltaic elements and observing a sectional configuration of the current collector [I:\DayLib\LiBE]02746a.docjls 168 o electrodes which were bonded.

Although the plus electrode is kept in conduction with the current collector electrodes in said heating pressure-bonding process, dotting with silver paste or soldering can be performed to enhance the confidence.

The heating pressure-bonding is performed with a device having a capability of simultaneous heating and pressurizing for a vacuum laminator.

Ten photovoltaic element modules were fabricated 10 in the above process.

oooe• The following describes a result of investigating initial characteristics of the obtained samples (in other words, the above photovoltaic element modules).

Voltage-current characteristicsin a dark state of said samples were measured. The shunt resistance was examined on the basis of an inclination around the origin. As a result of the examination, favorable Svalues, 200 kQcm 2 to 500 k cm 2 were obtained.

By using a simulated sun light source (hereinafter "simulator") having 100 mW/cm 2 quantity of light in the global sun light spectrum, characteristics of the solar battery for said samples were examined with measurement. Characteristics of measured transformation efficiency 7.9±0.02 were favorable and relatively uniform.

Next, encapsulation of said samples was performed in the following procedure. Clean glass and EVA were 169 cladded on the both sides of the substrate 1001, then further fluoroplastic film ETFE was laminated T n the both sides of it, and it was put into a vacuum laminator for lamination with keeping its temperature 150 °C for 60 min.

A confidence test was performed for the samples after the lamination. The test was based on the o,0 temperature and relative humidity cycle test NA2 defined in an environmental test method and an 10 endurance test method of crystal-system solar battery modules of Japan Industrial Standard C8917.

A cycle test was repeated 20 times by putting the samples into a constant temperature and humidity bath whose inside temperature and humidity were controllable *se 06 15 to change the temperature from -40 °C to +85 °C (relative humidity: 85 Afterwards, when a.

a characteristics of the solar battery were examined for the samples after the completion of the test by using the simulator in the same manner as for the initial q 20 state, a decrease of 2 at an average was obtained in comparison with the initial transformation efficiency without any significant deterioration.

As a result of this embodiment, it has been understood that the photovoltaic element of this disclosure has favorable characteristics and secures higher reliability.

(Comparison 3) 170- This example differs from Embodiment 41 in that thermoplastic conductive bonding material is used instead of the heat-hardening conductive bonding material used in Embodiment 41. Coated wires for current collector electrodes and samples were made by using thermoplastic conductive bonding material 107-25 manufactured by CMI, Ltd.

for a first coat layer 202 shown in Fig. 2A.

The first coat layer 202 was formed on the conditions below by using said conductive bonding material 107-25 to make the coated wires for current collector 10o electrodes.

The wire rolling speed is 8.9 mm/s, the drying time is 60 sec., the temperature in the drying oven is 120 0 C, and a bore diameter of the die used for enamel coating is 180 ipm. The thickness of a coat layer 202 is 8 utm at an average and a deflection of the thickness of the coat was within a range of ±1.5 pm as a result of the coating in 100 m length.

The second coat layer 203 was formed on the same conditions by using conductive bonding material made of the paste No. 4 which was the same as for 20 Embodiment 1.

Next, as the same manner as for Embodiment 41, said current collector electrodes 1004 were contact-bonded with heating on the cell surface of the substrate S 1001. It was performed under the conditions of 1 kg/cm 2 pressure and heating conditions S based on a profile such as increasing the temperature up to 150 -5 based on a profile such as increasing the temperature up to 150 °C II:\DayLib\LIBE02746a.docjs 171 in 40 min. in a ramp state and then cooling them in min.

In addition, ten photovoltaic element modules were fabricated in the same manner as for Embodiment i.

As a result of encapsulation of these samples in the same manner as for Embodiment 41 for measurement of initial characteristics, were obtained transformation efficiency 7.8 at an average and series resistance 27 RQcm 2 "1 0 As the same manner as for Embodiment 41, a cycle .00. test was repeated 20 times by putting the samples into the constant temperature and humidity bath whose inside temperature and humidity were controllable to change the temperature from -40 'C to +85 °C (relative 15 humidity: 85 Afterwards, when characteristics of ooo.the solar battery were examined for the samples after the completion of the test by using the simulator in the same manner as for the initial state. A decrease of 10 at an average was obtained in comparison with the initial transformation efficiency, which was a significant deterioration.

The deterioration is caused by an increase of the series resistance, such as, for example, an increase of an interface resistance between metal wire and thermoplastic bonding material due to a change of humidity and an increase of volume resistivity due to deterioration of the conductive bonding material.

172 (Embodiment 42) In this embodiment, were examined effects of coating of the moisture barrier paint for ten samples fabricated in the same manner as for Embodiment 41 being placed in a state before encapsulation.

Other characteristics are the same as for (Embodiment 41) When initial characteristics of the samples were measured in the same manner as for Embodiment 41, 10 characteristics of measured transformation efficiency 4.*e4 7.9±0.02 and series resistance 24 Qcm 2 were favorable and relatively uniform.

Said samples were hardened by drying on temperature conditions of increasing the temperature 15 from 80 °C to 190 °C in a ramp state in a hot-air ooo• drying oven after they were coated by hard coat material, Fine Hard manufactured by Toa Nenryo Kogyo S• K.K. with a spray.

When characteristics of the samples after thehard coating were gauged by using said simulator, the transformation efficiency 7.8 and series resistance 28 Qcm 2 were obtained without any significant deterioration.

(Comparison 4) In this embodiment, were examined effects of coating of the moisture barrier paint for ten samples fabricated in the same manner as for Comparison 3 being 173 placed in a state before encapsulation.

