METHANATION WITH TURBOCHARGER
20230392089 · 2023-12-07
Assignee
Inventors
Cpc classification
International classification
Abstract
The present invention relates to an improved methanation process, wherein energy released during the methanation process is used to drive a turbocharger to drive and/or maintain the process. The present invention is further concerned with a system for the production of methane-enriched gas and power from hydrogen and carbon-containing starting materials comprising at least one methanation reactor and at least one turbocharger.
Claims
1. A process for the production of methane-enriched gas from hydrogen and carbon-containing starting material in a system including at least one single-stage or multi-stage methanation process, comprising the following process steps: a) providing; one methanation reactor each for the at least one single-stage or multi-stage methanation process, wherein each methanation reactor comprises an entry for the introduction of feed gas, which comprises hydrogen and carbon-containing starting materials or methane-enriched gas from a previous methanation stage, and an exit for the methane-enriched product gas; a continuous gas line having an entrance for the introduction of hydrogen and carbon-containing starting material, and an exit for the removal of the methane-enriched gas from the system; and at least one turbocharger comprising a compressor and a turbine mechanically connected by a common shaft, wherein the methanation reactor(s) and the at least one turbocharger are connected via the continuous gas line; wherein the at least one compressor is connected with the continuous gas line, and is arranged in a section of the continuous gas line, which defines a path from the introduction of the starting material to the removal of the methane-enriched gas, in particular upstream, between, or downstream of the methanation reactor(s); b) introducing the hydrogen and carbon-containing starting material into the entrance of the continuous gas line; c) producing methane-enriched gas in the methanation reactor(s); and d) increasing the system pressure within the continuous gas line via the at least one compressor by using the energy released during the methanation process.
2. The process of claim 1, further comprising an additional step between steps b) and c) of injecting water or steam directly into at least one methanation reactor, or into the continuous gas line upstream of the entry for the introduction of feed gas of the at least one methanation reactor and/or turbocharger turbine.
3. The process of claim 1, wherein: in step a) a thermal power plant with a working medium conducted in thermal power plant lines is provided, the thermal power plant is coupled to at least one of the methanation reactors or a gas stream derived therefrom via at least one heat exchanger, the thermal power plant produces electrical power, and optionally the thermal power plant is a steam turbine with steam conducted in lines of a steam turbine cycle.
4. The process of claim 1, wherein the turbine of the at least one turbocharger is connected to the continuous gas line; and/or further comprising step e) of removing the methane-enriched gas at the exit of the continuous gas line from the system; and/or wherein the carbon-containing starting material is CO.sub.2 and/or CO; and/or wherein the hydrogen and the carbon-containing starting material is provided at atmospheric pressure; and/or wherein the pressure at the exit of the continuous gas line is higher than the pressure at the entrance of the continuous gas line.
5. The process of claim 1, further comprising; preheating the methanation reactor(s) prior to step b); and/or providing the compressor with external energy to facilitate the initial compression of the hydrogen and the carbon-containing starting material prior to the methanation process.
6. The process of claim 1, wherein: the one or more compressors increase the pressure within the continuous gas line at a position located between the entrance of the continuous gas line and the entry of the first methanation reactor; and/or the one or more compressors increase the pressure within the continuous gas line at a position located between the exit of the methanation reactor and the exit of the continuous gas line; and/or the turbine is located at a position upstream of the one or more compressors.
7. The process of claim 1, wherein: a plurality of turbochargers is used; or intermediate cooling or intermediate heating of the continuous gas line is performed via heat exchanger elements; and/or the at least one single-stage methanation process is adiabatic or at least one stage of the multi-stage methanation process is adiabatic.
8. The process of claim 3, wherein the at least one single-stage methanation process is isothermal or at least one stage of the multi-stage methanation process is isothermal, and wherein in the isothermal process, the temperature in the methanation reactor is controlled by the thermal power plant.
9. The process of claim 1, wherein: the turbine reduces the pressure of the gas exiting the methanation reactor.
10. The process of claim 1, wherein: the at least one turbocharger is located upstream of the methanation reactor and heat produced in the methanation reactor is supplied to the turbocharger at a location between the turbine and the compressor via at least one heat exchanger; the at least one turbocharger is located downstream of the methanation reactor and heat produced in the methanation reactor is supplied to the turbocharger at a location between the turbine and the compressor via at least one heat exchanger; or the at least one turbocharger is located between two methanation reactors, and heat produced in the methanation reactor located upstream of the turbocharger is supplied to the turbocharger prior to the turbocharger turbine inlet, preferably at a location between the turbine and the compressor, via at least one heat exchanger.
