None.
This invention relates to thermoelectrically enhanced fuel cells.
In general, fuel cells are electrochemical devices in which the chemical energy of fuels is converted directly into electrical energy via electrochemical reactions. Considering the basic principle thereof, the fuel cells are adapted to produce electricity by oxidation of hydrogen obtained by modifying fossil fuels, such as petroleum or natural gas, or pure hydrogen. During the oxidation of hydrogen, heat and water vapor are generated as byproducts. There are different types of fuel cells such as phosphoric acid fuel cells, alkaline fuel cells, molten carbonate fuel cells, solid oxide fuel cells, and proton exchange membrane fuel cells.
However, fuel cells are associated with some significant drawbacks despite their high energy conversion efficiency. There exist substantial temperature gradients within solid oxide fuel cells and fuel cell stacks. There are opportunities for generating additional electricity by taking advantage of such temperature gradients.
There exists a need for a method of utilizing the waste heat or temperature gradient of a fuel cell.
A fuel cell system comprising an anode, an electrolyte supported by the anode, and a cathode supported by the electrolyte. A primary thermoelectric ceramic is in contact with the cathode positioned on the opposing side of the electrolyte. An optional secondary thermoelectric ceramic is in contact with the anode positioned on the opposite side of the electrolyte. In this embodiment air and fuel gas surround the fuel cell at a temperature lower than the operational internal temperature of the fuel cell and both the primary thermoelectric ceramic and the optional secondary thermoelectric ceramic are capable of converting the temperature difference between the fuel cell and both the air and the fuel gas into an additional output voltage and power.
A solid oxide fuel cell system comprising an anode, an electrolyte supported by the anode, and a cathode supported by the electrolyte. A primary thermoelectric ceramic p-type conductor is in contact with the cathode positioned on the opposing side of the electrolyte. A secondary thermoelectric ceramic n-type conductor is in contact with the anode positioned on the opposite side of the electrolyte. In this embodiment air and a fuel gas surround the fuel cell at a temperature lower than the operational internal temperature of the solid oxide fuel cell and both the primary thermoelectric ceramic and the optional secondary thermoelectric ceramic are capable of converting the temperature difference between the solid oxide fuel cell and both the air and the fuel gas into an additional output voltage and power.
A more complete understanding of the present invention and benefits thereof may be acquired by referring to the follow description taken in conjunction with the accompanying drawings in which:
Turning now to the detailed description of the preferred arrangement or arrangements of the present invention, it should be understood that the inventive features and concepts may be manifested in other arrangements and that the scope of the invention is not limited to the embodiments described or illustrated. The scope of the invention is intended only to be limited by the scope of the claims that follow.
Conventional fuel cells, such as polymer electrolyte membrane fuel cells, direct methanol fuel cells, alkaline fuel cells, phosphoric acid fuel cells, molten carbonate, solid oxide fuel cells, or reversible fuel cells, all create heat during operation.
The present embodiment describes a fuel cell system comprising an anode, an electrolyte supported by the anode, and a cathode supported by the electrolyte. A primary thermoelectric ceramic is in contact with the cathode positioned on the opposing side of the electrolyte. An optional secondary thermoelectric ceramic is in contact with the anode positioned on the opposite side of the electrolyte. In this embodiment an air and a fuel gas surround the fuel cell at a temperature lower than the operational internal temperature of the fuel cell and both the primary thermoelectric ceramic and the optional secondary thermoelectric ceramic are capable of converting the temperature difference between the fuel cell and both the air and the fuel gas into an additional output voltage.
The electrolyte 206 diffuses the oxygen ions from the cathode 202 to the anode 204. Examples of the electrolyte materials that can be used include yittria-stabilized zirconia, scandium-stabilized zirconia, gadolinium doped ceria, or lanthanum strontium magnesium gallate. Other more specific examples of electrolyte materials can be (ZrO2)0.92(Y2O3)0.08, Ce0.9Gd0.1O2, Ce0.9Sm0.2O2, La0.8Sr0.2Ga0.8Mg0.2O3, BaZr0.1Ce0.7Y0.1Yb0.1O3.
The anode 204 uses the oxygen ions to oxidize hydrogen (H2) from the input fuel (i.e., combine the hydrogen and the oxygen ions). Examples of anode material include mixtures of NiO, yttria-stabilized zirconia, gadolinium-doped ceria, CuO, CoO and FeO. Other more specific examples of anode materials can be a mixture of 50 wt. % NiO and 50 wt. % yttria-stabilized zirconia or a mixture of 50 wt. % NiO and 50 wt. % gadolinium-doped ceria.
The oxidation of the hydrogen forms water (H2O) and free electrons (e−). The water exits the anode 204 with any excess fuel. The free electrons can travel through a circuit (shown dashed with a load 208) between the anode 204 and the cathode 202. A primary thermoelectric ceramic 210 is shown in contact with the cathode positioned on the opposing side of the electrolyte. It is envisioned that the primary thermoelectric ceramic should have good thermoelectric properties, the materials should have high values of Seebeck coefficients (ΔV/ΔT), high electrical conductivities, and low thermal conductivities. Additionally, the primary thermoelectric ceramic should be a p-type conductor and stable in oxygen at fuel cell operating temperatures. Examples of the primary thermoelectric ceramic include: La0.9Sr0.1FeO3, LaCoO3, La0.8Sr0.2CoO3, LaCo0.2Fe0.8O3, La0.8Sr0.2Co0.2Fe0.8, La0.7Ca0.3CrO3, LaFe0.7Ni0.3O3, Ca2.5Tb0.5Co4O9, Ca3Co4O9, Ca2Co2O5, Ca3Co2O6, Ca3Co3O9, Ca2.9Nd0.1Co4O9, CaCo3.9Cu0.1O9, CaMnO3, Ca2.9Nd0.1MnO3, SrTiO3, Si0.7Ge0.22, Ca0.9Yb0.1MnO3, Ca2.7Bi0.3Co4O9, Na2Co2O4, SrTi0.9Ta0.1O3, Sr0.925La0.15TiO3, Sr0.9Dy0.1TiO3.