Other characteristics are the same as for Embodiment 41.

When initial characteristics of the samples were measured in the same manner as for Embodiment 41, characteristics of measured transformation efficiency 7.9±0.02 and series resistance 24 Ocm 2 were favorable and relatively uniform.

In the same manner as for Embodiment 42, said 10 samples were hardened by drying on temperature oeo o conditions of increasing the temperature from 80 °C to 190 °C in a ramp state in a hot-air drying oven after they were coated by hard coat material, Fine Hard manufactured by Toa Nenryo Kogyo K.K. with a spray.

15 When characteristics of the samples after the hard e coating were gauged by using said simulator, the transformation efficiency 5.5 and series resistance S• 60 Qcm 2 were obtained, which was a significant deterioration. The deterioration may be caused by an increase of the volume resistivity due to peeling of the conductive bonding material on the electrode metal caused by the hard coat solvent soaking inside the electrodes and deterioration of the thermoplastic conductive bonding material caused by heating in a hardening process of the coat material.

(Embodiment 43) 174- This embodiment differs from Embodiment 41 in that a mixture of carbon black and urethane resin is used for a binder of the conductive bonding material instead of the Butyral resin of Embodiment 41 to make coated wires for current collectorelectrodes and samples.

The following describes a method of making paste No. 5 for forming a singleliquid typed heat-hardening conductive bonding material constituting a coated layer of the coated wires for current collector electrodes.

Mixed solvent containing 17.0 g of butyl carbitol acetate and 1 1 g of methyl ethyl ketone were taken into a shaker for dispersion as solvent.

S* Urethane resin 5120 manufactured by Nippon Polyurethane, Ltd. used as a chief 15 agent of binder was added by 8.9 g to the solvent in the shaker, then it was stirred with a ball mill until it was sufficiently dissolved.

i As a curing agent, 1.4 g of blocked isocyanate 2515 manufactured by Nippon Polyurethane, Ltd. and 15 g of glass beads for dispersion were added to said solvent.

As conductive grains, 5.3 g of Conductex 975 beads manufactured by Colombian Carbon, Ltd. were added to said solvent and it was placed statically until the conductive grains were settled out sufficiently in said solvent.

25 Dispersion was made for the shaker containing the above materials for 12 hours by using a paint shaker.

[I:\DayLib\LIBEI02746a.docjs 175 Afterwards, glass beads for dispersion were removed from the paste No. The paste No. 5 was cured under the standard curing conditions on said curing agent, 180 °C of the temperature and 30 min. of the time and its volume resistivity was measured. As a result of the measurement, 5.1 "cm was obtained, by which it could be confirmed that the resistivity was sufficiently low.

The following describes conditions on forming said 10 paste No. 5 as the first coat layer 202 by using a wire coater 300.

The wire rolling speed is 8.9 mm/s, the curing time is 60 sec., the temperature in the drying oven is 280 and a bore diameter of the die used for enamel 15 coating is 180 pm. The thickness of the first coat layer 202 was 11 pm at an average and a deflection of the thickness of the coat was within a range of ±1 pm as a result of the coating in 100 m length.

In addition,_the following describes conditions on forming conductive bonding material made of said paste No. 5 as the second coat layer 203 by using the wire coater 300.

The wire rolling speed is 8.9 mm/s, the drying time is 60 sec., the temperature in the drying oven is 120 and a bore diameter of the die used for enamel coating is 200 pm. The conditions were obtained through an experiment for finding a status in which the 176temperature was lower than the dissociation level of blocked isocyanate without any tack of the paste No. applied to said wire. The conductive bonding material made of the paste No. 5 applied to said wire existed in a thermoplastic status with the solvent volatilized.

The thickness of the coat layer 203 is 8 pm at an average and a deflection of the thickness of the coat was within a range of ±1.5 pm as a result of the "'coating in 100 m length.

S1 10 Next, ten photovoltaic element modules were o fabricated in the same manner as for Embodiments 41 and 42.

As a result of measuring initial characteristics of the samples attained in this embodiment in the same manner as for Embodiment 1, transformation efficiency r was 7.8 at an average and the series resistance was 25 Qcm 2 Subsequently, was performed the same temperature and humidity cycle test as for Embodiment 41, and deterioration rate 1.5 was obtained at an average in comparison with the initial transformation efficiency without any significant deterioration.

As a result of this embodiment, it has been understood that the photovoltaic element of the present invention has favorable characteristics and secures higher reliability.

(Embodiment 44) 177- This embodiment differs from Embodiment 41 in that titanium oxide is used for a filler of the conductive bonding material used for the first coat layer 202 instead of the Conductex 975 beads of Embodiment 41 to make coated wire for current collector electrodes and samples. The second coat layer 203 was formed on the same conditions by using conductive bonding material made of the paste No. 4 same as for Embodiment 41.

The following describes a method of preparing paste No. 6 for forming the conductive bonding material constituting the coat layer of the coated wire for current 0o collector electrodes.

00 0 Mixed solvent containing 17.4 g of butyl carbitol acetate and 11.6 g of methyl ethyl ketone were taken into a shaker for dispersion as solvent.

0 is Butyral resin BL-S manufactured by Sekisui Chemical Co., Ltd. used as chief agent of binder was added by 8.9 g to the solvent in the shaker and it was stirred with a ball mill until it is fully dissolved.

*S As a curing agent, 1.4 g of blocked isocyanate B-815N manufactured by Takeda Chemical Industries, Ltd. and 15 g of glass beads for dispersion were added to said solvent.

