The present disclosure relates in general to the fields of photovoltaic (PV) solar cells, and more particularly to self aligned contacts for solar cells.
As photovoltaic solar cell technology is adopted as an energy generation solution on an increasingly widespread scale, fabrication and efficiency improvements relating to solar cell efficiency, metallization, material consumption, and fabrication are required. Manufacturing cost and conversion efficiency factors are driving solar cell absorbers ever thinner in thickness and larger in area, thus, increasing the mechanical fragility, efficiency, and complicating processing and handling of these thin absorber based solar cells—fragility effects increased particularly with respect to crystalline silicon absorbers.
Generally, solar cell contact structure includes conductive metallization on base and emitter diffusion areas—for example aluminum metallization connecting silicon in base and emitter contact areas through relatively heavy phosphorous and boron areas, respectively.
The features, natures, and advantages of the disclosed subject matter may become more apparent from the detailed description set forth below when taken in conjunction with the drawings in which like reference numerals indicate like features and wherein:
Therefore, a need has arisen for fabrication methods for back contact solar cells. In accordance with the disclosed subject matter, methods for the fabrication of back contact solar cells are provided. These innovations substantially reduce or eliminate disadvantages and problems associated with previously developed back contact solar cell fabrication methods.
Related patent applications having partially common inventorship and providing structure and fabrication details in addition to those described herein include U.S. patent application Ser. No. 14/179,526 filed Feb. 2, 2014, U.S. patent application Ser. No. 14/072,759 filed Nov. 5, 2013 (Published as U.S. Pub. 20140326295 on Nov. 6, 2014), U.S. patent Ser. No. 13/869,928 filed Apr. 24, 2013 (Published as U.S. Pub. 20130228221 on Sep. 5, 2013), U.S. patent application Ser. No. 14/493,341 filed Sep. 22, 2014, and U.S. patent application Ser. No. 14/493,335 filed Sep. 22, 2014, all of which are hereby incorporated by reference in their entirety.
According to one aspect of the disclosed subject matter, self aligned contacts for a back contact back junction solar cell are provided. The solar cell comprises a semiconductor layer having a light receiving frontside and a backside opposite the frontside and attached to an electrically insulating backplane. A first metal layer having base and emitter electrodes self aligned to base and emitter regions is positioned on the semiconductor layer backside. A patterned second metal layer providing cell interconnection and connected to the first metal layer by via plugs is positioned on the backplane.
These and other advantages of the disclosed subject matter, as well as additional novel features, will be apparent from the description provided herein. The intent of this summary is not to be a comprehensive description of the subject matter, but rather to provide a short overview of some of the subject matter's functionality. Other systems, methods, features and advantages here provided will become apparent to one with skill in the art upon examination of the following FIGURES and detailed description. It is intended that all such additional systems, methods, features and advantages included within this description be within the scope of the claims.
The disclosed subject matter provides structures and methods for making self aligned contacts for back contact back junction solar cells. Specifically, the disclosed subject matter and corresponding figures provide low-damage, high-efficiency, and low-cost process flows for the formation of thin silicon solar cells using self aligned contacts for back contact back junction (e.g., interdigitated back contact IBC) solar cells. The novel self aligned contact structures described may achieve higher solar cell conversion efficiency. Additionally, solar cell fabrication methods having minimal or reduced process steps for the formation of solar cell structures with self aligned contacts are described.
The term self aligned describes cell structure such that the heavy doping of n+ and p+ areas under the base and emitter metal contacts are self-aligned with respect to the contact openings—such as that shown in
An advantage of a self aligned structure is that heavy doping areas are limited to only under the contact where they are needed. If the contact open needs to be aligned to the heavy doping with non-self aligned contact structures, the heavy diffusions need to be much wider than the contact open to accommodate for alignment tolerances. As compared to non-self aligned contact structures, the self aligned contact structures provided may have higher efficiency because of two distinct reasons. First, heavy dopings may be deleterious when used under passivation—in other words heavy dopings are more and in some instances only useful when used under poor passivation such as metal. Thus, a self-aligned structure eliminates the areas of heavy doping under high quality passivation. Second, for a non-self aligned structure two openings need to be made: first for doping and second for contact open. If these openings are made using methods which are prone to creating damage in silicon (e.g., in some instances laser processing) a self-aligned structure removes the outer nesting opening and minimizes and in some instances eliminates laser damage from this step. Further, in addition to efficiency advantages, the self-aligned structure may require less process steps and thus reduce cell cost.
