POLYIMIDE COMPOSITION AND METHOD FOR PROTECTING PHOTOREACTIVE CELLS

Abstract: Solar cells, particularly those positioned in space, require a coating to protect the solar cell against damage caused by solar radiation. The present invention provides such a protective coating which is a polyimide which has the required combination of properties of being colorless, transparent, relatively non-brittle, having a high degree of thermal stability and readily transmitting solar radiation without appreciable degradation. The coating (22) is heat resistant and does not degrade significantly when exposed to ultraviolet radiation, and is highly effective in repelling low energy proton particles. In a preferred embodiment, the protective polyimide coating is a polymer having the recurring structural unit (I).

Description: POLYIMIDE COMPOSITION AND METHOD FOR PROTECTING PHOTOREACTIVE CELLS BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to a polymeric coating for solar cells and to a polymer coated solar cell, and is particularly directed to polyimide coatings for solar cells and solar cells coated with such polyi ides and which coatings are colorless and transparent, relatively non-brittle, have good thermal properties, resistance to ultraviolet radiation degradation, effective in repelling low energy protons and also have other desir¬ able characteristics for use in outer space. 2. Description of the Prior Art Polymeric coatings for solar cells are required to provide a high degree of solar radiation protection. Conventional polyimides have the requisite thermal stability, but they are colored, and thus absorb in the visible portion of the solar spectrum which redJUces performance and generates heat which promotes degradation. Other polymers discolor excessively or lose structural integrity for various other reasons, such as instability to solar protons, electrons, or ultraviolet radiation. When these polymer coatings discolor, the portion of solar spectrum transmitted to the solar cells is reduced, thus effectively reducing the solar cell efficiency. JfcEAj OMPI In the prior art, coatings such as polyurethanes, epoxies, polyesters, polyimides, etc., were evaluated and found to have inadequate stability for various reasons. Perfluorinated aliphatic hydrocarbons, such as FEP Teflon (tetrafluoroethylene hexafluoropropylene copolymer) , had a better potential, but had inadequate stability. Further, it is necessary to employ an adhesive or a fusion process in order to apply the Teflon or other polymer coating to the solar cell itself. Usually such an adhesive is a silicone. However, after a period of time, the adhesive or fusion boundary fails and the Teflon becomes separated from the solar cell, thereby accelerating deterioration and failure of the cell. Because of the limitations of known polymers heretofore used or considered for solar cells, and particularly for solar cells positioned in outer space, it was necessary to employ a quartz cover over the solar cell itself, in order to protect the cell against low energy particles such as low energy proton bombardment. However, the quartz layer was usually quite heavy (relative to a polymeric coating) . This quartz layer thus increased the overall weight and made introduction of the solar cell into very large arrays much more difficult and costly. Some of the commonly used protective covers for solar cells are formed of fused silica. These fused silica layers usually require a multi-layer filter to effectively filter out all ultraviolet radiation-, as for example, that radiation less than 0.35 micrometer (vm) , to protect the adhesive, (e.g., a silicone adhesive) from darkening and losing transmission and hence power. Another protective cover commonly used is Ceria, namely a cerium oxide doped glass micro-sheet. This glass sheet has a natural cut-on frequency of about 0.35 μm and hence does not require a multi-layer filter for adhesive protection. The Ceria glass sheet does provide for radiation stability. In addition to the foregoing, a fused silica without a multi-layer filter has been used with the FEP Teflon as the adhesive. This combination is quite effective in view of the fact that glass processing is minimized. However, the overall covered solar cell is still too heavy for use as a space cell in extremely large solar cell arrays. The method of protecting solar cells which is currently used to a large degree involves the adhesive bonding of a thin ZnO/Ta2θs coated quartz coverslide onto the solar cells with a silicone adhesive. The multi-layer ZnO/Ta2θs coating on the quartz is a solar radiation cut-off coating which prevents damaging solar radiation (approximately less than 0.32 ) from penetrating through the quartz into the silicone adhesive. Although this means of protecting solar cells is effective, it is too expensive and impractical to apply to massive solar arrays, such as those which would be required for capturing solar radiation on a massive scale in space and transmitting it to earth. This technique is practical only for relatively "small" devices such as communication satellites where the added costs can be tolerated. It is not practical for large size applications, e.g., acre