Thermal energy storage and power generation systems and methods
US-10107268-B1 · Oct 23, 2018 · US
US11754346B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11754346-B2 |
| Application number | US-202117363541-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 30, 2021 |
| Priority date | Jan 7, 2019 |
| Publication date | Sep 12, 2023 |
| Grant date | Sep 12, 2023 |
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Systems and methods for energy storage and energy recovery are provided. An electrical-to-electrical energy storage system includes a thermochemical energy storage device, a blower, a compressor, a turbine, and an electrical generator. The TCES device includes a vessel, a porous bed, and a heater. The porous bed is disposed within an interior volume of the vessel. The porous bed comprises a reactive material. The reactive material is configured to release oxygen upon being heated to a reduction temperature, and generate heat when exposed to oxygen. The heater is in thermal contact with the reactive material. The blower is configured to remove oxygen from the interior volume. The compressor is configured to flow oxygen into the interior volume. The turbine is configured to receive a heated, oxygen-depleted gas from the interior volume. The generator is configured to be powered by the turbine to generate electricity.
Opening claim text (preview).
What is claimed is: 1. A thermochemical energy storage device comprising: a vessel defining an interior volume, the vessel including a first opening and a second opening; a porous bed disposed within the interior volume and being in fluid communication with the first opening and the second opening, the porous bed comprising a reactive material, the reactive material being configured to release oxygen upon being heated to a reduction temperature, and generate heat when exposed to oxygen; and a heater embedded within or in contact with the reactive material, and the heater being configured to heat the reactive material. 2. The device of claim 1 , wherein: the heater comprises at least 75% of a diameter of an interior volume of the shell; the heater comprises a serpentine or coil shape; and the reactive material comprises a metal oxide. 3. The device of claim 2 , wherein the metal oxide comprises a magnesium-manganese oxide. 4. The device of claim 1 , wherein: the reactive material is electrically conductive; and the porous bed comprises a plurality of particles comprising the reactive material, the plurality of particles defining an average size in a range of about 100 μm-8 mm. 5. The device of claim 1 , wherein the porous bed comprises a total porosity of less than or equal to about 70%. 6. The device of claim 1 , further comprising: insulation disposed between the porous bed and a shell of the vessel, the insulation being in thermal communication with the porous bed; the heater extending through the reactive material with ends electrically connected to an electricity source; and the heater withstands at least 1600° C. 7. The device of claim 6 , wherein the insulation comprises a first insulation layer and a second insulation layer, the first insulation layer being disposed between the shell and the second insulation layer, and the second insulation layer being disposed between the first insulation layer and the porous bed. 8. The device of claim 7 , wherein the first insulation layer comprises a plurality of refractory bricks, the refractory bricks comprising aluminum, calcium aluminate, zirconia, magnesium aluminate, a sub-combination thereof, or a combination thereof. 9. The device of claim 7 , wherein the second insulation layer comprises microporous alumina microporous silica, alumina, fibrous zirconia, microporous zirconia, a sub-combination thereof, or a combination thereof. 10. The device of claim 1 , further comprising a cooling system in thermal communication with the porous bed, the cooling system being configured to circulate a heat transfer fluid between the porous bed and a shell of the vessel. 11. The device of claim 1 , wherein the heater comprises a first pair of ceramic electrodes having the porous bed disposed therebetween and a second pair of ceramic electrodes having the first pair of ceramic electrodes and the porous bed disposed therebetween, the first and second pairs of electrodes having different characteristics from each other. 12. A thermochemical energy storage device comprising: a vessel defining an interior volume, the vessel including a first opening and a second opening; a porous bed disposed within the interior volume and being in fluid communication with the first opening and the second opening, the porous bed comprising a reactive material, the reactive material being configured to release oxygen upon being heated to a reduction temperature, and generate heat when exposed to oxygen; a heater configured to heat the reactive material; the heater comprising a first pair of ceramic electrodes having the porous bed disposed therebetween and a second pair of ceramic electrodes having the first pair of ceramic electrodes and the porous bed disposed therebetween; and the heater being configured for bulk resistive heating of the porous bed. 13. The device of claim 12 , wherein: the first pair of ceramic electrodes comprises a first ceramic material having a chemical formula La 1-x A x CrO 3 , where A is selected from the group consisting of Mg, Ca, Sr, Ba, or combinations thereof; and x ranges from 0-0.1; and the second pair of ceramic electrodes comprises a second ceramic material having a chemical formula B 1-y C y DO 3 , where B is selected from the group consisting of La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu, Al, Sc, Ti, Y, Zr, Hf, or combinations thereof; C is selected from the group consisting of Sr, Ba, or a combination thereof; D is selected from the group consisting of Co, Mn, Ni, Fe, or combinations thereof; and y ranges from about 0.3-0.6. 14. The device of claim 13 , wherein the first ceramic material comprises LaCrO 3 and the second ceramic material comprises La 0.7 Sr 0.3 CoO 3 . 15. An energy storage system comprising: a thermochemical energy storage device comprising a vessel defining an interior volume, a metal oxide redox material disposed within the interior volume, and a heater configured to receive electricity and heat the metal oxide redox material; the heater comprising a first pair of ceramic electrodes having the porous bed disposed therebetween and a second pair of ceramic electrodes having the first pair of ceramic electrodes and the porous bed disposed therebetween; a blower configured to remove a first gas from the interior volume; a compressor configured to provide a second gas to the interior volume; a turbine configured to receive a third gas from the interior volume; and a generator configured to be powered by the turbine to generate electricity. 16. The system of claim 15 , further comprising a bypass line having a variable control valve disposed thereon, the bypass line being fluidly connected to a first junction between the compressor and the thermochemical energy storage device, and a second junction between the thermochemical energy storage device and the turbine. 17. A method of storing electricity and recovering electricity, the method comprising: storing electricity by: (a) providing electricity to a heater, the heater being configured to heat a reactive material disposed within a vessel, the heater being embedded within or in contact with the reactive material, the heater comprises at least 75% of a diameter of an interior volume of the shell, and the reactive material being configured to release oxygen; and (b) removing at least a portion of the oxygen from the vessel; and recovering electricity by: (c) providing oxygen to the vessel, the oxygen chemically reacting with the reactive material to generate a heated, oxygen-depleted fluid; (d) removing the heated, oxygen-depleted gas from the vessel; (e) providing the heated, oxygen-depleted gas to a turbine; and (f) powering a generator with the turbine to generate electricity. 18. The method of claim 17 , wherein the removing is performed at an oxygen partial pressure ranging from about 0.01-0.1 bar. 19. The method of claim 17 , wherein (c) the providing oxygen comprises providing air to the vessel, and conducting electricity through the reactive material. 20. The method of claim 19 , wherein the providing air comprises providing air at a pressure ranging from about 20-25 bar and a temperature ranging from about 200-400° C. 21. The method of claim 17 , wherein the recovering electricity further comprises forming an admixture by admixing a bypass gas with the heated, oxygen-depleted gas after (d) and before (e), and (e) the providing the heated, oxygen-depleted gas to the turbine comprises providing the admixture to the
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