The present invention relates to an InGaAsN solar cell device, in particular with a wide depletion region width resulting in high short circuit current density. A method of making such a structure is also presented.
High efficiency multi junction solar cells based on III-V compound semiconductor p-n material have been proposed for space and concentrator photovoltaic applications. The solar spectrum consists of electromagnetic radiation across a whole spectrum of wavelengths, from 280 nm up to 4000 nm. A semiconductor layer absorbs photons with energy greater than its band gap and the electricity produced by a solar cell is the product of the current and voltage produced. Although a low band gap semiconductor will absorb most of the energy from the solar spectrum, a large current is generated but with low voltage, which is not desirable for many solar applications. As a result, single junction solar cells have low efficiencies.
To enable both large current and voltage generation capability, multi junction solar cell configuration has been suggested and used. Two or more semiconductor junctions connected in series are used, whereby each junction is designed to absorb a certain portion of the energy band. The current in the series connected multi junction solar cell is limited by the lowest current sub-cell, and the voltage generated is the sum of each sub-cell's voltages.
The most efficient solar cells to-date are multi junction solar cells. Fraunhofer Institute [Applied Physics Letters, vol. 94, pp. 223504 (2009)] reported a 41.1% efficient cell under 454 suns concentration (31.6% efficient under one-sun) using a metamorphic In0.65Ga0.35P/In0.17Ga0.83As/Ge triple junction cell. Boeing's Spectrolab later reported a 41.6% efficient cell using a similar triple junction configuration. The AM1.5 spectrum is shown on
Despite the potential benefits of an InGaAsN-based four junction cell, achieving good material quality in this material system is difficult. The high defect density in this material system results in high background doping levels and short minority carrier diffusion length of <200 nm [D. B. Jackrel, Journal of Applied Physics, vol. 101, 114916 (2007)].
In U.S. Pat. No. 6,252,287 B1 (issued Jun. 26, 2001), S. Kurtz et al. have increased the minority carrier diffusion length in InGaAsN/GaAs heterojunctions by rapid thermal annealing the sample at 650° C.-700° C. for a few minutes up to one-half hour, resulting in increased minority carrier diffusion length from 0.2-0.3 μm to 0.6-0.8 μm.
In U.S. Pat. No. 5,944,913 (issued Aug. 31, 1999), H. Q. Hou et al. used a metal organic chemical vapour deposition (MOCVD) grown p-n homojunction 1.05 eV InGaAsN and observed an increase in photoluminescence (PL) intensity upon in-situ annealing at 700° C.-800° C. for 5-10 minutes (
Another method to circumvent the short diffusion length in InGaAsN is by aiding the photo-generated carrier collection using a wide depletion region, whereby the effective collection length of photo-generated carriers is enhanced using the built-in electric field of the depletion region. Friedman et al. [Analysis of depletion-region collection in GaInNAs solar cells, “31st IEEE Photovoltaics Specialist Conference, Lake Buena Vista, Fla., (2005)] has shown by simulation that by increasing the depletion region width, the EQE of InGaAsN samples can be enhanced (
Although conventional wisdom may suggest that using a thick undoped i-region would result in a wide depletion region, this method has yet to produce wide depletion region width InGaAsN devices. To achieve InGaAsN with bandgaps of 1.0 eV to 1.05 eV, nitrogen (N) incorporation would have to increased to 2.5-3.0% (Indium content ˜8%). However, the material quality degrades with increasing N content and leads to high background doping concentration in the i-region and subsequently narrow depletion regions. As a result, achieving wide depletion region in 1.0-1.05 eV InGaAsN material has yet to be achieved. Depletion region widths reported in the prior art are less than 500 nm.
Ptak et al. [“Enhanced depletion-width GaInNAs solar cells grown by molecular beam epitaxy,” 31st IEEE Photovoltaics Specialist Conference, Lake Buena Vista, Fla., (February 2005)] have used a p-i-n GaAs/InGaAsN heterostructure with bandgaps of 1.15 V and 1.28 eV and successfully achieved wide depletion region widths of 2.3 μm and 2.7 μm respectively. Nevertheless, the bandgap of InGaAsN material at 1.15 eV remains too large and is not useful in a lattice matched 4-junction cell even if EQE of 100% is achieved.
