Production of liquid hydrocarbon fuels from hydrogen and carbon monoxide produced in a solid oxide electrolyzer by thermally integrating the electrolyzer with liquid fuel production process.
The increase in global atmospheric carbon dioxide concentrations has been linked to changes in the earth's climate. The combustion of fossil fuels in various engines produces atmospheric carbon dioxide. Concerns about climate change have led to significant societal changes toward renewable or low carbon electricity. This has also led to increasing activity to decarbonize the transport sector of the economy. As a result, we see increases in the use of electric vehicles that are powered by renewable electricity to aid in decarbonization of the transport sector. Heavy transport and aviation are some of the most carbon intensive transportation sectors. Efficient and economical production of low carbon fuels, diesel and sustainable aviation fuel, could lead to significant reductions in the carbon dioxide emissions by the heavy transport and the aviation sectors.
Production of fuels from low carbon electricity and from carbon dioxide by the use of a solid oxide electrolysis cell (SOEC) is demonstrated.
Several previous patent applications deal with the production of fuels and chemicals from carbon dioxide and low carbon fuel including U.S. patent application Ser. No. 17/300,259, U.S. patent application Ser. No. 17/300,260, U.S. patent application Ser. No. 17/300,262, and U.S. patent application Ser. No. 16/873,561. Each application is incorporated by reference in its entirety. However, each of these applications does not deal specifically with the integration process with a Solid Oxide Electrolyzer (SOE).
Cinti et al (Ref. 1) deals with an integration of fuels production with an SOEC but without the thermal integration process and the associated improvement in efficiency shown in this patent application.
In the SOEC, water is split into hydrogen and oxygen ions at the cathode. The oxygen ions diffuse across a ceramic membrane, and oxygen is produced at the anode by combination of oxygen ions using heat and electrochemical gradients as driving force. See equation 1 below. When carbon dioxide is also supplied, co-electrolysis takes place, and the carbon dioxide is reduced and produces carbon monoxide at the cathode and oxygen at the anode. See equation 2 below.
ΔH0 is the energy (enthalpy) necessary for the reaction(s) at standard temperature of 25° C. Both reactions are endothermic and require the addition of energy to be completed. ΔH is adjusted for the operating temperature of the SOEC. It should be noted that Eq. 1 is for gaseous water or steam as the feedstock. If the water is in the liquid state, then ΔH0=285.84 kJ/mol.
Eq. 3 shows the relationship between the enthalpy and the Gibbs Free Energy. The Gibbs free energy is the electrical work depending on the reversible potential between the cell electrodes (Erev, Eq. 4). Entropy is supplied in the form of heat. When the irreversible thermal losses are equivalent to the heat demand, the energy balance is obtained, and energy equilibrium takes the name of thermoneutral, Etn.
The SOEC efficiency (Eq. 6) is calculated as the ratio between chemical energy exiting the system, in terms of enthalpy and the electrical energy fed from the outside (Ee).
Where Ee is the electrical energy input equal to the current (z*F) multiplied by the operating potential E. The efficiency is equal to 1 at the thermoneutral conditions where all electrical energy and relative heat losses are converted into chemical energy.
As seen in
The fuel electrode (cathode) material is a Ni doped YSZ. However, high steam partial pressures and low hydrogen partial pressures at the interface often causes oxidation of the nickel which results in catalyst degradation. The hydrogen in the cathode feedstock can aid in overcoming this problem. Instead of, or in addition to Ni-YSZ as a cathode material, there are perovskite-type lanthanum strontium manganese (LSM) and lanthanum strontium manganese chromate (LSCM) that can be used instead of or in combination with Ni-YSZ.
On the anode side, the oxygen ions are produced in Eq. 1 and Eq. 2. In an SOEC, it is beneficial to use a sweep gas over the anode to sweep the anions (and oxygen gas) away from the anode. Feed stream 2 in
The electrolyte used in the SOEC is a dense ionic conductor consisting of ZrO2 doped with 8 mol % Y2O3 (also known as YSZ). Zirconia dioxide is used because of its high strength, high melting temperature (approximately 2700° C.) and excellent corrosion resistance. Other electrolyte materials include Scandia stabilized zirconia (ScSZ), ceria-based electrolytes or lanthanum gallate materials. All materials can be used separately or in combinations.
Product stream 2 or the hot cathode product comprises hydrogen and carbon monoxide. The product stream leaves the cathode at the SOEC operating temperature of 550 to 900° C. The product stream can be used to heat the incoming cathode feed via a feed/product heat exchanger. The cathode feed stream comprises steam and carbon dioxide.
Product stream 1 is the hot anode product stream that comprises oxygen or an oxygen-enriched sweep gas. The product stream leaves the cathode at the SOEC operating temperature of 550 to 900° C. The product stream can be used to heat the Feed Stream 2 or incoming anode feed via a feed/product heat exchanger.
The cooled Product Stream 2 or cathode product comprises synthesis gas. The steam goes to Unit 2 or the syngas conditioning unit. The syngas conditioning block is actually a collection of a number of unit operations. It includes additional cooling, water removal, adjustment of the hydrogen to carbon monoxide ratio, carbon dioxide removal, and compression to raise the pressure to the Unit 4 (LFP reactor). This produces a Product Stream 3 that becomes the LFP Feed stream that comprises syngas with a hydrogen to carbon monoxide molar ratio of 1.5 to 2.5, or more preferably 2.0 to 2.2. Besides the hydrogen and carbon monoxide in product stream 2, other components are likely in the stream including unreacted carbon dioxide, unreacted hydrogen, and water. Water is removed in a flash drum. The water removed becomes Product Stream 7 in
If the hydrogen to carbon monoxide ratio in the syngas conditioning unit feed is greater than 2.2, excess hydrogen can be removed from the stream by any know hydrogen removal system such as pressure swing adsorption (PSA), hydrogen membranes, or other methods. The excess hydrogen containing stream can be recycled to the front end of the process to supplement the Unit 1, and blended SOEC Cathode feed. If the hydrogen to carbon monoxide is less than 2.0, additional hydrogen can be produced by the water gas shift reaction (Eq. 7).