As conductive grains, 5.3 g of titanium oxide powder FT-1000 manufactured by *0 Ishihara Sangyo, Ltd. was added to said solvent and it was placed statically until the 25 conductive grains were settled out sufficiently in said solvent.

[i:\DayLib\LBE]02746a.doc:jls 178- Dispersion was made for the shaker containing the above materials for 10 hours by using a paint shaker manufactured by Toyo Seiki Seisakujyo, Ltd.

Afterwards, glass beads for dispersion were removed from the paste No. 6. The paste No. 6 was cured under the standard curing conditions on said curing agent, 160 0 C of the temperature and 30 min. of the time and its volume resistivity was measured. As a result of the measurement, 8 Qcm was obtained, by which it could be confirmed that the resistivity was sufficiently low.

Subsequently, coated wire for current collector electrodes were made by forming the first coat layer 202 with conductive bonding material made of the past No. 6 on the same conditions as for Embodiment 41.

15 Next, ten photovoltaic element modules were fabricated in the same manner as for Embodiment 41.

As a result of measuring initial characteristics of the samples obtained in this embodiment in the same manner as for Embodiment 41, the transformation efficiency was 7.7 and the series resistance was 27 Qcm 2 Subsequently, was performed the same temperature and humidity cycle test as for Embodiment 41, and deterioration rate 3 was obtained at an average in comparison with the initial transformation efficiency without any significant deterioration.

S jI:\DayLib\LIBE]02746a.docjIs 179 As a result of this embodiment, it has been understood that the photovoltaic element of the present invention has favorable characteristics and secures higher reliability.

(Embodiment In this embodiment, it was examined what effects could be obtained with changing the volume resistivity of the conductive bonding material by mixing pigment in a binder of the conductive bonding material, phenoxy r 9 resin, at a variety of the amount ratio. As said pigment amount ratio, six types of percentages, 20 wt%, 25 wt%, 30 wt%, 35 wt%, 40 wt%, and 45 wt% were used to (99 make paste Nos. 7-1 to 7-6 for forming heat-hardening rI. conductive bonding material.

15 The following describes a method of preparing (r paste Nos. 7-1 to 7-6.

As solvent, cyclohexanone was taken into a shaker o* for dispersion.

Phenoxy resin-PKHH manufactured by Union Carbide, Ltd. used as a chief agent of binder was added to the solvent in the shaker, then it was stirred with a ball mill until it was fully dissolved.

As a dispersion agent, butyral resin BL-S manufactured by Sekisui Chemical Co. Ltd. was added, and it was stirred with a ball mill.

As a curing agent, blocked isocyanate B-815N manufactured by Takeda Chemical Industries, Ltd. and 180 glass beads for dispersion were added to said solvent.

As conductive grains, Conductex 975 beads manufactured by Colombian Carbon, Ltd. were added to said solvent, and it was placed statically until the filler was settled out sufficiently in said solvent.

Dispersion was made for the shaker containing the above materials for 10 hours by using a paint shaker.

Afterwards, glass beads for dispersion were removed from the paste Nos. 7-1 to 7-6. The paste Nos. 7-1 to 7-6 was cured under the standard curing conditions on said curing agent, 160 oC of the temperature and min. of the time and its volume resistivity was measured. As a result of the measurement, the values in Table 17 were obtained.

[Table 17] Pig- Volume Initial ment resis- trans- Material (g) ratio tivity format- (Q cm) tion effici- Carbon Phenoxy Curing Sol- Bead ency resin agent vent 892.10 4.00 3.00 10.80 1.20 17.40 15.00 10.68 7.52 3.75 10.13 1.13 17.40 15.00 2.19 7.60 4.50 9.45 1.05 17.40 15.00 0.63 7.70 5.25 8.78 0.98 17.40 15.00 0.28 7.85 6.00 8.10 0.90 17.40 15.00 0.36 7.81 6.75 7.43 0.83 17.40 15.00 181 The following describes conditions on forming conductive bonding material with said paste No. 7-1 to 7-6 as the first coat layer 202 by using the wire coater 300.

The wire rolling speed is 8.9 mm/s, the curing time is 60 sec., the temperature in the drying oven is 280 0 C, and a bore diameter of the die used for enamel coating is 180 p.m. The thickness of the first coat layer 302 was 11 pm at an average and a deflection of the thickness of the coat was within a range of 1 pm as a result of the coating in 100 m length.

In addition, coated wire for current collector electrodes were fabricated with the •conductive bonding material made of said paste No. 4 used as the second coat layer 203 I* by using the wire coater 300.

•00000 15 Subsequently, five photovoltaic element modules were fabricated in the same manner as for Embodiment 41, each.

Transformation efficiency of the samples was measured in the same manner as 00 for Embodiment 41 and averaged, then the values in Fig. 12 were attained.

As a result of this embodiment, it has been understood that the photovoltaic element of the present disclosure has favourable initial characteristics of the conductive bonding material having volume resistivity 0.1 to 100 Qcm.

*0*000 .0 25 (Embodiment 46) [I:\DayLib\LIB E]02746a.doc:j Is 182- In this embodiment, it was examined what effect of an ion barrier could be obtained by changing porosity of the conductive bonding material. To confirm the-ion barrier effect, triple-layered coated wire for current collector electrodes and photovoltaic S element modules were fabricated in the following procedure by using conductive bonding material LS-708 containing silver filler manufactured by Asahi Kagaku, Ltd. as a first coat layer.

Metal wire used for this embodiment is copper wire having a 100 Pm diameter.

