Patent Application
20050252545
This invention concerns solar cell arrays and, in particular testing of solar cells and solar cell subassemblies prior to fabrication of finished modules.
Solar cell modules must not only convert sunlight into electrical current in an efficient manner but they must also be robust and durable enough to operate without servicing in remote or harsh environments. The need for highly reliable and weather resistant modules has lead to environmentally sealed constructions that require significant expense to assemble. Unfortunately, completed modules can sometimes fail, or operate in a sub-optimal manner, due to structural defects in one or more individual cells or in the wiring of such cells together. Often these faults are not detected until after encapsulation, when repair of defective cells is no longer possible.
There exists a need for better quality control during the steps that precede solar cell module finishing. Methods and apparatus that can detect defects in individual solar cells (or in strings of such cells) prior to final module assembly in a rapid or automated manner would satisfy a long-felt need in the art.
This invention discloses methods and apparatus for detecting solar cell defects by applying a forward-biasing electric current through a silicon solar cell or a group of interconnected solar cells for a short duration and then analyzing the resulting thermal image of each cell with an infrared (IR) camera. The invention is particularly useful in assembling solar cell arrays or modules in which large numbers of cells are to be wired together. Automated module assemblers are disclosed in which the cells (or strings of cells) are tested for defects prior to final module assembly.
The invention permits detection of defects such as microcracks, chipped cells, alignment errors and/or defective or missing solder joints, before module assembly and encapsulation. By providing quality assurance at this stage, the costs associated with assembly of non-functional (or low efficiency) modules can be avoided.
In
A variety of solar cell sizes and shapes can be processed. The number of cells per string, the number of strings per module, and the string orientation in the module are software programmable. Each completed string is ready for further processing by a module assembler 50.
However, prior to module assembly, the solar cells strings are tested in accordance with the present invention by test assembly 60. The test unit 60 can include a photoelectric test station 62. In one preferred embodiment of the photoelectric tester 62, a pulsed xenon lamp 64 illuminates the cell string, and an I-V curve is measured via electronic load and meter 66. Strings that fail the photoelectric response test are placed in a reject bin.
In a second defect-detection station 68, structural defects are detected by applying a forward-bias current to the string with a current source 70 to cause heating. In one embodiment, the forward-bias current density through one or more cells can range from about 70 mA/cm2 to about 200 mA/cm2. The cells are then thermally imaged, e.g., with an infrared CCD camera 72. Defects such as microcracks, chipped cells, alignment errors and/or defective or missing solder joints can be detected by discontinuities in the thermal image.
In one preferred embodiment, the inspecting step includes a comparison of the thermal image of a solar cell under inspection with a corresponding thermal image of a reference cell. The image analysis can employ, for example, an edge detection technique to detect microcracks, chips and the like. In this technique, detected edges can be compared with a known or model cell geometry to detect features that deviate from model cell parameters. Alternatively, the image analysis can be based on intensity variance measurements, in which non-uniformities are indicative of defects. Image analysis can be conducted with or without comparison to reference values. Based on this image analysis, the strings are again placed either in a reject bin or in the proper location for further assembly of the strings into modules in the module assembler 50.
In the module assembler 50, the module circuit design specifies the number of cells connected in series, the number of cells connected in parallel, and the frequency of parallel interconnects. The number of cells in series determines the module operating voltage. The cell area and the number of cells in parallel are proportional to the module current output. The assembled module is then encapsulated.
For example, the finished module can consist of interconnected and encapsulated solar cells in a durable and environmentally protected package. Tempered low-iron glass is normally used for the front cover (or superstrate) to provide permanently transparent protection for the optical surface of the module. However, other types of glass, such as window glass, may be used. The remainder of the laminate can consist of clear ethylene vinyl acetate (EVA) encapsulant, the cell circuit, a second layer of EVA, a fiberglass sheet, and a back cover film.
It should be appreciated that the techniques described above can be practiced in both fully-automated and batch-mode inspection processes. These techniques can be integrated with string assembly, as described, or they can be done as a stand alone operation. It should also be apparent that the techniques for testing of solar cell strings can be applied equally to the testing of individual cells. One advantage of performing thermal imaging after string assembly is that both structure faults in the individual cells and wiring defects in the strings can be determined at the same time before the more significant expense of module finishing and encapsulation is carried out.
Background information and further details on assembly of solar cell modules can be found in a report published by the National Renewal Energy Laboratory entitled “Automated Solar Cell Assembly Teamed Process Research” Pub. No. NREL/TP-411-20794 (February 1996), incorporated herein in its entirety by reference.
Those having ordinary skill in the art will appreciate that various modifications can be made to the above embodiments without departing from the scope of the invention.
The U.S. government has rights in this invention pursuant to contract awarded by the National Renewal Energy Laboratory, Contract No. ZDO-3-306628-12. This invention concerns solar cell arrays and, in particular testing of solar cells and solar cell subassemblies prior to fabrication of finished modules.