11. The process of claim 1, wherein a portion of the heat produced in the methanation process is used in the turbocharger, and another portion, which is preferably the bigger portion, is used to produce steam or power.
12. A system for the production of methane-enriched gas from hydrogen and carbon-containing starting material in at least one single-stage or multi-stage methanation process, wherein the system comprises: one methanation reactor each for the at least one single-stage or multi-stage methanation process, wherein each methanation reactor comprises an entry for the introduction of feed gas, which comprises hydrogen and carbon-containing starting materials or methane-enriched gas from a previous methanation stage, and an exit for the methane-enriched product gas; a continuous gas line having an entrance for the introduction of hydrogen and carbon-containing starting material, and an exit for the removal of the methane-enriched gas from the system; and at least one turbocharger comprising a compressor and a turbine mechanically connected by a common shaft; wherein the at least one compressor is connected with the continuous gas line, and is arranged in a section of the continuous gas line which defines a path from the introduction of the starting material to the removal of the methane-enriched gas, in particular upstream, between, or downstream of the methanation reactor(s).
13. The system of claim 12, further comprising a water/steam injection unit for directly injecting water or steam into the at least one methanation reactor, or into the continuous gas line upstream of the entry for the introduction of feed gas.
14. The system of claim 12, further comprising a thermal power plant with a working medium conducted in thermal power plant lines, in particular a steam turbine with lines of a steam turbine cycle, wherein the methanation reactor(s) and the at least one turbocharger are connected via the continuous gas line, wherein the thermal power plant is coupled to at least one of the methanation reactors or a gas stream derived therefrom via at least one heat exchanger, and wherein the thermal power plant is configured to produce electrical power.
15. The system of claim 12, wherein the at least one turbine is connected to the continuous gas line.
16. A method, comprising: using the system of claim 12 for the process of claim 1.
17. The process of claim 3, wherein the turbine reduces the pressure of the working medium conducted in thermal power plant lines used to control the temperature of a methanation reactor.
18. The process of claim 3, wherein the heat exchanger is a recuperator, the recuperator transferring heat from the gas exiting the turbine to the hydrogen and the carbon-containing starting material prior to the hydrogen and the carbon-containing starting material entering the methanation reactor.
19. The system of claim 3, wherein the turbine of the at least one turbocharger is connected to one of the thermal power plant lines.
20. The system of claim 14, wherein the at least one turbocharger turbine is connected to one of the thermal power plant lines.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DESCRIPTION OF THE INVENTION
[0052] The present invention concerns a process for the production of methane-enriched gas or methane and optionally power from hydrogen and carbon-containing starting material in a system comprising at least one single-stage or multi-stage methanation process, comprising the following process steps: [0053] a) providing [0054] one methanation reactor (1) each for the at least one single-stage or multi-stage methanation process, wherein each methanation reactor comprises an entry for the introduction of feed gas, which comprises hydrogen and carbon-containing starting materials or methane-enriched gas from a previous methanation stage, and an exit for the methane-enriched product gas; [0055] a continuous gas line having an entrance (6) for the introduction of hydrogen and carbon-containing starting material, and an exit (7) for the removal of the methane-enriched gas from the system; and [0056] at least one turbocharger (2) comprising a compressor (3) and a turbine (4) mechanically connected by a common shaft (5), wherein the methanation reactor(s) and the at least one turbocharger are connected via the continuous gas line; [0057] wherein the at least one compressor is connected with the continuous gas line, and is arranged in a section of the continuous gas line, which defines a path from the introduction of the starting material to the removal of the methane-enriched gas, in particular upstream, between, or downstream of the methanation reactor(s); [0058] b) introducing the hydrogen and carbon-containing starting material into the entrance of the continuous gas line, [0059] c) producing methane-enriched gas in the methanation reactor(s); and [0060] d) increasing the system pressure within the continuous gas line via the at least one compressor by using the energy released during the methanation process.