10o The wire rolling speed is 8.9 mm/s, the drying time is 60 sec., the temperature in the drying oven is 250°C, and a bore diameter of the die used for enamel coatinig is 180 Pm.

The thickness of the first coat layer 202 is 8 pm at an average and a deflection of the 00 thickness of the coat was within a range of ±1.5 pm as a result of the coating in 100 m length.

15 0 The second coat layer 203 was formed on the same conditions by using conductive bonding material made of the paste Nos. 7-1 to 7-6 which was the same as for Embodiment 45. As a result of measuring porosity of the conductive bonding material oi made of the paste Nos. 7-1 to 7-6 by using an AUTO-PORE9200 manufactured by Micrometrics, Ltd., the values in Table 18 were obtained.

The third coat layer 204 was formed on the same o [I:\DayLib\LBE02746a.docjs 183 conditions by using conductive bonding material made of the same paste No. 4 as for Embodiment 41, and triplelayered current collector electrodes 1004 were made.

Subsequently, in the same manner as for Embodiment 41, said current collector electrodes 1004 were contact-bonded with heating on the cell surface of the substrate 1001. Then, encapsulation was performed in the same manner as for Embodiment 41 and initial characteristics were measured and averaged, which 00 S4 10 caused the result of values in Table 2.

S "0 Next, in the same manner as for Embodiment 41, a unique test was performed for 100 hours by putting the samples into the constant temperature and humidity bath whose inside temperature and humidity are controllable 15 to keep its temperature at +85 °C and relative humidity at 85 and by applying 1 V of forward bias voltage.

As a result of the test, the values in Table 18 were obtained as leakage current and shunt resistance after the lapse of 100 hours.

184 0 *0*0

S

*6 @6 @6 0 SS 6 0 06

S

[Table 18] Pig- Volume Porosity Leakage Shunt ment resis- (ml/g) current resistance ratio tivity (mA) (kQ cm 2 cm) Initia- After Initia- After lly test lly test 892.10 4.00 5.0 5.0 100.0 120.0 10.68 7.52 10.0 11.0 83.0 90.0 30 2.19 7.60 11.0 10.0 98.0 101.0 35 0.63 7.70 9.0 9.0 90.0 115.0 40 0.28 7.85 10.0 800.0 100.0 45 0.36 7.81 11.0 810.0 80.0 As for samples having 0.03 ml/g or greater porosity, leakage current 800 mA was obtained after the lapse of 100 hours and its level has gradually increased immediately after starting the test. It has turned out that a shunt has occurred because of 5 kQcm 2 or less shunt resistance. It can be considered that a short circuit has occurred due to migration since silver in the conductive bonding material used for the first coat layer was ionized due to the forward bias application under the conditions of higher temperature and higher humidity, therefore, it was found that the ion barrier effect of the second coat layer has been decreased.

As a result of this embodiment, it was determined that the photovoltaic element of the present disclosure 185 secures a favourable ion barrier effect within a range of 0.02 ml/g or less porosity of the conductive bonding material.

(Embodiment 47) In this embodiment, it was examined what coated wire for current collector electrodes should be, having a coat layer made of conductive bonding material containing a coupling agent.

As shown in Fig. 2A, coated wire for current collector electrodes 200 of the invention were formed as described below. As for metal wire 201, was used copper wire 0 having 100 Vm diameter cladded with silver on its surface. In this embodiment, doublelayered coating as shown in Fig. 2A was applied.

The following describes a method of preparing paste No. 8 for forming conductive bonding material constituting a coat layer 202 for coating the metal wire 201 directly.

As solvent, methyl carbitol was taken into a shaker for dispersion.

S

Urethane resin (made by Nippon Polyurethane Co, Ltd.) used as a chief agent and Butyral resin (made by Sekisui Chemical Co, Ltd.) for enhancement of dispersion were added to the solvent, and it was stirred enough with a ball mill.

Blocked isocyanate (made by Takeda Chemical Industries, Ltd.) used as a curing agent and [j:\DayLib\LIBE]02746a.doc:jls 186 y-mercaptopropyltrimethoxysilane (made by Toray Silicon, Ltd. used as a silane coupling agent were added to said solvent.

Carbon black (made by Colombian Carbon, Ltd.) having 0.05 pm of an average primary grain diameter was added to said solvent as conductive grains. In this composition, it has 67 wt% of resin and 33 wt% of conductive grains in weight ratio.

Dispersion was made for the shaker containing the above materials for 10 hours by using a paint shaker made by Toyo Seiki Seisakujyo, Ltd..

Glass beads for dispersion were removed from the paste No. 8. As a result of measuring an average grain diameter of the paste No. 8 in a laser diffraction 15 method, approx. 0.8 pm was obtained, which proves favorable dispersion. The same result was obtained when a beads mill was used instead of the paint shaker.

To check characteristics of conductivity of said paste No. 8, it was cured under the standard curing conditions on said curing agent, 160 °C of the temperature and 30 min. of the time and its volume resistivity was measured. As a result of the measurement, 0.5 Qcm of the volume resistivity was obtained and it was confirmed that the resistivity is sufficiently low.

The following describes a method of preparing paste No. 9 for forming conductive bonding material 187 constituting the coat layer 203 being in contact with a substrate of the photovoltaic element.

As solvent, cyclohexanone was taken into a shaker.

Were added urethane resin (made by Nippon Polyurethane, Ltd.) used as a chief agent and Phenoxy resin (made by Tomoe Kogyo, Ltd.) for removing the tack effect at rolling the coated wire on a bobbin to the solvent, and it was stirred enough with a ball mill.

