1. Field of the Invention
This invention generally relates to solar generated power and, more particularly, to an easily fabricated flat panel system that combines the advantages of silicon photovoltaic cells with concentrated (Group III-V) photovoltaic solar cells.
2. Description of the Related Art
The solar photovoltaic (PV) industry is dominated by conventional, “1-sun” silicon PV cells. The most efficient are made of single crystalline silicon (c-Si), with the highest performing cells at the time of this writing of around 25% efficient, and best panels at about 21% (e.g., SunPower@). However, the fundamental thermodynamic limit for Si is 29%. In contrast, concentrated III-V solar cells (CPV) have demonstrated record cell efficiencies of 46%, still far below their thermodynamic limits. However, “1-sun” c-Si PV can capture both direct and diffuse sunlight, while CPV requires high optical concentrations of 400-1000× (due to the high cost of the III-V cells), and so collect only direct sunlight. Furthermore, CPV systems require accurate two-axis tracking to continually point their optics towards the sun. CPV module efficiencies of 35% or more have been achieved (e.g., Semprius), but are only applicable to areas with very high direct sunlight.
If, for example, a 30% efficient CPV system is deployed in a geographic area with a higher diffuse component, say 40%, only 0.3×(1−0.4)=18% of the total sunlight is collected. This is less than a cheaper c-Si system that can collect 21% of the sunlight, both direct and diffuse. Furthermore, on a partly-cloudy day the power generation of the CPV system would go from maximum to almost nothing in a few seconds when a cloud crosses the sun, putting strain on the electrical grid. If diffuse sunlight could also be collected, the decrease would be much less. Furthermore, the optical systems and 2-axis trackers for CPV systems have tended to be very large and bulky, requiring expensive, massive support structures, further limiting their market potential.
There is a need for CPV systems that can collect both direct and diffuse light, to enable greater than 30% total efficiency in geographic areas and markets with more than 25% diffuse sunlight. There is a need for compact and light systems, to reduce mechanical constraints and balance of system (BOS) costs, and to expand into more potential markets.
There have been a wide variety of systems devised to make CPV more compact, but few which enable collection of both direct and diffuse sunlight. One approach uses lenslet arrays to couple light into a waveguide, with CPV cells mounted on the side of the waveguide. However, for most of these systems it is difficult to also incorporate the collection of diffuse sunlight. A recent review of tracking-integrated schemes is given in Reference [1]. Some of the approaches described in this reference include lenslet arrays and planar lightguides with lateral motion. Much of the analysis discussed below is from Reference [1].
There exist a number of other designs for coupling of light focused by a lenslet array into a planar waveguide. These use a light-induced material property change to passively track the sun over a limited angular range [6-11].
FIG. 3 is a schematic depicting a hybrid CPV/PV architecture (prior art). Recently, there have been efforts to collect both direct and diffuse sunlight [12, 13]. These efforts involve integrating 2D arrays of lenslets which concentrate direct sunlight onto III-V CPV cells placed on a backplane made up of conventional cells like Si or thin-films. These latter cells collect the diffuse sunlight.
It would be advantageous if a hybrid solar system combining 1-sun silicon PV cells with CPV solar cells could be optimized for use with 2-axis tracking.
The following articles and patent applications are incorporated herein by reference:
Disclosed herein is the integration of high efficiency concentrating photovoltaic cells (CPV) with conventional 1-sun solar panels (thin film or c-Si) to capture both direct and diffuse sunlight, particularly, in low direct normal insolation (DNI) regions. In addition, a lower-cost version with no integrated 1-sun cells is disclosed that is more applicable to high DNI regions. An array of lenses captures and concentrates direct sunlight to a line focus and then couples it into a horizontal waveguide. The waveguide further concentrates direct sunlight onto high performance III-V CPV cells that are mounted on an underlying 1-sun panel, which collects diffuse sunlight. In one variation, the entire assembly is mounted on a 2-axis tracker for optimum collection of sunlight throughout the day and year. Initial optical analysis indicates that greater than 30% total efficiency can be achieved in a thin, flat form factor. Furthermore, mass production analogous to that of current liquid crystal display (LCD) panel fabrication can be expected to drive costs down, thus satisfying the overall objective of large-scale expansion of the market for an entirely new class of micro-scale CPV solar panels.