When combined with other fuel cells 200 within a fuel cell stack, the power generation capabilities of all of the solid oxide fuel cells 200 can be combined to output more power.
In yet another embodiment, the fuel cell system can describe a solid oxide fuel system wherein the solid oxide fuel cell system comprises an anode, an electrolyte supported by the anode, and a cathode supported by the electrolyte. A primary thermoelectric ceramic p-type conductor is in contact with the cathode positioned on the opposing side of the electrolyte. A secondary thermoelectric ceramic n-type conductor is in contact with the anode positioned on the opposite side of the electrolyte. In this embodiment an air and a fuel gas surround the fuel cell at a temperature lower than the operational internal temperature of the solid oxide fuel cell and both the primary thermoelectric ceramic and the optional secondary thermoelectric ceramic are capable of converting the temperature difference between the solid oxide fuel cell and both the air and the fuel gas into an additional output voltage.
When combined with other fuel cells 300 within a fuel cell stack, the power generation capabilities of all of the solid oxide fuel cells 300 can be combined to output more power.
The additional output voltage from the primary thermoelectric ceramic and the secondary thermoelectric ceramic would be partially dependent upon the temperature difference between the operation internal temperature of the fuel cell and the temperature of both the air and the fuel gas. While not limited to this range it is anticipated that the additional output voltage would range from about 5 mV to about 150 mV. It is also envisioned that the temperature difference between the operation internal temperature of the fuel cell and the temperature of the air and fuel gas mixture range from about 5° C. to about 250° C.
The thickness of the primary thermoelectric ceramic and the secondary thermoelectric ceramic independently range from about 30 μm to about 5 mm.
The following examples of certain embodiments of the invention are given. Each example is provided by way of explanation of the invention, one of many embodiments of the invention, and the following examples should not be read to limit, or define, the scope of the invention.
La0.9Sr0.1FeO3 was tested as a thermoelectric material. One end of a 20 mm long bar was held in a furnace with a set temperature of 700° C. while the other end was cooled with ambient air to create a temperature gradient. The results of the temperature gradient are shown in
La0.9Sr0.1FeO3 was added to a fuel cell (the fuel cell has a 30 μm La0.6Sr0.4Co0.2Fe0.8O3—Ce0.9Gd0.1O2 cathode, a 10 μm (ZrO2)0.92(Y2O3)0.8 electrolyte, and a 300 μm NiO—(ZrO2)0.92(Y2O3)0.08 anode with ceramic contact paste. The fuel cell was kept at 700° C. while the top end of the La0.9Sr0.1FeO3 bar cooled to 550° C. by blowing ambient air. The fuel cell showed an open circuit voltage of 1.066 V while the voltage measured at the end of the La0.9Sr0.1FeO3 bar was 1.119V, an improvement of 53 mV. These voltages are shown in
La0.9Sr0.1FeO3 was added to a fuel cell (the fuel cell has a 30 μm Sm0.5Sr0.5CoO3—Ce0.9Gd0.1O2 cathode, a 10 μm (ZrO2)0.92(Y2O3)0.08 electrolyte, and a 300 μm NiO—(ZrO2)0.92(Y2O3)0.08 anode) with ceramic contact paste. The fuel cell was kept at 700° C. while the top end of the La0.9Sr0.1FeO3 bar cooled to 480° C. by blowing ambient air. The fuel cell showed an open circuit voltage of 1.09V while the voltage measured at the end of the La0.9Sr0.1FeO3 bar was 1.18V, an improvement of 90 mV. The voltages are shown in
A p-type thermoelectric ceramic, Ca2.9Nb0.1Co4O9 was developed. The material has a perovskite structure as shown in its X-ray diffraction pattern (
In closing, it should be noted that the discussion of any reference is not an admission that it is prior art to the present invention, especially any reference that may have a publication date after the priority date of this application. At the same time, each and every claim below is hereby incorporated into this detailed description or specification as an additional embodiment of the present invention.
Although the systems and processes described herein have been described in detail, it should be understood that various changes, substitutions, and alterations can be made without departing from the spirit and scope of the invention as defined by the following claims. Those skilled in the art may be able to study the preferred embodiments and identify other ways to practice the invention that are not exactly as described herein. It is the intent of the inventors that variations and equivalents of the invention are within the scope of the claims while the description, abstract and drawings are not to be used to limit the scope of the invention. The invention is specifically intended to be as broad as the claims below and their equivalents.
This application is a non-provisional application which claims the benefit of and priority to U.S. Provisional Application Ser. No. 62/752,581 filed Oct. 30, 2018, titled “Thermoelectrically Enhanced Fuel Cells,” which is hereby incorporated by reference in its entirety.
Number | Date | Country | |
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62752581 | Oct 2018 | US |