Then, blocked isocyanate (made by Takeda Chemical 10 Industries, Ltd.) used as a curing agent and y-mercaptopropyltrimetoxysilane (made by Toray Silicon, Ltd.) used as a silane coupling agent were added to said solvent.

Carbon black (made by Colombian Carbon, Ltd.) 15 having 0.05 pm of an average primary grain diameter was added to said solvent as conductive grains. In this composition, it has 65 wt% of resin and 35 wt% of conductive grains in weight ratio.

(11) The above materials were dispersed in the same manner as for the paste No. 8 to make the paste No. 9.

The paste has approx. 1.0 pm of an average grain diameter.

(12) To check characteristics of conductivity of said paste No. 9, it was cured under the standard curing conditions on said curing agent, 160 °C of the temperature and 30 min. of the time and its volume resistivity was measured. As a result of the 188 measurement, 0.4 Qcm of the volume resistivity was obtained and it was confirmed that the resistivity is sufficiently low.

The following describes a method of forming the coat layer 202 made of the paste No. 8 and the coat layer 203 made of the paste No. 9 by using the wire coater 300 in Fig. 3.

First of all, a bobbin having a metal wire around its delivery reel was set, and said metal wire was 0 extended in the direction of a bobbin for rolling.

Then, said paste No. 8 was injected into the coater.

The coating was repeated five times under the conditions of 40 m/min. of the coating speed, 2 sec..

of the detention time, and 350 'C of the temperature in e 15 the drying oven. Dices for enamel coating each having 110 pm to 200 pm diameter were used sequentially.

Under these conditions, the paste No. 8 was cured o o enough to have favorable adhesion and solvent resistance. The thickness of the coat layer 202 made of the paste No. 8 is 5 pm at an average and a deflection of the thickness of the coat was within a range of ±0.5 pm as a result of the coating in 100 m length.

Subsequently, the paste No. 9 was applied. The coating was repeated five times under the conditions of m/min. of the wire rolling speed, 2 sec.. of the drying time, and 120 'C of the temperature in a drying 189 oven 306. Dices for enamel coating each having a 150 pm to 200 pm bore diameter were used. Although the paste No. 9 applied to said wire existed in -an uncured state with the solvent volatilized, any tack properties were not observed. The thickness of the coat layer 203 made of the paste No. 9 is 20 pm at an average and a deflection of the thickness of the coat was within a range of ±1.0 pm as a result of the coating in 100 m length.

1 0 The electrodes made in the above procedures were examined with adhesion tests for two classes of adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8 and adhesion between a substrate of the photovoltaic element and a substrate o 15 of a metal tab and the coat layer 203 made of the paste No. 9.

First of all, to examine the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8, the coat layer 202 and the coat layer 203 were set on the metal wire 201 as electrodes 200 to make sample 1 which was cured in a drying oven (not shown) under the conditions of the 160 °C temperature and the min. time. As a result of stretching the electrode 200 rapidly on the basis of an adhesion test of JIS3003 and checking the adhesion with observing broken section, favorable adhesion was confirmed without any abnormal cracks nor peeling.

190 Next, to check the adhesion between the substrate of the photovoltaic element and the substrate of the metal tab and the coat layer 203 made of the paste No.

9, sample 2 was made by contact-bonding the electrodes 200 with heating on an amorphous solar battery substrate with ITO cladded as a transparent conductive coating and a copper tab substrate with silver cladded on its surface. As a result of stretching the 0 e 0 electrodes 200 perpendicularly to each substrate S" 10 direction on the basis of the adhesion test of JIS3003 and checking the adhesion with measuring its tension, 6 favorable adhesion was confirmed with 0.15 kgfN or greater tension.

In addition, to check reliability of said 15 electrodes 200, said sample 1 and sample 2 were left in an environmental tester whose temperature was 85 °C and S relative humidity was 85 for 1,000 hours (hightemperature and high-humidity test). As a result of the same adhesion-test after the high-temperature and 20 high-humidity test, any changes did not occur in their characteristics.

The above description proves that the electrodes according to this disclosure have uniform width of lines and secures superior adhesive properties. In addition, they endure a hostile environment such as hightemperature and high-humidity for a long time without any cracks nor peeling and it is confirmed that they 191 also secures higher reliability.

(Comparison This example differs from Embodiment 47 in that a coupling agent is not mixed at compounding of paste.

Others are the same as for Embodiment 47 in forming electrodes.

As a result of checking adhesion of the created electrodes in the same manner as for Embodiment 47, o •some cracks were partially observed as for adhesion 1: 0 between the metal wire 201 and the coat layer 202 made .n of the paste No. 8. Adhesion between the substrate of the photovoltaic element and the coat layer 203 made of the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9 was o oo relatively low to 0.09 kgfN and 0.03 kgfN, respectively.

Furthermore, an adhesion test was performed after a high-temperature and high-humidity test in the same manner as for Embodiment 47, and cracks and a lot of peeling were observed as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8. Additionally, the adhesion between the substrate of the photovoltaic element and the coat layer 203 made of the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9 was decreased to 0.04 kgfN and almost zero, respectively.

192 (Embodiment 48) This embodiment differs from Embodiment 47 in that a titanate-series coupling agent, isopropyl tri-isostearoyl titanate (made by Ajinomoto Co., Inc.) is used as a coupling agent for compounding of the paste No. 8. Others are the same as for Embodiment 47 in forming electrodes.

As a result of performing adhesion tests in the same manner as for Embodiment 47, favorable adhesion 10 could be obtained without any abnormal cracks nor peeling as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8. In addition, as for the adhesion between the substrate of the photovoltaic element and the coat layer 203 made of 15 the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9, favorable adhesion was confirmed; 0.15 kgfN and 0.14 kgfN, respectively.