Table 1 below shows a front-end process flow for the formation of a selective emitter solar cell having self aligned contacts and a field emitter—such as that shown in FIG. 1A—using a dopant paste step.
Table 1 shows a process flow where self-aligned contact is used for making high efficiency back contact back junction solar cell. Shown, Step 1 is a saw damage removal step to remove damage from a wafer (e.g., a CZ wafer); however, the flows provided are equally applicable to an epitaxially formed silicon substrate processed while on template in which case Step 1 Saw Damage Removal is replace with a porous silicon and epitaxial silicon deposition step as described in detail herein. Thus, in epitaxial embodiments, the front-end processing described occurs on the exposed surface of the template attached epitaxial substrate after which the epitaxial substrate may be released (e.g., mechanical or wet etch release) from the template in back end processing. Importantly, the exemplary process flows provided are described in the context of fabrication high efficiency back contact back junction solar cells for descriptive purposes and one skilled in the art may combine, add or remove, alter, or move within an overall process flow the various processing steps disclosed. In other words, elements from each of the process flows described in the table provided herein may be combined together or with other known solar cell manufacturing methods. For example, with reference to Table 1: the laser contact open shown in Step 3 in can be separated in two steps (for example as shown in Table 2) to form self aligned contacts only for base and emitter contacts separately; the dopant paste printing step shown in Step 4 may have additional third print of undoped paste on top of already printed dopant pastes (for example as shown in
Table 2 below shows a front-end process flow for the formation of a selective emitter solar cell having self aligned contacts using dopant paste and using separate contact open steps.
Table 3 below shows a front-end process flow for the formation of a selective emitter solar cell having self aligned contacts with dopant paste and the application of a diffusion barrier.
Alternatively, the diffusion barrier deposition shown in Step 5 of Table 3 as an APCVD USG deposition may also be an undoped paste print.
The process flow embodiments of Tables 2 and 3 may be used to reduce autodoping from dopant pastes during diffusion anneal.
Table 4 below shows a front-end process flow for the formation of a non abutted junction solar cell—such as that shown in FIG. 1C—having self aligned contacts with diffusion barrier dopant paste print.
Alternatively with reference to the non abutted junction solar cell flow of Table 4, Steps 2, 3, and, 4 of Table 4 may be replaced with two steps of APCVD boron doped silicon oxide (BSG1) deposition followed by picosecond (ps) CO2 laser—an alternative embodiment referred to as self aligned contacts with dopant paste print and non abutted junction with boron doped silicon oxide by APCVD.
Table 5 below shows the fabrication process flow for a non selective emitter solar cell having self aligned contacts and using phosphorous dopant paste.
Alternatively, Table 6 below shows the fabrication process flow for a non selective emitter solar cell having self aligned contacts and using phosphorus oxychloride POCl3 (POCl).
Table 7 below shows the fabrication process flow for a non selective emitter solar cell having self aligned passivated base contacts using dopant paste.
Table 8 below shows the fabrication process flow for solar cells having self aligned base tunneling/hetero junction contacts—such as those shown in
Table 9 below shows the fabrication process flow for solar cells having self aligned contacts without a heavy diffusion region below the base contact.
Alternatively, the self aligned contact structures and methods described herein may be applied to a
Table 10 below shows a front-end process flow for the formation of a solar cell having self aligned contacts with a field base—such as that shown in
Alternatively, Table 11 below shows a front-end process flow for the formation of a solar cell having a field base self aligned contacts with etch paste and dopant paste prints—such as that shown in
While the methods to manufacture self-aligned back contact back junction solar cells are described in general context of CZ wafers, these methods are also equally applicable in context of epitaxially grown back contact back junction solar cells. In addition, the methods are applicable to both thick crystalline silicon (e.g., having an absorber thickness in the range of approximately 100 um to 200 um) as well as thin crystalline silicon back contact back junction solar cells (e.g., having an absorber thickness in the range of approximately 5 um to 100 um).