[0061] The present invention is also concerned with a system for the production of methane-enriched gas or methane and optionally power from hydrogen and carbon-containing starting materials in at least one single-stage or multi-stage methanation process. The present invention is also concerned with a system for maintaining the production of methane-enriched gas or methane and power from hydrogen and carbon-containing starting materials in at least one single-stage or multi-stage methanation process.
[0062] The system is used in the process of the present invention and comprises: [0063] one methanation reactor (1) each for the at least one single-stage or multi-stage methanation process, wherein each methanation reactor comprises an entry for the introduction of feed gas, which comprises hydrogen and carbon-containing starting materials or methane-enriched gas from a previous methanation stage, and an exit for the methane-enriched product gas; [0064] a continuous gas line having an entrance (6) for the introduction of hydrogen and carbon-containing starting material, and an exit (7) for the removal of the methane-enriched gas from the system; and [0065] at least one turbocharger (2) comprising a compressor (3) and a turbine (4) mechanically connected by a common shaft (5); [0066] wherein the at least one compressor is connected with the continuous gas line, and is arranged in a section of the continuous gas line which defines a path from the introduction of the starting material to the removal of the methane-enriched gas, in particular upstream, between, or downstream of the methanation reactor(s).
[0067] Another aspect of the present invention is the use of the system of the present invention for the methanation process of the present invention.
[0068] With the process or system of the present invention, a methanation process can be maintained efficiently by using the heat generated in the methanation reactor to drive a turbocharger to increase the pressure in the system. Therefore, the present invention can also be described as being a process or system for maintaining the production of methane-enriched gas or methane and optionally power from hydrogen and carbon-containing starting materials in a system comprising at least one single-stage or multi-stage methanation process as described above.
[0069] A feed gas in the context of the present invention is the gas that enters the methanation reactor, and, prior to the first methanation stage, the feed gas entering the methanation reactor comprises hydrogen and the carbon-containing starting materials. The feed gas in subsequent methanation stages comprises the product gas of the previous methanation stage, which is the methane-enriched gas produced in the previous methanation stage. The product gas in the context of the present invention is the gas exiting a methanation reactor. The product gas is methane-enriched or methanized gas, wherein the content of methane is increases compared to the feed gas entering the same methanation reactor. Depending on the composition of the feed, gas, for example the content of methane in the feed gas, and the reaction condition in the methanation reactor, the methane-enriched product gas can have a methane concentration of more than about 97%. The carbon-containing starting materials are preferably CO.sub.2 and/or CO.
[0070] The process and the system can be operated with the parameters used by the person skilled in the art.
[0071] The carbon-containing starting materials are preferably provided at atmospheric pressure. By using the compressor according to the invention, the pressure at the exit of the continuous gas line is higher than the pressure at the entrance of the continuous gas line. Preferably, the pressure can range from 0.1-100 bar, more preferably from 1.5-25 bar and even more preferably from 2-8 bar. In a generic setting, the compressor of a turbocharger increases the pressure by a factor of 2 to 8, and the turbine reduces the pressure by a factor of 1.5 to 3. The specific performance depends on the quality of the turbocharger. With every turbocharger stage, a pressure increase of a factor of about 1.5 to 3 can be expected. In the system shown in Example 1 and
[0072] In a two-stage system such as shown in Example 12 and
[0073] The process and the system of the present invention are particularly efficient in maintaining an ongoing methanation process. They can however also be used when a new methanation reaction is started. To start a new methanation reaction, the process of the present invention can further comprise preheating the methanation reactor(s) prior to introducing the hydrogen and carbon-containing starting materials into the entrance of the continuous gas line. The temperature range of the starting materials at the entrance of the continuous gas line can range from ambient temperature, such as room temperature, up to 100° C. The temperature at the entrance of the first methanation reactor is preferably at least about 130 to 150° C., as at this temperature range the exothermic reaction in the reactor maintains itself. The methanation process starts with a reactor temperature of about 200° C., more preferably of about 250° C. The feed gas comprising the hydrogen and carbon-containing starting materials is heated electrically to about 200° C. and fed into the system, which allows the process to start.