Advantageously, the system may use cylindric, acylindric, or Fresnel lenses instead of a 2D array of lenslets to minimize the loss or “dead space” where lenses meet. Unlike the conventional designs described in the Background Section, the CPV cells are mounted on a flat substrate instead of the edge of the waveguide, so they are much easier to manufacture. The entire design involves parallel sheets of: lenses, waveguides, and PV/CPV cells. The CPV cell array may be placed atop a 1-sun panel cell for monolithic integration and excellent heat dissipation. Diffuse sunlight is collected, as well as direct sunlight, as the waveguide only occupies a portion of the surface area, increasing the collection of diffuse light.
Accordingly, a flat panel photovoltaic (PV) system is provided formed from a first sheet with a first row of concentrated III-V photovoltaic solar cells, where each CPV solar cell has an optical input and an electrical output. A second sheet overlies the first sheet and is made up of a first row of waveguides. Each waveguide has an optical input and optical output aperture coupled to a corresponding CPV solar cell optical input. A third sheet includes a one-piece linear lens overlying the first row of waveguides, having a focal line coupled to the optical input aperture of each waveguide in the first row. In one aspect, a fourth sheet underlies the first sheet, which is a 1-sun solar panel including a plurality of silicon PV cells. Note: when silicon PV cells are used in the system, the CPV cells may be formed on top of the 1-sun solar panel, so that the entire system is made up of a 3-sheet stack. However, for greater clarity, this discussion assumes that the first and fourth sheets are separate.
The second sheet may also include a first mirror configured to redirect light from the focal line of the one-piece linear lens towards the optical output aperture of each waveguide in the first row of waveguides. Since the waveguides are transparent their optical input apertures may be formed in planar top surfaces, with the first mirror positioned at a (−α) degree angle with respect to the planar top surface, where (α) is in the range of 30 to 60 degrees. Typically, each waveguide has an optical output aperture formed in a planar bottom surface. A plurality of second mirrors is configured to redirect light from the first mirror to the waveguide optical output, and is positioned at an angle of (−λ) degrees with respect to the planar top surface, where λ is in a range of 30 to 60 degrees.
In one variation, the second sheet further includes a second row of waveguides, with each waveguide in the second row having an optical output aperture coupled to a corresponding CPV cell in the first row of CPV cells. That is, each CPV cell collects radiation from one waveguide in the first row of waveguides and one waveguide in the second row of waveguides. Then, a first one-piece linear lens overlies the first row of waveguides, a second one-piece linear lens overlies the second row of waveguides, and intersection of the first and second one-piece linear lenses overlies the first row of CPV cells. Typically, such a system is made up of a plurality of CPV solar cell rows. If the first row of waveguides and second row of waveguides are defined as a first waveguide assembly, then the second sheet further includes a plurality of waveguide assemblies, each waveguide assembly associated with a corresponding CPV solar cell row.
In another variation, the second sheet further includes a second row of waveguides, where each waveguide in the second row is adjacent to a corresponding waveguide in the first row of waveguides, with an optical output aperture coupled to an optical input aperture of the corresponding waveguide. Alternatively stated, the two waveguides can be considered a single waveguide of two sections with two optical input apertures and a single optical output aperture coupled to a corresponding CPV cell in the first row of CPV cells. Then, a one-piece linear lens overlies each corresponding row (section) of waveguides, with a focal line coupled to the optical input of each waveguide in the corresponding row of waveguides.
