The invention generally relates to ribbon crystals and, more particularly, the invention relates to string used to form the ribbon crystals.
Solar cells may be formed from silicon wafers fabricated by a “ribbon pulling” technique. The ribbon pulling technique generally uses a crystal growth system that includes a specialized furnace surrounding a crucible containing molten silicon. During the growth process, two strings are typically passed through the crucible so that molten silicon solidifies onto its surface, thus forming a growing ribbon crystal between the two strings. Two or more ribbon crystals may be formed at the same time by passing multiple sets of strings through the crucible.
The composition and structure of the strings can affect the properties of the resultant ribbon crystal, which may impact the performance of devices made with such ribbon crystals, e.g., the conversion efficiency of a solar cell. The composition and structure of the string can also affect the manufacturing process, which may impact the cost of forming the ribbon crystal. For example, string formed of brittle materials may cause the string to break during the ribbon crystal growth process, causing reduced yields and unnecessary downtime during the manufacturing process. Similarly, manufacturing inefficiencies may also result when the string material and the melt material have large differences in coefficients of thermal expansion, which may result in breakage at the interface between the string and the ribbon crystal during the cooling process.
In accordance with one embodiment of the invention, a method of forming a string for use in a string ribbon crystal provides a refractory metal as a core for the string and forms a first layer of material on the core.
In accordance with another embodiment of the invention, a method of growing a ribbon crystal provides a pair of strings. Each string has a refractory metal core. The method also passes the strings through a molten material to grow the ribbon crystal between the pair of strings. Each string may have a first layer formed on the refractory metal core.
In accordance with another embodiment of the invention, a ribbon crystal wafer includes a ribbon crystal material and a pair of strings in the ribbon crystal material. Each string defines an outer edge of the wafer, and each string includes a refractory metal core. The string may have a first layer and a second layer.
In related embodiments, the method may further form a second layer of material on the first layer. The first layer may include silicon carbide and/or the second layer may include carbon. Forming may include a chemical vapor deposition process. Forming may include forming the first layer in a molten material that substantially forms the string ribbon crystal. Passing the strings through the molten material may further include forming a first layer on the refractory metal core in the molten material. The refractory metal may include titanium, vanadium, nickel, chromium, tantalum, niobium, tungsten, molybdenum, rhenium, or alloys thereof.
The foregoing and advantages of the invention will be appreciated more fully from the following further description thereof with reference to the accompanying drawings wherein:
Various embodiments of the present invention provide a string with a refractory metal core that may be used to grow a ribbon crystal. The string may also include one or more layers formed on the refractory metal core, formed either before or during the ribbon crystal growth process. A refractory metal core allows the string to be produced more easily and into longer lengths than would be possible with conventional prior art materials and processes.
Using a refractory metal material was initially not considered to be a viable option for replacing the core material in the string. This is primarily due to the fact that refractory metal materials act as contaminants in the ribbon crystal, and care is usually taken throughout the process to reduce the amount of contaminants that are present in the ribbon crystal. Contaminants may detrimentally affect the properties of the ribbon crystal, which may impact the performance of devices made with such ribbon crystals. It was surprisingly found, however, that the refractory metal contaminant level within the ribbon crystal was insubstantial, so it did not detrimentally impact the composition of the melt material. Details of illustrative embodiments are discussed below.
Although
The growth system 10 also includes insulation that is configured based upon the thermal requirements of the regions in the housing 12, e.g., the region containing the molten material and the region containing the resulting growing ribbon crystal 16. As such, the insulation includes a base insulation 26 that forms an area containing the crucible 14 and the molten material, and an afterheater 28 positioned above the base insulation 26 (from the perspective of the drawings). The afterheater 28 may be supported by the base insulation 26, e.g., by posts (not shown). In addition, or alternatively, the afterheater 28 may be attached or secured to a top portion of the housing 12. The afterheater 28 may have two portions which are positioned on either side of the growing ribbon crystals 16. The two portions may form one or more channels through which the ribbon crystal 16 grows. The afterheater 28 provides a controlled thermal environment that allows the growing ribbon crystal 16 to cool as it rises from the crucible 14. In some embodiments, the afterheater 28 may have one or more additional openings or slots 30 within the afterheater 28 for controllably venting heat from the growing ribbon crystals 16 as it passes through the inner surface of the afterheater 28.
