World wide demand for petroleum is increasing. It would be desirable to provide alternative energy technologies.
For example, it would be desirable to provide improved solar cell technology, particularly where the technology is based on relatively low cost manufacturing techniques.
It would further be desirable to provide improved energy harvesting techniques, to extract energy from waste heat.
This application specifically incorporates by reference the disclosures and drawings of each patent application identified above as a related application.
A first aspect of the concepts disclosed herein is directed to an improved dye-sensitized solar cell (DSSC).
In a first exemplary embodiment, a photo energy conversion efficiency (PCE) of a DSSC is increased by employing a substantially transparent electrolyte, a substantially transparent substrate supporting the electrolyte, and a reflective layer disposed underneath the DSSC device to direct light that would otherwise be wasted, back into the DSSC device.
In a second embodiment, the PCE of a DSSC is increased by adding an additional dye, which exhibits significant absorption in the red and near infra-red (IR) regions. A novel phthalocyanine derivative has been developed, which absorbs well in the red and near IR-regions, and which readily couples to the titanium oxide semiconductor in the DSSC, thus enabling the DSSC device to exhibit a high photo-current efficiency.
A second aspect of the concepts disclosed herein is the identification of thermal electric materials, including Mg2Si, which can be used to harvest energy from waste heat in a variety of environments.
This Summary has been provided to introduce a few concepts in a simplified form that are further described in detail below in the Description. However, this Summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
Various aspects and attendant advantages of one or more exemplary embodiments and modifications thereto will become more readily appreciated as the same becomes better understood by reference to the following detailed description, when taken in conjunction with the accompanying drawings, wherein:
Exemplary embodiments are illustrated in referenced Figures of the drawings. It is intended that the embodiments and Figures disclosed herein are to be considered illustrative rather than restrictive. No limitation on the scope of the technology and of the claims that follow is to be imputed to the examples shown in the drawings and discussed herein.
Some of the Figures schematically illustrate exemplary DSSCs, enabling different layers of the DSSCs to be visualized. It should be recognized that the relative dimensions of each layer are not intended to be limiting, and the concepts disclosed herein encompass DSSCs having similar layers of different relative dimensions.
Disclosed herein are several improved DSSCs, which employ either rigid transparent substrates (such as glass) or flexible transparent substrates (such as polymers). An exemplary flexible substrate is a platinum-coated PET film, which can be employed as a counter electrode. Other useful transparent conductive flexible substrates include polymers coated with an indium tin oxide (ITO) layer. While ITO represents an exemplary conductive coating, it should be recognized that other conductive coatings can be employed. In many embodiments, generally transparent coatings are preferred; however, it should be understood that in some embodiments, an opaque bottom counter electrode is acceptable, if a reflective layer will not be disposed below the bottom counter electrode.
In empirical studies, PCEs of about 6% were observed for the improved DSSC devices disclosed herein. If one calculates the PCE/weight, one can define the specific energy conversion efficiency (SECE) of a DSSC. The SECE of higher density devices will be lower than the SECE of lower density devices. The SECE of empirical glass-based DSSC devices disclosed herein was determined to be about 66% (cm2/g), while the SECE of the empirical flexible substrate DSSC devices disclosed herein was determined to be about 660% (cm2/g). Clearly, the flexible DSSC devices offer advantages in applications where the weight penalty is high, such as an airplane or spacecraft. Thus, one aspect of the concepts disclosed herein is the incorporation of the improved DSSC devices based on transparent flexible substrates into an airplane, a remotely piloted vehicle (RPV), an unmanned aerial vehicle (UAV), or a spacecraft.
Inorganic-based solar cells generally exhibit a relatively good conversion efficiency, but they are generally expensive, difficult to manufacture, heavy and bulky, utilize toxic materials, and have limited scalability due to their lack of a large flexible area. The conversion efficiency of prior art dye-sensitized solar cells (DSSC) is still relatively low. However, DSSCs are relatively low-cost, light weight, employ relatively less toxic materials, and are more readily scalable.