Additional details of the above-described system are presented below.
c are partial cross-sectional views of a flat panel photovoltaic (PV) system.
c are partial cross-sectional views of a flat panel photovoltaic (PV) system. In
A second sheet 510 overlies the first sheet 502 and comprises a first row 512 of waveguides 514. Each waveguide 514 has an optical input 516, and optical output 518 coupled to a corresponding CPV solar cell optical input 508. A third sheet 520 overlies the second sheet 510 and comprises a one-piece linear lens 522 overlying the first row 512 of waveguides. A focal line 524 (shown as a “dot” coming out of the page) is coupled to the optical input 516 of each waveguide 514 in the first row. Edge rays 525 are shown for reference. Typically, the system 500 may comprise a plurality of CPV rows and a plurality of waveguide rows associated with a one-piece linear lens 522. Therefore, CPV row 534 and waveguide row 536 are also shown. The one-piece linear lens 522 may be cylindric, acylindric, or a Fresnel lens, with an f-number in the range of F/0.5 to F/5, where an f-number is the ratio of focal length to lens aperture (i.e., lens width). Typically, an acylindric lens would be associated with the lower range of f-numbers and a cylindric lens would be associated with the higher range. There is significantly less boundary region associated with a linear lens, as opposed to a lenslet array of many 2D lenses, which reduces the amount of “dead space” (undefined light propagation) between lenses.
Referring to
In
The third sheet comprises a plurality of adjacent one-piece linear lenses 522 (only one lens is shown for greater clarity). Each one-piece linear lens 522 has a first width 700. Adjacent rows of waveguides 514 in the second sheet are separated by a distance equal to the first width (see
As can be seen in
In the third sheet, a first one-piece linear lens 522a overlies the first row of waveguides 512a, a second one-piece linear lens 522b overlies the second row of waveguides 512b, and the intersection 800 of the first and second one-piece linear lenses 522a/522b overlies the first row of CPV cells 504. Note, although not explicitly shown, the system 500 of
As shown, the system may comprise a plurality of CPV solar cell rows. If the first row of waveguides 512a and second row of waveguides 512b form a first waveguide assembly, then the second sheet further comprises a plurality of waveguide assemblies, each waveguide assembly associated with a corresponding CPV solar cell row. If the one-piece linear lens (e.g., 522a) has a lens first width 700, then adjacent waveguide assemblies in the second sheet are separated by a distance 802 equal to the first width 700. Further, each waveguide 514 has a waveguide first length 702, between the optical input and optical output (see
Alternatively stated, the first and second rows of coupled waveguides 512a may be fabricated or conceptually considered as a first row of waveguides 900, where each waveguide has a first optical input aperture, a second optical input aperture, and an optical output aperture (see
A second mirror 1008 is configured to redirect light from the second focal line 524b of the second one-piece linear lens towards the optical output 1004 of each waveguide in the first row of waveguides, via transparent section 1012. The second mirror is positioned at a −(Φ) degree angle with respect to the planar top surface, and where (Φ) is in a range of 30 to 60 degrees. Again it is assumed that the planar top surface and CPV optical input are in the same (horizontal) plane. If they are not, the angles described above may include an additional adjustment to account for any offset. As described above, the first and second mirrors 1006/1008 may be discrete pieces associated with each waveguide, or single pieces associated with an entire row of waveguides. A plurality of third mirrors 1010 may be associated with a row of waveguides (one is shown in profile). Each third mirror 1010 is positioned at a −(λ) degree angle and configured to redirect light through the waveguide optical output aperture 1004 to the CPV cell 506 optical input 508.
The system of
Returning to
A detailed loss and power model has been formulated and is summarized below. The major loss mechanisms are: Loss#1 and #2: the top lens plate, which even antireflective (AR) coated, induces 2% loss (1% for each surface). These losses occur for both direct and diffuse illumination.
Loss#3: For DNI light loss occurs when focused light is coupled into the waveguide; however, an optimized AR coating at the aperture can reduce this to 1%.
Loss#4: DNI light is reflected laterally by a silvered surface, which induces an additional 4% loss.
Loss#5: Likewise, there is a 4% loss upon exit of light from the waveguide to illuminate the CPV cells.
Loss#6: For diffuse light, there is transmission loss upon passing through the waveguides (even though they are transparent). This loss is 4% at entry and exit surfaces (8% total) although waveguides occupy only one quarter of the total area in some variations of the waveguide design. However, these losses could be reduced by coating of the waveguides.
Loss#7: Another diffuse loss is simply due to shadowing by silvered surfaces, which is about 5% of total 1-sun panel area.