The process begins at step 100, which provides a refractory metal core 32 for the string 24. The refractory metal core 32 is formed with a refractory metal material. As defined herein, a refractory metal is a material that has a melting temperature of about 1200° C. or higher, such as titanium, vanadium, nickel, chromium, tantalum, niobium, tungsten, molybdenum, rhenium, or alloys thereof. For example, the refractory metal material should be able to sufficiently withstand the high temperatures of the melt. The refractory metal core 32 may be fabricated by known forming processes, such as wire drawing or extrusion. One of the benefits of using a refractory metal is its ease of manufacturing, which can subsequently improve the manufacturability of the string itself. For example, embodiments of the present invention may allow the string to be formed into longer lengths than previously provided with prior art processes.
For instance, in current string forming processes, the material typically used to form the string core is carbon. Carbon is relatively difficult to handle and tends to break due to its brittle nature. This results in shorter lengths for the core material, and thus the string, which translates into reduced yields for the ribbon growth process. For example, the string manufacturing process would need to be more frequently interrupted in order to introduce the new core into the system. In addition, the standard carbon core is typically more difficult to make than embodiments of the present invention (e.g., metal forming processes, such as extrusion). This may further lead to manufacturing variations and increased production costs. For example, the carbon core is typically a monofilament fiber that is formed with standard ceramic forming processes. These processes typically entail numerous steps, such as a spinning step to form the material into the desired shape, an oxidation step to stabilize the material, and a carbonization step to leave a substantially carbon fiber, which may also introduce dimensional variations to the string's core.
In contrast, embodiments of the present invention use metal forming processes, such as extrusion, which allow the core to be produced more easily, more repeatably with less dimensional variations, and into longer lengths than would be possible with the prior art materials and processes. The refractory metal core 32 may be formed into a substantially cylindrical shape having any desired diameter and length. For example, in a string having a diameter of about 150 μm or so, the refractory metal core 32 may be about 10 μm to about 30 μm in one embodiment, and may be about 80 μm to about 130 μm in another embodiment, although other diameters may be used.
In step 120, a first layer 34 is formed on the refractory metal core 32. The first layer 34 may be formed from a material with a similar coefficient of thermal expansion as the melt material. For example, when silicon is the melt material, the first layer 34 may be silicon carbide, such as a carbon-rich silicon carbide. The first layer 34 may be formed on the refractory metal core 32 before entering the melt by any known forming process. For example, the first layer 34 may be formed on the refractory metal core 32 using a chemical vapor deposition process. Alternatively, the first layer 34 may be formed in the melt material when the refractory metal core 32 contacts the melt material. The melt material may react with or diffuse into the refractory metal core 32 forming the first layer 34. For example, when tungsten is the refractory metal core material and silicon is the melt material, the first layer 34 may be formed from tungsten silicide. The first layer 34 may have any desired thickness. For example, in a string having a diameter of about 150 μm or so, and the first layer 34 formed on the refractory metal core 32 before entering the melt, the refractory metal core 32 may be about 10 μm to about 30 μm and the first layer 34 may be about 60 μm to about 70 μm, although other thicknesses may be used. Similarly, in a string having a diameter of about 150 μm or so, and the first layer 34 formed on the refractory metal core 32 in the melt material, the refractory metal core 32 may be about 80 μm to about 130 μm and the first layer 34 may be about 20 μm to about 70 μm, although other thicknesses may be used.