size applications. f Consequently, there still exists a need for a much more reliable, light weight protective coating for solar cells, and particularly for those solar cells which are to be exposed to outer space environments. The prior art cover materials or coating materials such as quartz and the other polymers, are of limited effectiveness. The polymer systems, particularly, suffer from the disadvantage in that they exhibit loss of transmission, cracking and loss of adhesion to the cell after exposure to solar ultraviolet radiation for any reasonable period of time. Further, adhesion is affected materially after subjection to the outer space environments. Consequently, the critical properties for solar cell coatings include the property of being resistant to ultraviolet radiation and maintaining optical clarity, even after a period of time. These coatings must also be resistant to degradation by low energy protons and exhibit good adhesion to the cell after some thermal cycling. Further, they must be formulated for ease of application to the solar cells without any damage to the cell itself. In addition, the coatings must be formulated to be more cost effective than the previously and presently used quartz and glass s stems. U.S. Patent No. 3,356,648 discloses linear polyimides derived from the hexafluoroisopropylidene bridged diamine, such as dianiline, and tetracarboxylic dianhydride. These polyimides are useful as shaped structures and for wrappings, packaging and the like. U.S. Patent No. 3,959,350 discloses linear polyimides similar to those of U.S. Patent No. 3,356,648, but which do not have hexafluoroisopropylidene groups bridging the amine moieties. These polyimides a e useful as molding compounds, and for preparing self-supporting film structures and composites. However, these " poly— imides are not colorless. The lack of transparency and the other physical characteristics, such as pro- cessability of these polyimides, render them ineffective as solar cell coatings. SUMMARY OF THE INVENTION According to the invention, solar cells are coated with a polymer in the form of a polyimide to form a protective coating thereon. The coating is a polyimide which has the following specific properties. The polyimide (1) is colorless, (2) is transparent to the solar radiation in the visible light spectrum, (3) is relatively non-brittle, (4) has a high degree of thermal stability, (5) readily transmits solar radiation without appreciable degradation, (6) is heat resistant, (7) does not degrade significantly when exposed to ultraviolet radiation, and (8) is highly effective in protecting against low energy particles, such as proton particles, by effectively absorbing such particles. In a more preferred embodiment, the coating is formed from a polyimide composition which has the recurring structural unit shown below: s # where R is: II III and n has a value range from 10 to about 2000. Pref¬ erably, n has a value from about 10 to about 1000. The polyimide which is most preferred according to the invention is the meta amino phenylene derivative of formula II above, and having the recurring structural unit: IV z and its precursor has the polyamic acid structure: V where n has the values noted above. It has been found that the above polyimide, particularly of structure IV above, when applied as a coating to a solar cell has excellent resistance to degradation from solar radiation and particularly radiation in the ultraviolet wave length range. The film also has remarkable proton absorption capa¬ bilities. It has been noted that no other polymer coatings evaluated to date provide the degree of solar radiation protection afforded by the polyimide coatings of the structure of formula I above, and especially of formula IV while providing the advantage of these coatings. ^ z. More particularly, the above polyimide cc&ting is highly suitable for solar cell coating application because of its unique combination of properties. This unique combination of properties includes their excellent thermal stability, which is at least equivalent to that of other aromatic polyimides, transparency in films, colorless nature, stability to ultraviolet radiation, and ability to protect against low energy proton and electron bombardment. This combination of properties is essential for a coating to be useful in the protection of solar cells. A particular advantage of the solar cell coatings of this invention is their capability for use without the quartz cover heretofore employed on solar cells and without the need for an adhesive layer susceptible to ultraviolet light degradation. This invention possesses many other advantages and has other purposes which may be made more clearly apparent from a consideration of the forms and compo¬ sitions in which it may be embodied. They will now be described in detail for the purposes of more fully setting forth the general principles of the invention, but it is to be understood tha.t such,detailed descrip¬ tion is not to be taken in a limiting sense. BRIEF DESCRIPTION OF THE DRAWING In the accompanying drawing, the Figure is a vertical section view of a solar cell having a coating in accordance with the present invention