Additionally- adhesion tests were performed after a high-temperature and high-humidity test in the same manner as for Embodiment 47, and any changes did not occur in their characteristics.

(Embodiment 49) This embodiment differs from Embodiment 47 in that an aluminum-series coupling agent, acetoalkoxy aluminum di-isopropylate (made by Ajinomoto Co., Inc.) is used as a coupling agent for compounding of the paste No. 8.

193 Others are the same as for Embodiment 47 in forming electrodes.

As a result of performing adhesion tests in the same manner as for Embodiment 47, favorable adhesion could be obtained without any abnormal cracks nor peeling as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8. In S: addition, as for the adhesion between the substrate of the photovoltaic element and the coat layer 203 made of 10 the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9, favorable adhesion was confirmed; 0.15 kgfN and 0.14 -kgfN, respectively.

Additionally, adhesion tests were performed after 15 a high-temperature and high-humidity test in the same manner as for Embodiment 47, and any changes did not occur in their characteristics.

(Embodiment This embodiment differs from Embodiment 47 in that epoxy resin (made by Yuka Shell Epoxy, Ltd) is used as a chief agent of polymer resin for compounding of the paste No. 8, and a silane agent, y-glycidoxypropyltrimethoxysilane (made by Toray Silicon, Ltd.) is used as a coupling agent. Others are the same as for Embodiment 47 in forming electrodes.

As a result of performing adhesion tests in the same manner as for Embodiment 47, favorable adhesion 194 could be obtained without any abnormal cracks nor peeling as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No.- 8. In addition, as for the adhesion between the substrate of the photovoltaic element and the coat layer 203 made of the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9, "favorable adhesion was confirmed; 0.15 kgfN in both.

Additionally, adhesion tests were performed after 10 a high-temperature and high-humidity test in the same manner as for Embodiment 47, and any changes did not occur in their characteristics.

(Embodiment 51) This embodiment differs from Embodiment 47 in that .000, 15 phenol resin (made by Dainippon Ink Chemicals, Inc.) is used as a chief agent of polymer resin for compounding of the paste No. 8, and a silane agent, y-(2-aminoethyl) aminopropyltrimetoxysilane (made by Toray Silicone, Ltd.) is used as a coupling agent.

Others are the same as for Embodiment 47 in forming electrodes.

As a result of performing adhesion tests in the same manner as for Embodiment 47, favorable adhesion could be obtained without any abnormal cracks nor peeling as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8. In addition, as for the adhesion between the substrate of 195 the photovoltaic element and the coat layer 203 made of the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste-No. 9, favorable adhesion was confirmed; 0.15 kgfN in both.

Additionally, adhesion tests were performed after a high-temperature and high-humidity test in the same manner as for Embodiment 47, and any changes did not occur in their characteristics.

S S (Embodiment 52) 10 This embodiment differs from Embodiment 47 in that polyimide (made by Nippon Polyimide, Ltd.) is used as a chief agent of polymer resin for compounding of the paste No. 8, and a silane agent, y-anilinopropyltrimethoxysilane (made by Toray 15 Silicone, Ltd.) is used as a coupling agent. Others are the same as for Embodiment 47 in forming electrodes.

As a result of performing adhesion tests in the same manner as for Embodiment 47, favorable adhesion could be obtained without any abnormal cracks nor peeling as for the adhesion between the metal wire 201 and the coat layer 202 made of the paste No. 8. In addition, as for the adhesion between the substrate of the photovoltaic element and the coat layer 203 made of the paste No. 9 and between the substrate of the metal tab and the coat layer 203 made of the paste No. 9, favorable adhesion was confirmed; 0.15 kgfN in both.

196 Additionally, adhesion tests were performed after a high-temperature and high-humidity test in the same manner as for Embodiment 47, and any changes did not occur in their characteristics.

(Embodiment 53) In this embodiment, an amorphous solar battery 400 was fabricated in a pin-junction-typed single structure with grids whose grid length was 30 cm in a layer structure shown in Fig. 4A.

10 The following describes a method of the fabrication according to the fabrication procedure.

After putting sufficiently degreased and cleaned substrate 401 made by SUS430BA into a DC sputtering device (not shown) and depositing Ag up to 400 nm, a 15 lower electrode 402 was formed by depositing ZnO up to 400 nm.

After taking out the substrate was taken out, it was put into an RF plasma CVD film generator (not shown), then deposition is made for an amorphous silicone semiconductor layer in an order of n layer 403, i-layer 404, and p-layer 405.

It was put into a metallizing apparatus of a resistance heating system (not shown) and an ITO film was generated as a transparent conducting film 406 having also a function of anti-reflection effect (film generation temperature: 450 film thickness: 70 nm).

By using the same paste No. 8 and No. 9 as for 197- Embodiment 47, electrodes 200 having a coat layer made of conductive bonding material was made.

The electrodes 200 were arranged on the substrate 401 having a copper-foiled tab 501 cladded with silver on its surface by using a wiring machine (not shown), with providing an adhesive portion which was 5 mm wide outside an effective area of the solar battery, then they were temporarily fixed with adhesive at their both ends.

10 By using a heat contact-bonding machine (not shown), they were fixed on the substrate through the paste No. 9 applied to the wire to form a grid electrode 307.

As shown in Fig. 13, an anode drain section 1302 and a cathode drain section 1303 were connected with soldering to generate a single cell 30 cm square.