Jackrel et al. [“Journal of Applied Physics, vol. 101, pp. 114916 (2007)] have used a p-i-n GaAs/InGaAsN heterostructures with an i-region thickness of 1-μm for band gaps of 1.03 eV and 1.08 eV and achieved depletion region widths of 280 nm and 370 nm, respectively. Therefore, despite the thick i-region used, the depletion region width remains small at <0.4 μm.
Similarly, Friedman et al. [“GaInNAs Junctions for Next-Generation Concentrators: Progress and Prospects,” International Conference on Solar Concentrators for the Generation of Electricity or Hydrogen, Scottsdale, Ariz. May 2005] achieved a depletion region width of only 500 nm for a 1-μm i-region p-i-n MOCVD-grown GaAs/InGaAsN sample. Note that no post-growth treatments were used or described in all examples given by Ptak et al., Jackrel et al. and Friedman et al.
Ptak et. al., [“Effects of temperature, nitrogen ions, and antimony on wide depletion width GaInNAs,” Journal of Vacuum Science and Technology B, vol. 25 (3), (May 2007)] have used deflection plates and increased nitrogen flow to increase the depletion region width in a 3-μm i-region 1.15 eV p-i-n GaAs/InGaAsN samples. Although the depletion region width was increased from 1.9 μm to 2.4 μm, the InGaAsN bandgap remains too large and is not feasible in a lattice matched 4-junction cell.
Therefore, these examples clearly indicate that achieving wide depletion region for 1.0-1.05 eV InGaAsN is non-trivial, and a structure and method of achieving this is required in the art. The poor minority carrier diffusion length coupled with the inability to achieve wide depletion region widths have resulted in poor Jsc achieved to-date of ˜7 mA/cm2, much lower than the maximum achievable value of ˜16 mA/cm2 (light harvested from 873 nm to 1240 nm, AM1.5G).
The aim of the present invention is to produce an InGaAsN solar cell structure with a wide depletion region width, and high Jsc performance. A method of manufacturing for such a structure is also described.
The present invention describes an InGaAsN solar cell structure with a bandgap of 1.0 eV-1.05 eV, with a wide depletion region width and a method of making. The resulting device produces a high Jsc which is suitable for use in a 4-junction lattice matched solar cell.
An aspect of the invention is that for the structure to consist of an n-i-p InGaAsN homojunction with bandgaps of between 1.0 eV to 1.05 eV. The undoped i-region thickness of the sample is at least 1.0 μm, and has a depletion region width of at least 1.0 μm.
Another aspect of the invention is a structure for the wide depletion region width n-i-p InGaAsN homojunction to be configured in a lattice matched 4-junction solar cell.
According to another aspect of the invention, a manufacturing method for providing a wide depletion region InGaAsN layer is described, comprising the steps of ex-situ rapid thermal annealing at temperatures of between 900° C. to 1000° C. in N2 ambient. The high anneal temperature increases the depletion region width to its i-region thickness.
According to a particular aspect of the invention, the method to achieve the wide depletion region width results in an ideality factor of ˜2.0, whereby the dark current mechanism is now dominated by recombination in the space charge region.
According to an aspect of the invention, an InGaAsN solar cell is provided which includes an InGaAsN structure having a bandgap between 1.0 eV to 1.05 eV, and a depletion region width of at least 1.0 μm.
In accordance with another aspect, the InGaAsN structure includes a p-doped InGaAsN layer, an n-doped InGaAsN layer, and an undoped InGaAsN i-region layer disposed between the p-doped and n-doped layers. The p-doped, n-doped and i-region layers each have a bandgap between 1.0 eV to 1.05 eV.
According to yet another aspect, the i-region layer has a thickness of at least 1.0 μm.
In accordance with still another aspect, the solar cell includes one or more additional junctions lattice matched with the InGaAsN structure.