applied thereto. DETAILED DESCRIPTION OF THE INVENTION Referring now in more detail and by reference characters to the drawing, there is shown a solar cell having a polyimide coating as hereinafter described. The photocell itself generally comprises a base^of p- type semiconductor material which constitutes a p-layer 10 and which is doped on one surface with an n-type material forming an n-layer 12 having a p-n junction 14 therebetween. OMPI A p-layer electrode 16 is attached to the bottom side of the p-layer 10 for an electrical conductor to be connected thereto. An n-layer electrode 18 may be connected to the n-layer 12 to enable an electrical conductor to be connected thereto. The n-layer electrode usually includes a number of so-called relatively thin fingers extending throughout the surface area of the n- layer so as to avoid any substantial interference with visual light radiation impingement on the photocell. The photoreactive layers or so-called "photo¬ voltaic" layers including the n-layer 12 and p-layer 10 and junction 14 may adopt the form of a silicon material or it may be a III-V compound such as gallium arsenide, gallium arsenide-phosphide, etc. Other photo-voltaic materials well known in the art may be employed and may be properly doped. In many cases, an anti-reflective coating 20 may be employed and would be deposited directly on the active surface of the cell prior to application of the polyimide protective coating. A suitable anti-reflective coating is a combination of TiO x and AI2O3, Ta2θ5 or SiO x . Prior to the application of a polyimide coating 22 prepared in accordance with the present invention, a primer coating 24 may be applied to the upper surface of the n-layer 12 or to the anti-reflective coating 20, if employed. The primer coating 24 would generally increase the adhesion of the polyimide coating £0 the solar cell and particularly to the upper surface of the anti-reflective layer 20 thereof. A typical primer for this purpose is a silane adhesion promoter, such as aminopropyltrimethoxysilane. Other silane adhesion promoters are also known in the art and might also be used for this purpose. OMPI The polyimide of formula IV above is prepared by the reaction of substantially equal molar proportions of the two monomers 2,2-bis(3-aminophenyl)hexafluoro¬ propane and 4,4'-hexafluoroisopropylidene[bis(phthalic anhydride)], in a solvent for such monomers. The solvents which can be used include, for example, tetrahydrofuran, N-methyl pyrrolidinone, N-methylformamide, dimethylform- amide and N,N-dimethylacetamide and mixtures thereof. The resulting polyamic acid solution can be cast as a film and the film imidized to the polyimide structure IV above. Both the polyamic acid and the polyimide have an inherent viscosity of at least 0.1, usually 0.3-0.5. The inherent viscosity of the polyimide is measured at 30°C as a 0.5% solution in a suitable solvent, such as cold concentrated (96%) sulfuric acid, or methanesulfonic acid. As noted above, in preparing the coated solar cells according to the invention, a solution of the polyamic acid precursor of formula V above in a solvent, such as tetrahydrofuran, at a concentration of about 10 to about 30% of the polyamic acid, can be used as a varnish for application to the active surface of a solar cell. The varnish or solution of the polyamic acid precursor can be coated over the primer coating 24 of the solar cell in any suitable manner, for example, by dipping, electrocoating, spraying, electrostatic spraying and the like. Spraying is a convenient method ø,f application, as contrasted, for example, to the/use of Teflon applied as a solar coating according to the prior art, and which requires application of a film. A 15% solids content solution of the polymer in N-methylpyrroli- dinone or dimethylformamide has been found to be effec¬ tive. The solution is sprayed after applying the -gJRE OMPI primer (Union Carbide A1100, aminopropyltrimethoxy- silane) from a 5% solution in ethanol. The amount of the polyamic acid in the solvent will vary depending primarily on the type of sprayer or other coating means which is used. The solid content of the polyamic acid in the solvent solution can vary greatly and could be as high as 30% in tetrahydrofuran and in which solution dimethylformamide can be present in an amount of normally at least 60%. After application of the polyamic acid varnish to the solar cell, that is, over the primer, the solvent is essentially evaporated off and the a ic acid polymer is converted into the imidized or polyimide structure of formula IV by heating such amic acid polymer at about 250°C. Lower temperatures, such as at 120°C, can also be used to promote the imidization, but the reaction rate is slower and the elimination of solvent residues is slower. Preferred imidization temperatures range between about 160°C and 250°C. The polyimide coating may also be dried at 350°F (about 175°C) in a vacuum bag. Thinner coatings (about 0.1 mil or 2.54 x 10~ 6 m thick) can be dried and then cured for 1 to 2 hr. at 485°F (about 250°C) in a vacuum bag. However,- the preferred temperature for effecting imidization is that which provides the best solar cell performance, and