H2O+CO↔H2+CO2 Eq. 7
If required to meet the syngas composition specification, a catalytic reactor can be used to convert some of the CO to additional hydrogen.
Removal of carbon dioxide in the syngas is useful as carbon dioxide is a diluent in downstream processing. Carbon dioxide removal is done by any of a number of different processes including: 1) amine absorbers, 2) Rectisol or methanol absorbers, 3) Other physical absorbers like Solexol, 4) Cryogenic CO2 fractionation. The captured and removed CO2 will result in a CO2 stream that can be sent back to the front end of the process to add to the Feed Stream 1.
The operating pressure of the SOEC is near ambient pressure. Unit 4, the LFP reactor operates at pressures of 250 to 450 psig. The syngas conditioning block, unit 2, comprises a syngas compressor. This will be a multi-stage compressor system with interstage cooling.
Unit 2 produces a Product Stream 3 that is the feed stream to Unit 4. Unit 4 is the Liquid Fuel Production (LFP) reactor.
The F-T reaction is exothermic with a standard enthalpy of reaction released of 165 kJ/mol of CO converted. The high heat of reaction makes control of the F-T reactor temperature critical. If uncontrolled, the temperature rise in the reactor would result in higher methane production and higher catalyst deactivation. As such control of the temperature is important. Ideally the temperature of the F-T reactor is maintained at 200 to 240° C.
The multi-tubular fixed bed reactor of
Feed stream 3, comprising liquid water, is fed to Unit 3 (
The hydrocarbon product from the LFP reactor is further processed downstream of the Unit 4 LFP reactor. Water is also produced in the F-T reaction (Eq. 8). Water can be removed from the F-T product stream by a flash drum. The recovered water can also be recycled back to the liquid water processing, Unit 3, in
In one embodiment of the invention, the kerosene cut of the LFP product does not meet all the ASTM D7566 specification for use as jet fuel. Jet fuel may have a higher value than diesel fuel in certain circumstances. It may be necessary to hydroprocess the LFP product or a fraction of the LFP product such as LFP kerosene or LFP light diesel to meet the specification for use as jet fuel or sustainable aviation fuel (SAF). The hydroprocessing includes the hydroisomerization of the C9-C15 alkanes produced in the LFP reactor. The LFP product or a fraction of the product is pressurized and mixed with a stream comprising hydrogen. The hydrogen can be produced from the electrolysis of water or from the reforming of natural gas or from the gasification of waste or biomass. It is preferred that the hydrogen is a low carbon hydrogen.
The combined stream comprising hydrogen and at least a portion of the LFP product is then heated and fed to the hydroprocessing reactor. The hydroprocessing reactor operates at an elevated pressure of greater than 100 psig but generally less than 2000 psig. The hydroprocessing reactor operates at a temperature between 250° C. and 400° C. Effluent from the hydroprocessing reactor is cooled before entering the hot separator where gas and liquid are separated in hot and cold separators.
The hydrocarbon products from the hot and cold separators are sent to the fractionation section where the light-ends and hydrocarbon products are separated. This fraction system may include a wax stripper and main fractionator as well as a naphtha stabilizer and a kerosene vacuum column. The fractionators are operated in a manner such that the kerosene stream will meet the specifications of ASTM D7566 and is useful as a Sustainable Aviation Fuel (SAF).
The following examples illustrate some aspects of the invention.
In this example, 1000 molts of liquid water and 500 molts of carbon dioxide are fed to an SOEC. 800 mol/s of hydrogen and 400 molts of carbon monoxide are produced. Using the heat requirements for the reactions of Eq. 1 and Eq. 2 with liquid water as a feedstock, a minimum electrical demand for the SOEC stack can be calculated. In this example, the minimum electrical requirement is 401.3 MW.
In this example, 1000 molts of steam produced in the LFP reactor Unit 5 boiler are fed to the SOEC instead of the liquid water in example 1. 800 molts of hydrogen and 400 molts of carbon monoxide are produced in the SOEC. Using the heat requirements for the reactions of Eq. 1 and Eq. 2 with steam as a feedstock, a minimum electrical demand for the SOEC can be calculated. In this example, the minimum electrical requirement is 360.4 MW.
Table 1 shows the improvement of Example 2 versus Example 1. The use of steam saves 40.9 MW of electricity and shows a 10.2% improvement in electricity required by the SOEC.
The amount of steam that can be produced in the LFP reactor boiler drastically reduces the feed water required for the SOEC. Table 2 below highlights the overall process improvements. With a 50% single pass CO conversion in the LFP reactor, the amount of reaction heat released is equal to 33.0 MW. That amount of reaction heat can produce 745.4 molts of steam from water. The remaining 245.3 molts required by the SOEC can be partially supplied by recycle of unconverted steam.
This application claims priority benefit of U.S. Provisional Patent Application No. 63/372,384, filed Mar. 8, 2022, the entire content of which is hereby incorporated by reference into this document.
Number | Date | Country | |
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63372384 | Mar 2022 | US |
Number | Date | Country | |
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Parent | 18445018 | Mar 2023 | US |
Child | 18445548 | US |