1. Field of the Invention
The present invention relates generally to solar cells, and more particularly but not exclusively to solar cell fabrication processes and structures.
2. Description of the Background Art Solar cells are well known devices for converting solar radiation to electrical energy. They may be fabricated on a semiconductor wafer using semiconductor processing technology. Generally speaking, a solar cell may be fabricated by forming p-doped and n-doped regions in a silicon substrate. Solar radiation impinging on the solar cell creates electrons and holes that migrate to the p-doped and n-doped regions, thereby creating voltage differentials between the doped regions. The side of the solar cell where connections to an external electrical circuit are made includes a topmost metallic surface that is electrically coupled to the doped regions. There may be several layers of materials between the metallic surface and the doped regions. These materials may be patterned and etched to form internal structures. It is important to etch these materials in a way that would not compromise the operability and performance of the solar cell.
A solar cell is fabricated by etching one or more of its layers without substantially etching another layer of the solar cell. In one embodiment, a copper layer in the solar cell is etched without substantially etching a topmost metallic layer comprising tin. For example, an etchant comprising sulfuric acid and hydrogen peroxide may be employed to etch the copper layer selective to the tin layer. A particular example of the aforementioned etchant is a Co-Bra Etch® etchant modified to comprise about 1% by volume of sulfuric acid, about 4% by volume of phosphoric acid, and about 2% by volume of stabilized hydrogen peroxide. In one embodiment, an aluminum layer in the solar cell is etched without substantially etching the tin layer. For example, an etchant comprising potassium hydroxide may be employed to etch the aluminum layer without substantially etching the tin layer.
These and other features of the present invention will be readily apparent to persons of ordinary skill in the art upon reading the entirety of this disclosure, which includes the accompanying drawings and claims.
The use of the same reference label indifferent drawings indicates the same or like components.
In the present disclosure, numerous specific details are provided such as examples of process parameters, materials, process steps, and structures to provide a thorough understanding of embodiments of the invention. Persons of ordinary skill in the art will recognize, however, that the invention can be practiced without one or more of the specific details. In other instances, well-known details are not shown or described to avoid obscuring aspects of the invention.
In
In the example of
Copper layer 110, copper layer 108, titanium-tungsten layer 106, and aluminum layer 104 form a Cu/TiW/Al metal stack that provides electrical connectivity to doped regions in silicon substrate 100. In one embodiment, copper layer 110 is electroplated to a thickness of about 20 microns on copper layer 108. Masks (not shown) may be formed between individual structures of copper layer 110 in gaps 113 before the electroplating process. The masks are removed after the electroplating process to obtain the structure shown in
Copper layer 108 serves as a seed layer for the electroplating of copper layer 110. Copper layer 108 may be formed to a thickness of about 1600 Angstroms by sputtering. Titanium-tungsten layer 106 and aluminum layer 104 may also be formed by sputtering. In one embodiment, titanium-tungsten layer 106 and aluminum layer 104 are each formed to a thickness of about 1000 Angstroms. Aluminum layer 104 may comprise aluminum with 1% silicon alloy.
Silicon dioxide layer 102 serves as a dielectric layer providing electrical isolation between the overlying Cu/TiW/Al metal stack and silicon substrate 100. Vias are formed through silicon dioxide layer 102 in sections where the Cu/TiW/Al metal stack makes contact with the doped regions in silicon substrate 100. In one embodiment, silicon dioxide layer 102 is formed to a thickness of about 950 Angstroms.
There may be steps in the fabrication of a solar cell where an etch is performed through a stack of materials comprising copper, titanium-tungsten, and aluminum. To prevent damaging the solar cell, each layer in the material stack may need to be etched without attacking (i.e., excessively etching) other layers of the solar cell. In the example of
One way of etching through copper layer 108, titanium-tungsten layer 106, and aluminum layer 104 is to use a so-called “PAWN” (phosphoric, acetic, water, nitric) solution to etch copper layer 108 and aluminum layer 104. For example, the sample of
Continuing in
In
In
The teachings of the present disclosure may be generally employed to etch one or more layers of materials in a solar cell being fabricated. For example, the etching techniques disclosed herein may be employed in the fabrication of solar cells disclosed in the following commonly-assigned disclosures, which are incorporated herein by reference in their entirety: U.S. application Ser. No. 10/412,638, entitled “Improved Solar Cell and Method of Manufacture,” filed on Apr. 10, 2003 by William P. Mulligan, Michael J. Cudzinovic, Thomas Pass, David Smith, Neil Kaminar, Keith McIntosh, and Richard M. Swanson; and U.S. application Ser. No. 10/412,711, entitled “Metal Contact Structure For Solar Cell And Method Of Manufacture,” filed on Apr. 10, 2003 by William P. Mulligan, Michael J. Cudzinovic, Thomas Pass, David Smith, and Richard M. Swanson. It is to be noted, however, that the aforementioned disclosures are referenced herein only as examples.
The etch chemistries provided herein not only allow selectivity to materials found in solar cells, but also have relatively high etch capacity, are cost-effective, and are easily replenished and controlled. Embodiments, of the present invention may thus be advantageously employed to etch a single layer of material or a stack of materials in solar cell fabrication processes in general.
Referring now to
In step 502 and with reference to
In step 504, the sample of
In step 506, copper layer 108 is etched as shown in
In step 508, the sample of
In step 510, titanium-tungsten layer 106 is etched as shown in
In step 512, the sample of
In step 514, aluminum layer 104 is etched as shown in
In step 516, the sample of
In step 518, the sample of
While specific embodiments of the present invention have been provided, it is to be understood that these embodiments are for illustration purposes and not limiting. For example, the above described etchants may also be applied using in-line drag-through and in-line spray systems. Many additional embodiments will be apparent to persons of ordinary skill in the art reading this disclosure.
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Number | Date | Country | |
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20050022861 A1 | Feb 2005 | US |