Encapsulation was made for an amorphous solar battery in which the above electrodes were formed as described below. -The amorphous solar battery 1300 was cladded with EVA on its both sides, then further with fluoroplastic film ETFE (ethylene tetrafluoroethylene) (Du Pont product name, "Tefzel"), and it was put into a vacuum laminator for vacuum lamination with increasing the temperature and keeping 150 °C for 45 min.

Generation of the samples of this embodiment was completed in the above to process.

The initial characteristics for the generated 198 samples were measured as described below. By using a simulated sun light source (hereinafter "simulator") having 100 mW/cm 2 quantity of light in the AM1.5 global sun light spectrum, characteristics of the solar battery were examined with measurement.

Characteristics of measured transformation efficiency 6.7 shunt resistance (dark state) 50 kQcm 2 and series resistance 9.5 Qcm 2 were favorable.

A confidence test for these samples was performed 10 on the basis of the temperature and relative humidity oooeo cycle test A-2 defined in an environmental test method and an endurance test method of crystal-system solar *"battery modules of Japan Industrial Standard C8917.

First of all, a cycle test was repeated 20 times by 15 putting the samples into a constant temperature and eoeu humidity bath whose inside humidity was controllable and changing the temperature from -40 'C to +85 °C (relative humidity: 85 Afterwards, when characteristics of the solar battery were examined every after the completion of ten times repetition of the test by using the simulator in the same manner as for the measurement of the initial characteristics, a decrease of 3.2 was observed in comparison with the initial transformation efficiency and a decrease of for the shunt resistance (dark state) after the completion of 20 times repetition of the test, therefore, any significant deterioration was not found 199 in both. In addition, the series resistance was measured and an increase of only approx. 2.4 was observed in the samples of this embodiment as shown in Fig. 14, and a phenomenon such as peeling in the electrode section was not found.

As a result of this embodiment, it has been understood that the solar battery according to the invention has favorable characteristics and secures higher reliability.

(Comparison 6) ooooo In this example, the electrodes were formed in the same manner as for Embodiment 1 except that a coupling agent was not mixed at compounding of paste. Then, by using these electrodes, an amorphous solar battery was 15 made in the same manner as for Embodiment 53.

oo• Additionally, samples were made with performing encapsulation of said amorphous solar battery in the same manner as for Embodiment 53.

As a result of measuring the initial characteristics of the samples in the same manner as for Embodiment 53, the initial transformation efficiency was 5.8 and the series resistance was 15.5 Ccm 2 therefore, the series resistance was higher in comparison with Embodiment 53.

Subsequently, a confidence test was performed for these samples in the same manner as for Embodiment 53.

As a result of measuring the transformation efficiency 200 of the samples after completion of a temperature and humidity cycle test, a decrease of 17% was observed in comparison with the initial value after 20 times repetition of the test, which indicated a significant deterioration.

When the series resistance of these samples was measured, a change on standing was observed as shown in Fig. 14 and it increased up to approx. twice as high as the initial state after 20 times repetition of the 10 test. Accordingly, it was found that adhesion between co go the electrodes was decreased.

(Embodiment 54) This embodiment differs from Embodiment 53 in that oo a solar battery has a structure shown in Fig. 4C as a :i 15 triple-typed amorphous solar battery 400 and that a •one o microwave CVD method is used for generating a semiconductor layer.

The following describes a method of the generation according to the generation procedure.

A lower electrode 402 comprising Ag and ZnO was formed on an SUS substrate 401.

It was put into a microwave plasma CVD film generator (not shown), and a bottom layer was formed in an order of n layer 403, i-layer 404, and p-layer 405.

Then, in the same manner, a semiconductor layer was generated by forming a middle layer in an order of n layer 413, i-layer 414, and p-layer 415 and a top layer 201 in an order of n layer 423, i-layer 424, and p-layer 425 sequentially.

An ITO film was generated as a transparent conducting film 406 having also a function of antireflection effect (film generation temperature: 450 'C, film thickness: 70 nm) in the same manner as for Embodiment 53.

By using the same paste No. 8 and No. 9 as for Embodiment 47, electrodes 200 having a coat layer made of conductive bonding material was generated.

e The electrodes 200 were arranged on the substrate 401 having a copper-foiled tab 501 cladded with silver ."on its surface by using a wiring machine (not shown), with providing an adhesive portion which was 5 mm wide 15 outside an effective area of the solar battery, then they were temporarily fixed with adhesive at their both ends.

By using a heat contact-bonding machine (not shown), they were fixed on the substrate through the paste No. 9 applied to the wire to form a grid electrode 307.

Encapsulation was made for an amorphous solar battery in which the above electrodes were formed in the same manner as for Embodiment 53.

202 Generation of the samples of this embodiment was completed in the above to process.

The initial characteristics for the generated samples were measured in the same manner as for Embodiment 53. Characteristics of measured initial transformation efficiency 8.3 shunt resistance (dark state) 42 kQcm 2 and series resistance 33.0 !cm 2 were favorable.

.In addition, a confidence test for these samples 0 was performed in the same manner as for Embodiment 53.

As a result, an increase of 2.7 was observed as for the series resistance in comparison with the initial **value after 20 times repetition of the test and a e decrease of only 1.8 as for the transformation 15 efficiency in comparison with the initial value, therefore, any significant deterioration was not found in both.

(Embodiment In this embodiment, to check a long-term preservation stability of electrodes, the electrodes in Embodiment 47 were rolled in a bobbin-like configuration and they had been kept in an environment at a room temperature for 100 days. Afterwards, 203 adhesion of the electrodes 200 was checked in the same manner as for Embodiment 47, and favorable adhesive characteristics were confirmed like Embodiment 47.