Loss#8: Diffuse light at low angles becomes trapped in the acylindric lens by total internal reflection (TIR) with a collateral loss of about 21% for the worst-case scenario of a uniformly illuminated sky, as may occur on a day with thick clouds. Equivalent TIR loss in a Fresnel lens is only about 11%. For both acylindric and Fresnel lenses, the linear design of the top lens is subject to a lower loss than conventional pixelated 2D lenslet arrays.
This loss mechanism involves the trapping of diffuse light inside the cylindrical lens array from TIR. There is little loss within +/−20° of the normal direction to the lenses, but loss increases beyond that. Loss is less for diffuse light incident in the axial plane of the lenses (along the long direction of the cylinders), and more in the transverse plane. The simulations are for F/1 optics. These losses can be reduced with slower optics (i.e., a larger F/#). The amount of this loss depends on the character of the diffuse light. If the sun can be seen through high clouds, most of the light is within +/−20° and can be collected. If the sun cannot be seen at all due to thick clouds, this loss is high. However, in this latter case there is very little sunlight to be collected, so the absolute loss is not large.
TIR losses were further investigated by comparing linear arrays of acylindric lenses, unique to the systems described herein, and a conventional 2D lenslet arrays. These simulations are for F/1 and F/2 acylindric optics, but losses can be further reduced by using Fresnel lenses. Several assumptions were used in the simulations:
1) Worst-case scenario for diffuse sunlight: a diffuse sky which is uniformly bright.
2) Fresnel reflection and absorption losses are not included.
3) Only the geometric losses are calculated from TIR.
Transmission integrated over all incident angles is summarized for these four cases in the following table.
It can be seen qualitatively that F/2 optics have a higher transmission than F/1 optics. It is further evident that a linear array of acylinder lenses is superior to a 2D array of lenslets in both cases. Nevertheless, worst-case, it is found that ˜20% of diffuse light is trapped inside a F/1 acylinder lens array. Even so, further simulations reveal that this can be reduced by about half using a linear array of Fresnel lenses, instead of acylinders.
Considering all these losses, a total optical efficiency for DNI light of 87.6% and for diffuse light of ˜85% is achievable. Therefore, the efficiency for AM1.5G (1000 W/m−2) depends on both PV cell efficiency and the diffuse/direct fraction. Current state-of-the-art III-V cell efficiency is about 46% at 1000×. Therefore, a CPV cell with efficiency between 40% and 44% is a reasonable. Likewise, current c-Si panel efficiencies are 21%.
As always in solar power, achieving the lowest possible cost is of the highest importance. To enable a low cost, the modular assembly strategy presented herein substantially resembles manufacturing methods currently in use for production of LCD panels in which two layers of glass carrying complicated electrical and optical components are registered and assembled with high accuracy. Such methods enable long-inventors: term cost savings by improvement of manufacturing efficiency and economy-of-scale. Alternatively, in high DNI regions the 1-sun panels need not be included to achieve proposed system efficiency. In this case, long-term cost is reduced even further.
A flat panel PV system has been provided to effectively capture both high and low DNI. Examples of particular subcomponents and components layouts have been presented to illustrate the invention. However, the invention is not limited to merely these examples. Other variations and embodiments of the invention will occur to those skilled in the art.
The application is a Continuation-in-part of an application entitled, SOLAR CONCENTRATOR WITH ASYMMETRIC TRACKING-INTEGRATED OPTICS, invented by Wheelwright et al., Ser. No. 14/577,842, filed Dec. 19, 2014, Attorney Docket No. SLA3462; which is a Continuation-in-part of an application entitled, HYBRID TROUGH SOLAR POWER SYSTEM USING PHOTOVOLTAIC TWO-STAGE LIGHT CONCENTRATION, invented by Wheelwright et al., Ser. No. 14/503,822, filed Oct. 1, 2014, Attorney Docket No. SLA3454. Both applications are incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 14577842 | Dec 2014 | US |
| Child | 14825240 | US | |
| Parent | 14503822 | Oct 2014 | US |
| Child | 14577842 | US |