In step 130, an optional second layer 36 may be formed on the first layer 34 when the first layer 34 is formed before entering the melt. The second layer 36 may be formed of a material that wets well to the melt material, but is thin enough that it does not substantially affect the coefficient of thermal expansion properties between the first layer 34 and the melt material. For example, when silicon is the melt material, the second layer 36 may be a carbon layer that, preferably, is about a few microns in thickness. The second layer 36 may be formed on the first layer 32 by any known forming process. For example, the second layer 36 may be formed on the first layer 34 using a chemical vapor deposition process.
Although one or two layers are discussed above, additional layers may be formed on the refractory metal core 32 depending on the application in embodiments where the first layer 34 is formed before entering the melt. In addition, other shapes and configurations may be used for the refractory metal core 32, the layers 34, 36, and/or the string 24, e.g., as disclosed in U.S. patent application Ser. No. 12/200,996, entitled Reduced Wetting String for Ribbon Crystal, U.S. patent application Ser. No. 12/201,117, entitled Ribbon Crystal String for Increasing Wafer Yield, and U.S. patent application Ser. No. 12/201,180, entitled Ribbon Crystal String with Extruded Refractory Material, all filed on Aug. 29, 2008, the disclosures of which are incorporated herein by reference in their entirety.
Once string 24 is formed, two or more strings 24 are passed through the crucible 14 at a rate as to allow the molten material to solidify onto its surface, thus forming the growing ribbon crystal 16 between the two strings 24 (step 140). Two or more ribbon crystals may be formed at the same time by passing multiple sets of strings 24 through the crucible 14. For example, the crucible 14 may have an elongated shape with a region for growing ribbon crystals 16 in a side-by-side arrangement along its length, as shown in
After the ribbon crystals 16 are pulled out of the housing 12, they may be cut into strips or wafers 38 of desired length, such as shown in
The ribbon crystals 16 may be cut using a laser cutting process, as is well known to those skilled in the art. The resulting wafer 38 may then be subjected to additional processes depending on its application. For example, in photovoltaic applications, the wafer 38 may be subjected to a texturing process in order improve the conversion efficiencies of the wafer 38. The wafer 38 may also be subjected to a metal etch process in order to clean off any surface contaminants that may inadvertently get incorporated into the wafer in subsequent processes. The wafer 38 may also be subjected to a deposition process (e.g., an n-type or p-type material deposited onto the wafer) and a high temperature diffusion process in order to drive the n-type or p-type material into the wafer 38.
Throughout the manufacturing process, there was a concern that the refractory metal core material would be introduced into the ribbon crystal 16 or wafer 28 at various times and contaminate it. For example, if the string broke while in the melt, the exposed refractory metal material could be incorporated into the melt material. Similarly, during the laser cutting process, the exposed refractory metal material could get incorporated into the wafer during the cutting process or the subsequent high temperature diffusion process. Surprisingly, however, the refractory metal material did not get incorporated into the ribbon crystal or wafer in any significant amount. Although the reasons behind this surprising result are not fully understood, it is believed that any exposed refractory metal material forms a protective layer with the melt or the ribbon crystal material. For example, if the refractory metal core material is tungsten and the ribbon crystal material is silicon, the exposed refractory metal core material may form a tungsten silicide, which is not incorporated into the ribbon crystal or wafer materials. Thus, it was realized that the process of forming the first layer 34 on the refractory metal core 32 may occur before the refractory metal core 32 enters the melt or while the refractory metal core 32 is in the melt.
Although the above discussion discloses various exemplary embodiments of the invention, it should be apparent that those skilled in the art can make various modifications that will achieve some of the advantages of the invention without departing from the true scope of the invention.
The present application claims priority to U.S. Provisional Patent Application No. 61/093,946 filed Sep. 3, 2008, the disclosure of which is incorporated by reference herein in its entirety.
Number | Date | Country | |
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61093946 | Sep 2008 | US |