[0074] The process of the present invention can further comprise an additional step between steps b) and c) of injecting water or steam directly into at least one methanation reactor, or into the continuous gas line upstream of the entry for the introduction of feed gas of the at least one methanation reactor. This provides the advantage of increasing the mass flow in the turbine compared to the compressor, allowing the compressor to provide an increased pressurizing ratio. Furthermore, the temperature in the reactor can be limited if desired by injection of steam or water into the methanation reactor directly or prior to the entry of the methanation reactor. In these embodiments comprising a water/steam injection step, the system of the present invention comprises a water/steam injection unit for directly injecting water or steam into the at least one methanation reactor, or into the continuous gas line upstream of the entry for the introduction of feed gas. The water/steam injection unit comprises a line carrying water and/or steam. The water is pumped by a pump towards the methanation reactor or the continuous gas line at location prior to the entry of the methanation reactor. The water is converted to steam or hot water in a heat exchanger element using the heat provided by the product gas prior to the product gas exiting the system.
[0075] The process of the present invention can further comprise, additionally or alternatively, providing the compressor with external energy to facilitate the initial compression of the hydrogen and the carbon-containing starting materials prior to the start of the methanation process.
[0076] The location of the compressor in the process and system of the present invention is not particularly limited as long as the compressor is located at a position where it can pressurize gas in the continuous gas line. In one alternative, the compressor increases the pressure within the continuous gas line at a position located between the entrance of the continuous gas line and the entry of the methanation reactor, i.e. the compressor can be located at a position in the continuous gas line, which is located prior to the methanation reactor(s). This provides the advantage of having the methanation process occurring at an increased pressure level. In another alternative, the compressor increases the pressure within the continuous gas line at a position located between the exit of the methanation reactor and the exit of the continuous gas line, i.e. the compressor can also be located at a position in the continuous gas line, which is located after the methanation reactor(s). This provides the advantage that the volume flow in the compressor is reduced. In the methanation reaction, four molecules H.sub.2 and one molecule CO.sub.2 are reacted to two molecules water and one molecule methane, which corresponds to a reduction in volume to about ⅗. Reduction of volume flow in the compressor allows increase of the compressor performance.
[0077] In another alternative, the turbine can be located at a position upstream of the compressor. This provides the advantage of reducing the volume flow in the compressor further. The gas leaving the turbine can be cooled and water vapor can be condensed and removed prior to the gas entering the compressor. Thereby the gas volume is further reduced, particularly when comparing gas volume in the turbine and gas volume in the compressor.
[0078] In embodiments with more than one turbocharger, one compressor can be located prior to the first methanation reactor, and another compressor can be located after the last methanation reactor. One or more compressors can also be located between any two methanation reactors.
[0079] In the process or system of the present invention, the at least one turbocharger can be located upstream of the methanation reactor and heat produced in the methanation reactor can be supplied to the turbocharger at a location between the turbine and the compressor via at least one heat exchanger. Alternatively, the at least one turbocharger can be located downstream of the methanation reactor and heat produced in the methanation reactor can be supplied to the turbocharger at a location between the turbine and the compressor via at least one heat exchanger. The heat exchanger ensures that heat can be transferred to the turbocharger between its compressor and turbine components even in cases where the turbocharger is located upstream or downstream of the methanation reactor. Alternatively, the at least one turbocharger can be located between two methanation reactors, and heat produced in the methanation reactor located upstream of the turbocharger is supplied to the turbocharger prior to the turbocharger turbine inlet, preferably at a location between the turbine and the compressor, via at least one heat exchanger.
[0080] The process or system of the present invention comprise at least one turbocharger. They can also comprise a plurality of turbochargers. In certain embodiments 2, 3, or more turbochargers can be used. With every additional turbocharger stage, the pressure in the system can be increased.
[0081] The process or system of the present invention can further be controlled by intermediate cooling or intermediate heating of the continuous gas line via heat exchanger elements.
[0082] The term “heat exchanger element/heat exchanger” as used in this description can refer to an intermediate cooling element, an intermediate heating element, a recuperator, a gas cooling element, a pre-heating element, a condenser, and/or an evaporator. In a preferred embodiment, the heat exchanger can be a recuperator, wherein the recuperator transfers heat from the gas exiting the turbine to the hydrogen and the carbon-containing starting material to enter the methanation reactor.