Conventional DSSCs include five major parts, a nano crystalline titanium oxide (TiO2) semiconductor film, a dye sensitizer, a redox electrolyte, a counter electrode (generally platinum (Pt)), and a transparent conductive substrate.
Photons pass through transparent conductive substrate 12 and enter the working layer. Some photons encounter molecules of the dye sensitizer, exciting these molecules and causing the excited molecules to eject an electron. The ejected electrons dissipate through the working layer into the transparent conductive substrate 12. The electrolyte layer provides replacement electrons to the previously excited molecules of the dye sensitizer, and the counter electrode acquires replacement electrons from transparent conductive substrate 12 via conductor 24. The lower counter electrode layer does not need to be transparent.
The exemplary improved DSSC devices disclosed herein include one or more of the following elements: (1) a transparent counter electrode layer coupled to a reflective surface, enabling photons that pass through the DSSC to be reflected back into the DSSC to excite additional dye molecules; (2) a coating for the upper transparent conductive substrate to enable the DSSC to capture oblique rays of light, which otherwise would be reflected off the upper transparent conductive substrate (and not pass through the transparent conductive substrate); (3) the use of flexible transparent conductive substrates (for the upper electrode and the lower counter electrode) to enable the DSSC to conform to surfaces; (4) the use of an additional dye sensitizer that interacts with IR and red light, and an additional electrode; and, (5) the use of an electrolyte that remains functional at relatively low temperatures. It should be understood that the novel concepts disclosed herein encompass DSSC embodiments that include any combination and permutation of the above elements, including embodiments implementing only one of the above elements.
DSSC 30 also includes working layer 14, comprising the plurality of titanium oxide (TiO2) semiconductor particles 16 coated with molecules 18 of the dye sensitizer. An electrolyte layer 20a is not based on the conventional iodine/tri-iodide electrolyte, but instead, employs an electrolyte material that remains functional at relatively low temperatures, so that the DSSC can be used in a wide range of environmental conditions. As noted above, one aspect of the concepts disclosed herein is to provide DSSCs that can be used in aviation applications, and temperatures at higher altitudes can drop as low as −50 degrees F.
Referring once again to
With respect to the dye sensitizer, ruthenium-based dyes are conventionally employed, and such dyes can harvest the photon energy for the visible light region. The PCE of such a device can be significantly increased (to more than 10%) by employing the upper anti-scattering or anti-reflecting layer, and the lower reflecting layer of DSSC 30, to increase the number of photons entering the device.
Note that DSSC 30 of
Referring to
The flexible DSSC device of
As noted above, a significant drawback of ruthenium-based sensitizers is their lack of absorption in the red region of the visible spectrum. Phthalocyanine dyes exhibit intense absorption in the red and near-IR regions. Another aspect of the concepts disclosed herein are novel phthalocyanine derivatives, which have absorption in the red and near-IR regions and which couple well to TiO2. The incident photon-to-photon current efficiency (IPCE) of an empirical DSSC specimen using the phthalocyanine derivative as a sensitizer is 51% at 690 nm, as shown in
As noted above, ruthenium-based sensitizer dyes work well for part of the visible light range, and the novel phthalocyanine derivatives disclosed herein work well with red and near-IR light. Unfortunately, if both dyes are incorporated into a single TiO2-based working layer, charge interactions between the dyes actually reduce the effectiveness of the DSSC. While the phthalocyanine derivatives disclosed herein can be used alone (i.e., without the conventional ruthenium dyes), a DSSC including only the phthalocyanine derivatives would not make use of photons outside of the red and near-IR range.
Referring to
DSSC 50 includes both a working layer with TiO2 and a ruthenium-based dye, and a working layer with TiO2 and a phthalocyanine-based dye. As shown in
An electrolyte layer 20 is disposed immediately adjacent to each working layer, to provide a source of electrons to replace electrons displaced from the dye sensitizer by interaction with photons. In some embodiments, the different electrolyte layers employ the same electrolyte. In other embodiments, a first electrolyte (optimized for interacting with the ruthenium working layer) is used with ruthenium working layer 14, and a second electrolyte (optimized for interacting with the phthalocyanine working layer) is used with phthalocyanine working layer 14a. Note that the second working layer from the top is disposed below the first electrolyte layer, so that the first electrolyte needs to be generally transparent (at least with respect to photons needed to interact with the dye in the second working layer). The second working layer needs to be generally transparent where reflective layer 34 is employed.