Generally and particularly applicable to the process flows represented in the tables below, emitter or base contacts are opened sequentially (in either order) or simultaneously using various field dielectric removal techniques such as using lasers or wet etch or etch paste. And subsequently, depositing the dopant source in the opened contact, driving the dopant into silicon at high temperature, and selectively removing/etching the dopant source while keeping the field dielectric unharmed from the etchant. This leaves the dopant driven into silicon only in the area under where the contact was opened leaving a self-aligned structure.
The methods of manufacturing described may be further categorized by the source of the under-contact dopants. These can be from a dopant paste (for example phosphorous for n-type and Boron for p-type) or deposited films which incorporate dopants in them, for example APCVD deposited Boron or phosphorous doped SiO2 films. Finally, a hybrid source where N+ and p+ dopant sources come from APCVD for one type and dopant paste for the other type of dopant. A further subcategory is defined by the technique to etch away/remove the dopant source which is applicable to both wafer and epitaxial based absorbers as well as dopant source categories (dopant paste, APCVC film, and hybrid dopant source). As an example, for oxide based dopant sources such as doped SiO2, either a wet process with HF can be used or a dry process using HF vapor phase etching may be deployed. If the field area is also SiO2 then the wet HF selectivity is obtained as a heavily doped SiOx film may etch much faster than an undoped film. Alternatively the field area stack may contain an Al2O3 (e.g., deposited using APCVD as well). This film, once treated at high temperatures for example greater than 900° C., may have high selectivity to HF solution. Alternatively, HF vapor also very selectively etch the dopant source.
Generally, if the contacts are opened simultaneously, then both dopant sources may be screen printed dopant paste. If the contacts are open sequentially, then a deposited film for both contacts or hybrid sources can be utilized.
Table 12 shows a front-end self aligned contact fabrication flow which yields a separated junction and is accomplished using dopant pastes (for example, screen printed dopant pastes). In the separated junction the emitter doping is not abutting the base contact doping and is separated by the background bulk doping of the base. Step 2 shows the deposition of the emitter followed by a cap. And although the emitter source is shown to be an APCVD deposited boron doped Al2O3, it may also be a boron doped SiO2 layer or another dopant source layer deposited using different means. The first laser ablation (Step 3) is to open up the separation between emitter and base doping such that upon anneal, there is a separation between the junctions. The flow suggests using laser ns UV and ps UV. Pico second green laser, a femto second laser, or etch paste or lithography techniques may also be used to create this base window. If pico second laser is used, it may be followed by a small wet etch of silicon to remove laser damage in silicon. Step 5 of Table 12 may also be done using pico second green laser or a femto second laser. Step 5 is a contact open within the base window for base contact as well as a contact open for the emitter. Both contacts are opened up in the same step—hence the method of printing the dopant source should be a selective print on top of these contacts such as screen printing of the dopant paste (as compared to a blanket deposition of a thin dopant sourced film). Subsequent to anneal to drive the dopants in both contacts in Step 7, the dopant source is either wet etched or etched selectively using HF vapor. In a separate embodiment if the source of the dopant is conductive as with silicon based dopant source, the etching step may be skipped (Step #8).
In another embodiment, if there is risk of co-diffusion during drying or dopant driving the contacts can be opened sequentially. In this scenario, either base or emitter contact is opened first and the corresponding paste is printed and dried. Next, the other contact is opened and the corresponding paste is printed and dried. Finally, both pastes are driven in at the same time. This alternative may avoid cross contamination in the contact during drying and burn.
In a more extreme case if the problem of cross contamination is during the dopant drive, then contact open, dopant paste print, drying/burn, and anneal may be performed on one type of dopant. This sequence is followed by the same steps repeated for the second type of contact. This leads to two different anneals in which case the thermal budgets should be optimized.
In an abutted junction embodiment of the process flow in Table 12, Steps 3 and 4 may be skipped and contacts can be directly opened for both base and emitter.
Finally, in another variation, the field area may be capped by a thin film which is resistant to the dopant source etchant chemistry. In the case where the dopant source is SiOx based, and the etching chemistry is HF based, the cap layer may be APCVD based Al2O3 (undoped or doped) or titanium oxide (TiO2) or amorphous silicon (a-Si).