this may vary depending upon the specific type of cell and the specific batch of amic acid polymer available. _• * The polyimide film 22 thus formed is generally a very thin layer, as is the silane primer film. The polyimide film itself is preferably about 0.2 to 0.5 mil (5.08 x 10 -6 to 1.27 x 10" 5 m) thick. However, the practical minimum thickness is about 0.1 mil (2.54 x 10~ 6 m). There is no absolute maximum thickness, except that the film should be as thin as possible and yet provide the desired characteristics to minimize weight of the solar cell. EXAMPLES The invention is further illustrated by, but not limited to, the following examples: Example I This example I discloses the preparation of the polyimide and its casting into a film. A 100 ml three-necked flask was fitted with a stirrer and gas inlet and outlet tubes. The flask was charged with a solution of 2,2-bis(3-aminophenyl)- hexafluoropropane. (1.6344 grams, 0.004890 mole) in 30 ml of purified N,N-dimethylacetamide. Under an argon atmosphere at room temperature and with good stirring, powdered solid 4,4'-hexafluoroisopropylidenebis- (phthalic anhydride) (2.1700 grams, 0.004890 mole) was added over a three minute period. The solution was stirred overnight under argon. The solution increased in viscosity during this time. A clear colorless film could be cast from the solution and after drying at 75°C in an air circulating oven, the film could be imidized by heating above 200°C to form a clear and colorless film after imidization. Example II A solution of varnish of about 15% of the polyamic acid precursor of formula V above in 25% tetrahydrofuran, and containing about 60% of dimethylformamide was pre- z. pared in a manner as essentially disclosed in Example I above. The varnish was applied by spraying over the silica covers of a K6 3/4 solar cell, where K6 3/4 is an arbitrary numerical designation for a shallow diffused 10 ohm-cm silicon solar cell with a back surface field and reflector. After application of the amic acid coating to the solar cell, the coating was heated at about 250°C for a period of about 60 minutes, causing substantially all of the solvent to evaporate off, and converting the polyamic acid to a colorless transparent film of the polyimide of structure IV above. A 0.5 mil (1.27 x 10~ 5 m) thick colorless transparent polyimide coating was thus formed on the solar cell. In a 1200 hour test of the 0.5 mil (1.27 x 10"" 5 m) polyimide coating of the type specified above, under a Xenon light source equivalent to 1.5 suns of UV exposure, the net loss in short circuit (Isc- 1 corresponding to UV transmittance loss, showed an estimated net UV loss (I sc ) of only 8.1%, and with a 0.2 mil (5.08 x 10 "6 m) polyimide coating, was only 8.4%. This loss was an order of magnitude less than that which has been observed with other polymeric coatings such as polyurethanes, epoxies or polyesters, indicating only very minor degradation of the polyimide coating due to UV exposure as compared to other polymeric coatings. Example III Thermal cycling of the polyimide coated solar cells [0.2 and 0.5 mil (5.08 x 10" 6 and 1.27 x 10" 5 m) coating] for Example II (room temperature to liquid nitrogen, 25 cycles) showed no loss of adhesion, via ; tape pull test, of the coating to the cell substrate. The tape pull test involves the application of ^an adhesive tape, such as a Scotch Brand number 600 tape or the equivalent, to the solar cell and particularly the n-layer electrode and the p-layer electrode surfaces. The tape is pulled away from these contacts or electrodes with a continuous pull. The pull is initiated at one end and progresses toward the other. The cell is then examined for conformance to a desired adhesion level. Exposure of the coated cells [0.2 mil (5.08 x 10~6m) and 0.5 mil (1.27 x 10- 5 m) coating] to simulated space radiation showed essentially no loss in short circuit current. Dosages of 1 x lθH protons/cm 2 (50 KeV) and 2 x lθH protons/cm 2 (50 KeV) gave identical results. Spectral response was measured before and after proton exposure. No significant changes were noted, thus indicating resistance of the polyimide solar cell coatings to proton radiation. Several additional tests were conducted with the standard 10 ohm-cm shallow diffused silicon solar cells designated as the K6 solar cells. These cells had a back surface field and a back surface reflector. In some cases, tests were conducted with solar cells having a textured front surface designated as the K-7 cells. Tests were generally conducted with thicknesses of the polyimide films of about 0.2 and 0.5 mil (5.08 x 10-6 aru j ι.27 x 10""5 m ) . Further, the thickness variation of the polyimide layer did not apparently have any significant influence on the amount of ultraviolet degradation. Consequently, relatively thin films can be employed. _ s From the foregoing, it is seen that the invention provides an improved polymer coated solar cell with a specific polyimide coating having the following advantages: a colorless polymeric coating is provided which readily transmits solar energy, does not degrade significantly when exposed to proton radiation, electron ( OMPI radiation and ultraviolet light; is transparent