An additional transparent electrode 23 is disposed between the two different working layers. Again, the transparent electrode can employ a rigid substrate, or a flexible substrate, generally as discussed above. Finally, generally as discussed above, conductor 24 couples the upper transparent electrode with the lower counter electrode.
Thermoelectric Materials for Harvesting Energy from Waste Heat
Another aspect of the concepts disclosed herein is a set of new thermoelectric (TE) materials, each exhibiting a relatively high specific figure of merit (ZT/density). These materials include Mg2Si, Mg2Si—Ge, Mg2Si—Bi, SiGe and their doped derivatives. TE modules based on these materials have been designed, and the module efficiencies predicted, based on various geometries. In the study, the objective function of a TE module was proposed, based on the specific figure of merit, the Clarke number, and the p- and n-pillar aspect ratio. For example, to achieve a larger load resistance, it is advantageous to employ as many pairs of p- and n-type TE pillars as practical.
Thermoelectric materials and TE modules are equally important as thermal energy harvesters for human carried equipment, equipment embedded in the human body (i.e., pacemakers, medical devices), and vehicles. For example, future air vehicles may incorporate TE modules for energy harvesting and cooling, in locations such as the leading edge of wings of a reentry vehicle, high power equipment such as radar and antennas, and engine exhaust.
Among the TE materials so far studied, the Mg2Si system was found to have the highest specific figure of merit (i.e., ZT/weight of TE), for a typical use high temperature of 800 deg. K., as shown in Table 1 (which also provides the average Clarke number, indicating how abundant the material is on earth, based on the relative percentage of all elements; thus, the higher the Clarke number, the more abundant those elements are on earth, and more abundant materials are more likely to be available at a lower cost). In view of its specific ZT and higher Clark number, the Mg2Si TE system appears to be the most favorable TE material.
Current efforts are focused on designing TE modules based on Mg2Si—Bi doped (n-type) and Mg2Si—Ag doped (p-type). These designs consider the relative number of p- and n-type pillars, and the aspect ratio of the pillars, for a given set of boundary conditions (high temperature, low temperature, available surface area, etc.).
Among the TE materials listed in Table 2, Mg2Si compounds and their derivatives (doped with Bi, and so on) with high specific ZT values were produced. SiGe TE materials, whose specific ZT values increase under higher use temperatures (up to 1000° C.), were also developed. The TE materials so developed were prepared as mechanical alloys (MA), followed by spark plasma sintering (SPS), from which n- and p-type TE specimens were removed for measurements of their TE properties (thermal conductivity, electrical conductivity and Seebeck coefficient as a function of RT—800° K).
The study also developed the concept of a nano composite based on single crystal SiGe, where nano-holes are formed into which another metal, such as Ge, is inserted, thereby forming a nano composite whose thermal conductivity is lowered, thus increasing the material's figure of merit value (ZT, which contains thermal conductivity in the denominator).
Although the concepts disclosed herein have been described in connection with the preferred form of practicing them and modifications thereto, those of ordinary skill in the art will understand that many other modifications can be made thereto within the scope of the claims that follow. Accordingly, it is not intended that the scope of these concepts in any way be limited by the above description, but instead be determined entirely by reference to the claims that follow.
This application is based on a prior copending provisional application Ser. No. 61/085,732, filed on Aug. 1, 2008, the benefit of the filing data of which is hereby claimed under 35 U.S.C. §119(e).
This invention was made with U.S. government support under Grant No. FA 9550-06-01-0326 awarded by the Air Force Office of Scientific Research (AFOSR). The U.S. government has certain rights in the invention.
Number | Date | Country | |
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61085732 | Aug 2008 | US |