According to another aspect of the invention, the solar cell is a lattice matched 4-junction solar cell.
According to still another aspect of the invention, a method of making an InGaAsN solar cell is provided. The method includes forming an InGaAsN structure with a bandgap between 1.0 eV to 1.05 eV, and thermally annealing the structure at a temperature of at least 900° C.
According to another aspect, the structure includes a p-doped InGaAsN layer, an n-doped InGaAsN layer, and an undoped InGaAsN i-region layer disposed between the p-doped and n-doped layers, wherein the p-doped, n-doped and i-region layers each have a bandgap between 1.0 eV to 1.05 eV.
In accordance with still another aspect of the invention, the step of thermally annealing includes ex-situ rapid thermal annealing.
According to yet another aspect, the step of thermally annealing is performed in an N2 ambient.
In accordance with another aspect, the step of thermally annealing increases a depletion region width of the structure to at least 1.0 μm.
According to another aspect, the step of thermally annealing increases a depletion region width of the structure to the thickness of the i-region layer.
In accordance with yet another aspect, the structure is annealed at a temperature of between 900° C. to 1000° C.
According to still another aspect, the structure is grown by molecular-beam epitaxy.
According to another aspect, the resultant solar cell has an ideality factor of approximately 2.0.
To the accomplishment of the foregoing and related ends, the invention, then, comprises the features hereinafter fully described and particularly pointed out in the claims. The following description and the annexed drawings set forth in detail certain illustrative embodiments of the invention. These embodiments are indicative, however, of but a few of the various ways in which the principles of the invention may be employed. Other objects, advantages and novel features of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the drawings.
In the annexed drawings, like references indicate like parts or features:
The present invention provides an InGaAsN solar cell with bandgap of 1.0 eV to 1.05 eV and has a wide depletion region width. The solar cell and method of achieving the wide depletion region width is described.
In an exemplary embodiment, the configuration of an n-i-p InGaAsN structure with wide depletion region width in a lattice matched 4-junction solar cell is described with reference to
Referring now to
With specific reference to
Samples A to C are rapidly annealed at much higher temperatures>900° C. for 30 seconds, and this method found to produce a wide depletion region width. Although the annealing is conducted under N2 ambient and on pre-processed samples, this sequence is not exhaustive and can also be applied on post-processed samples. A GaAs wafer is used to cap the InGaAsN surface to prevent surface desorption at high temperatures. The key feature to achieve the wide depletion region width is the ‘trigger point anneal temperature’ between 900° C.-1000° anneal, whereby the depletion region width is found to extend to almost its full i-region thickness when triggered. The trigger point is found to be at 925° C. for samples A and B, and 910° C. for sample C, and up to 950° C. in other samples. C-V measurements are used to determine if the trigger point has been met, whereby the depletion region width will increase thereafter. Using the invention method, the depletion region width extends upon activating the trigger point at high anneal temperatures. From
To determine the light I-V performance, a commercial one-sun solar simulator under AM1.5G conditions (Total Power=100 mA/cm2) is used.
Although the invention has been shown and described with respect to a certain embodiment or embodiments, equivalent alterations and modifications may occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. For example, although the present invention is described herein primarily in the context of an n-i-p type structure, it will be appreciated that the present invention may also be implemented in a p-i-n type structure. In particular regard to the various functions performed by the above described elements (components, assemblies, devices, compositions, etc.), the terms (including a reference to a “means”) used to describe such elements are intended to correspond, unless otherwise indicated, to any element which performs the specified function of the described element (i.e., that is functionally equivalent), even though not structurally equivalent to the disclosed structure which performs the function in the herein exemplary embodiment or embodiments of the invention. In addition, while a particular feature of the invention may have been described above with respect to only one or more of several embodiments, such feature may be combined with one or more other features of the other embodiments, as may be desired and advantageous for any given or particular application.
An InGaAsN solar cell structure with a wide depletion region width and high Jsc performance is provided. The structure is suitable for space and concentrator photovoltaic applications as well as other solar cell applications. A method of manufacturing such a structure is also provided.