[Advantage of the Invention] As described in detail above, according to this disclosure, coated wires for reliable current electrodes having excellent adhesion and long-term preservation characteristics are obtained.

S In addition, by using the coated wires for current electrodes, photovoltaic elements having higher initial characteristics and superior long-term reliability are *i obtained.

*o o 15 Furthermore, since a yield on production is improved, a method of generating photovoltaic elements having favorable reliability characteristics is obtained.

*f ooft *oo [R:\LIBE]02746 doc.avc

Claims

1. A coated wire with a collector electrode, said coated wire comprising: a metal wire coated with a coating layer of a conductive adhesive and formed to adhere to a photovoltaic element through said coating layer, wherein the coating layer is for preventing a metal ion of said metal wire from migrating into a light incident surface of a photoelectric conversion layer of said photovoltaic element.

2. A coated wire as claimed in claim 1, wherein said coating layer has a performance for preventing the metal ion from the migration even in case of applying to said metal wire a voltage higher than a photogenerated voltage of said photovoltaic element.

3. A coated wire as claimed in claim 1 or 2, wherein said conductive adhesive comprises conductive particle and high polymer resin.

4. A coated wire as claimed in claim 1 or 2, wherein said conductive adhesive comprises coupling agent, conductive particle and high polymer resin.

5. A coated wire as claimed in claim 4, wherein said coupling agent is at least one kind selected from silane based coupling agent, titanate based coupling agent and aluminum based coupling agent.

6. A coated wire as claimed in any one of claims 1-5, wherein said conductive adhesive has a porosity 0.04ml/g or more smaller with regard to a void of radius 1 ltm or more smaller.

7. A coated wire as claimed in any one of claims 1-6, wherein number average molecular weight of said high polymer resin is 500-50000.

8. A coated wire as claimed in any one of claims 1-7, wherein said high polymer resin has a gel fraction of 20-100%. [R:ALBE]02746.doc:avc -205

9. A coated wire as claimed in claim 7 or 8, wherein said coating layer comprises at least two or more layers, and among them, at least the coating layers except for mostly outer coating layer comprises the conductive adhesive made of the high polymer resin as claimed in claim 7 or 8. A coated wire as claimed in claim 9, wherein said coating layer comprises at least two or more layers, and at least mostly outer coating layer is formed from conductive adhesive formed from thermally hardening high polymer resin not hardened.

11. A coated wire as claimed in claim 10, wherein said conductive adhesive has a resistivity of 0.1-100 cm.

12. A coated wire as claimed in any one of claims 1-11, wherein said high 15 polymer resin is at least one kind selected from urethane, phenoxy, epoxy, butyral, phenol, polyimide, polyamide and polyamideimide.

13. A coated wire as claimed in any one of claims 1-12, wherein said conductive adhesive contains as a hardening agent a block isocyanate.

14. A coated wire as claimed in any one of claims 1-13, wherein said conductive adhesive has a glass transition point not lower than 1000 C.

15. A coated wire as claimed in any one of claims 1-14, wherein said 25 conductive particle has firstly particle of an average radius 0.02tm-15tm.

16. A coated wire as claimed in any one of claims 1-15, wherein said conductive particle is at least one kind selected from graphite, carbon black, In 2 0 3 TiO 2 SnO 2 ITO, ZnO and those material doped with trivalent metal element.

17. A photovoltaic element comprising: a semiconductor layer comprising at least one pin junction or pn junction, and a collector electrode provided at a light incident side of said semiconductor layer, wherein said collector electrode is formed by a coated wire as claimed in any one of SRA claims 1-16. [R:\LIBE]02746.doc:avc -206-

18. A photovoltaic element as claimed in claim 17, further comprising a transparent electrode at the light incident side of said semiconductor layer, and a coated wire for the collector electrode as the collector electrode on said transparent electrode.

19. A photovoltaic element as claimed in claim 17, wherein said coated wire for the collector electrode is provided as the collector electrode so that, on the transparent electrode arranged on the semiconductor layer of the photovoltaic element, the conductive adhesive of the coated wire for the collector electrode as claimed in any one of claims 1-16 contacts. A photovoltaic element as claimed in claim 17 or 18, wherein said semiconductor layer comprises at least one kind selected from single crystalline silicon, polycrystalline silicon, thin film polycrystalline silicon, amorphous silicon, amorphous silicon germanium, and amorphous silicon carbon.

21. A photovoltaic element as claimed in any one of claims 17-20, wherein said semiconductor layer is a triple cell comprising stacked three cells comprising pin junction or pn junction.

22. A method for producing a photovoltaic element of a structure provided with a collector electrode at a light incident side, wherein a coated wire for a collector electrode as claimed in any one of claims 1-16 is bonded to a light incident surface of said photovoltaic element by heating, pressure or both of heating and pressure.

23. A method for producing a photovoltaic element as claimed in claim 22, wherein the heat applied to said coated wire for said collector electrode is not lower than a dissociation temperature of the block isocyanate.

24. A method for producing a photovoltaic element as claimed in claim 22 or 23, wherein said coated wire is heated, so that the not hardened thermally hardening high polymer resin forming said coating layer is heated to have gel fraction of 20-100%. [R:\LIBE]02746.doc:avc 4 I. -207- A coated wire substantially as described herein in relation to any one embodiment with reference to the drawings. a metal wire with a coating layer of a conductive adhesive bonded through said coating to a photovoltaic element, wherein said coating layer comprises at least two layers. DATED this Eighth Day of June, 2000 Canon Kabushiki Kaisha Patent Attorneys for the Applicant SPRUSON FERGUSON [R:\LIBE]02746.doc:avc