and heat resistant, and protects the solar cell from the damaging effects of solar protons, electrons, ultraviolet light and other forms of radiation, is a relatively non- brittle film forming coating, and has processing characteristics which permit it to be readily coated onto solar cells. The specific polyimide coatings of the present invention obviate the problems heretofore described. These coatings are very light in weight due to the fact that they can be applied in very thin coatings and nevertheless still provide the necessary protection. For example, a 0.2 mil (5.08 x 10" 6 m) coating has been found to be highly effective. Further, the low molecular weight of the polymers may provide for good adhesion to the solar cell itself. In addition, this also enables the adhesion to be maintained over a long lifetime. Indeed, exposure of the solar cells coated with the polyimide resin of the invention with a thickness of 0.2 mil (5.08 x 10" 6 m) to 0.5 mil (1.27 x 10""5 m ) an d subjected to simulated space radiation showed essentially no loss in short circuit current. Spectral response was also measured before and after exposure to low energy protons. Once again, no significant changes were noted and the polyimide coated solar cell permitted effective transmission ofi- solar radiation in the range of 0.32 urn to 0.96^μm. Thus, there has been described a novel polyimide composition and method for protecting photoreactive cells, such as solar cells, and which composition and method provides a coating which is relatively durable, tightly adherent and capable of withstanding ultraviolet radiation degradation and bombardment by low energy particles. This composition and method thereby fulfills all of the objects and advantages sought therefor. It should be understood that many changes, modifications, OMPI variations and other uses and applications will become apparent to those skilled in the art after considering this specification and the accompanying drawing. Therefore, any and all such changes, modifications, variations and other uses and applications which become apparent to those skilled in the art after considering this specification are deemed to be covered by the present invention. z. r MEL: blm [103-14]

Claims: CLAIMS What is Claimed is: 1. A substantially colorless and transparent protective polymeric coating for a solar cell, said coating transmitting solar radiation and having high degradation resistance to radiation in the ultraviolet sprectrum and including low energy particle resistance, comprising a polyimide having the recurring structural unit: where R is: OMP 2. The protective polymeric coating of Claim 1, comprising a polyimide having the recurring structural unit: and where n is a number ranging from 10 to about 1000. 3. The protective polymeric coating for a solar cell as defined in Claim 2, said polyimide being formed by heating a solution of the amic acid precursor having the recurring structural unit: and where n is a number ranging from 10 to aboyt 1000. 4. The protective polymeric coating of Claim 2. where said polyimide in solution and before coating has an inherent viscosity of at least 0.1 as measured at 30 β C on a 0.5% by weight basis when in a solvent therefor selected from the group consisting of sulfuric acid and methanesulfonic acid. OMP 5. In a solar cell comprising a photoreactive layer (10 and 12) and a primer coating (24) on said photoreactive layer, the improvement comprising a substantially colorless transparent protective polymeric coating (22) on said primer coating (24), said polymeric coating comprising the polyimide set forth in Claim 1 or 2. 6. The improvement as defined in Claim 5, where said polymeric coating having a thickness of about 0.2 mil (5.08 x 10"6m) to 0.5 mil (1.27 x 10-5m). 7. A method for applying to a solar cell a substantially colorless, transparent, protective, heat-resistant polymeric coating as set forth in Claim 2, said coating transmitting radiation and having high resistance to low energy protons, electron bombardment and resistance to ultraviolet light degradation, which comprises: a) applying a solution of polyamic acid to a solar radiation transmitting component of a solar cell, said polyamic acid having the recurring structural unit set forth in Claim 3? and *' b) heating said polyamic acid to convert same to the polyimide in the form of a film having the recurring structural unit set forth in Claim 2 and where n is a number ranging from 10 to about 2000. OMPI 8. The method as defined in Claim 7, said polyamic acid being formed by reacting equal molar proportions of the two monomers 2,2-bis(3-aminophenyl)hexafluoropropane and 4,4'-hexafluoroisopropylidenebis(phthalic anhydride), in a solvent for such monomers. 9. The method as defined in Claim 8, said solution containing a solvent selected from the group consisting of tetrahydrofuran, N-methyl pyrrolidinone, N-methylformamide, imethylformamide and N,N-dimethyl- acetamide, and mixtures thereof. z.

Inventors: BILOW NORMAN, DUPONT PRESTON S, BILOW, NORMAN, DUPONT, PRESTON, S.
Applicants: HUGHES AIRCRAFT CO, HUGHES AIRCRAFT COMPANY
Application year: 1983
Main classification: C08G73
IPC codes: C08G73, H01L23, H01L31