Table 13 shows a front end separated junction self aligned solar cell process flow using only APCVD deposited films which serves as dopant sources. This flow follows the same steps as Table 12 (with all the variations described above) until Step 4. At Step 5, only one type of contact is opened first. In this case it is the emitter contact (for an n-type back contact cell). This is followed by an APCVD BSG film which is the dopant source for emitter contact doping (Step 6). Next, the base contact is opened and PSG is deposited using APCVD. In a variation, the sequence of emitter and base contact open can be reversed. An abutted version of the separated junction flow described in Table 13 skips/removes Steps 3 and 4 to create abutted junctions.
Table 14 below shows a front end separated junction self-aligned process flow using a hybrid approach. In this approach one of the dopant source is a deposited APCVD film while the other type of dopant source is a printed dopant paste.
The flow of Table 14 shares the first four steps (along with its variations) with Table 13. In Step 5 of Table 14, the emitter contact is opened. BSG is deposited in Step 6 and Step 7 opens base contact with a laser (note, although, the flow suggests using ps lasers, nano or femto second lasers with different wavelengths are not precluded as long as they meet the contact open requirements). Subsequently, phosphorous based dopant paste is printed, dried in Step 8. Step 9 is an anneal step to drive the dopants from the BSG and from the phosphorous paste to create under-contact doped areas, while step 10 removes the dopant sources based on either wet or HF vapor technique. An abutted version of the separated junction flow described in Table 14 skips/removes Steps 3 and 4 to create abutted junctions.
In a variation the flow of Table 14 the sequence of BSG2 (Step 6) and phosphorous dopant paste (Step 8) is reversed. Base contact is opened first, followed by phosphorous paste. This is in turn followed emitter contact and BSG2 deposition and the remaining flow is similar.
In another variation, the hybrid dopant sources are based on APCVD PSG and dopant paste boron such that the base contact is made with the APCVD deposited doped SiO2 film while the emitter contact is made using boron based dopant paste. This variation has further variations where the sequence of contact open and its accompanying dopant source has two possibilities.
Table 15 below is a front end process flow showing a variation of the hybrid approach of Table 14 where both dopant paste and doped dielectric films are used as a source of dopants for base and emitter under contact doping.
In a variation of Table 15 as compared to Table 14, both emitter and the base contacts are separated by APCVD-PSG and diffusion anneal. This is done to reduce the risk of dopant co-diffusion during diffusion anneal. Co-diffusion is a process when dopant source from base or emitter contact diffusion areas (phos or boron) from dopant paste (phos or boron) moves into other polarity (base or emitter) through gaseous phase. This process may avoided, for example, by putting a solid phase dopant sources (APCVD-PSG) on top of PSG and adding anneal before the next contact emitter contact open step—as shown in Table 15. In some cases, the paste is phosphorous and the base is opened first (for an n-type back contact cell) and in a variation the paste is the boron paste and the emitter is opened first.
A variation of the Table 15 process flow forms abutted junctions by skipping Steps 3 and 4 as shown in Table 16 below. As throughout this disclosure, the variations described in conjunction with Table 15 are equally applicable with the abutted junction flow.
In the variation of Table 15 and 16, the co-diffusion risk may be avoided by eliminating either APCVD-PSG or eliminating diffusion anneal.
Note, all the self-aligned process flows with their variations described so far are equally valid with an epitaxially grown thin film solar cell. A representative process flow which corresponds to the approach outlined in Table 12 (separated junction with dopant paste) is shown in Table 17 for an epitaxial thin film solar cell. Epitaxial flow may use the HF vapor approach to keep the flow mostly dry while the epitaxial absorber is still on the template. All the other embodiments with abutted and separate junctions with hybrid dopant sources or all APCVD dopant sources (shown for CZ wafers) are equally valid for epitaxial solar cells with the modified flow based on Table 16. The present application provides more detailed flows around other aspects of epitaxial formation. The self aligned attribute along with its manufacturing methods can be combined with any of the previously discussed variations of the epitaxial and CZ wafer based process flows.
The foregoing description of the exemplary embodiments is provided to enable any person skilled in the art to make or use the claimed subject matter. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without the use of the innovative faculty. Thus, the claimed subject matter is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
It is intended that all such additional systems, methods, features, and advantages that are included within this description be within the scope of the claims.
This application claims the benefit of U.S. provisional patent applications 61/920,271 filed Dec. 23, 2013 and 61/954,116 filed Feb. 26, 2014, all of which are hereby incorporated by reference in their entirety.
Number | Date | Country | |
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61920271 | Dec 2013 | US | |
61945116 | Feb 2014 | US |