[0083] In the process or system of the present invention, the at least one single-stage methanation process can be adiabatic or at least one stage of the multi-stage methanation process can be adiabatic. In an adiabatic process the gas temperature increases, which enhances the performance of the turbine. In a preferred embodiment, the first stage is performed in an adiabatic methanation reactor, leading to a maximum temperature in the system. The maximum temperature reached in the reactor can range from 350 to 800° C., such as from 500 to 800° C., and depends on the composition of the gas and the pressure. A preferred maximum temperature ranges from about 430 to about 720° C., such as from 630 to about 720° C. An adiabatic process is preferably used because it allows using the heat flow generated in the adiabatic process to drive the turbocharger, and particularly the compressor of the turbocharger. Further stages can also be adiabatic.
[0084] In the process or system of the present invention, the at least one single-stage methanation process can be isothermal or at least one stage of the multi-stage methanation process can be isothermal. The isothermal reaction occurs at a lower temperature range of about 200 to 300° C. and provides the advantage of the providing a better gas composition that can be used in downstream applications without further processing. A better gas composition means that more of the starting materials are reacted to methane. The product gas of an isothermal process comprises more methane than the product gas of an adiabatic process using the same starting materials. This is the case because the reaction balance at the high temperatures reached in an adiabatic process for the reaction to methane is not optimal.
[0085] In a preferred embodiment of the invention, the process or the system comprise a combination of at least one adiabatic process and at least one isothermal process to benefit from the advantages provided by both of these processes. The number of methanation stages can be chosen by the person of skill in the art depending on the requirements for the methane-enriched gas to be produced in the system. Further stages allow increasing the concentration of methane in the product gas.
[0086] In the isothermal methanation process of the invention, the temperature in the methanation reactor is controlled by a thermal power plant.
[0087] A thermal power plant in the context of the present invention is a system in which heat energy can be converted to electric power. When the thermal power plant is present in the system or process of the present invention, the system or process of the invention can be used to produce methane-enriched gas and power. For example, a steam-driven turbine can convert heat to mechanical power as an intermediate to electrical power. The steam turbine is connected to thermal power plant lines, in which a working medium is conducted. In preferred embodiments, the working medium is water and/or steam.
[0088] Alternatively, the working medium can be thermal oil or molten salt. Thermal oil or molten salt are generally used in intermediate circuits to store heat. The heat stored in the thermal oil/molten salt circuit is then transferred to a steam circuit. Therefore, the system will comprise an additional circuit compared to a system, which uses direct cooling with water/steam, making the system more complex. On the other hand, with indirect cooling via a thermal oil/molten salt circuit, the reactor does not need to be designed to work with high pressure such as up to 80 bar, as can be the case for direct cooling with a water/steam circuit. This is the case because a thermal oil circuits does not require pressure.
[0089] In the thermal power plant, the working medium, such as water, is heated, turns into steam and drives a steam turbine, which can drive an electrical generator. In several embodiments of the present invention, the heat flow generated in an isothermal methanation reactor can be used to heat the working medium in the thermal power plant system. Additionally, the working medium can be preheated in a heat exchanger element, wherein the heated methanized gas preheats the working medium prior to the methanized gas exiting the system. After the steam passes through the turbine, the steam is condensed in a condenser and recycled to where it was heated.
[0090] In the process or system of the present invention, the turbine of the turbocharger can reduce the pressure of the gas exiting a methanation reactor. Additionally or alternatively, the turbine can be located in the steam circuit of the thermal power plant and reduce the pressure of the working medium conducted in thermal power plant lines used to control the temperature of another methanation reactor.
[0091] In the process or system of the present invention, a portion of the heat produced in the methanation process can be used in the turbocharger, and another portion, which is preferably the bigger portion, can be used to produce steam or power. As it is thermodynamically impossible to use all of the heat produced in the methanation process in the turbocharger, it is advantageous to use the remaining heat for the generation of power.
[0092] This makes the process and system more efficient.
[0093] The invention is further illustrated in the following examples.
EXAMPLES
Example 1
[0094] One example for a system and process of the present invention is shown in
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Example 9
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[0104] Produced methane-enriched gas exits the second methanation reactor, is used to heat water flowing from the pump to the turbine of the turbocharger, and then exits the system.
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REFERENCE SIGN LIST
[0120] 1: Methanation reactor [0121] 2: Turbocharger [0122] 3: Compressor [0123] 4: Turbine [0124] 5: Shaft [0125] 6: Entrance of continuous gas line for the introduction of hydrogen and carbon-containing starting materials (feed gas) [0126] 7: Exit for the removal of the methane-enriched gas produced (product gas) [0127] 8: Heat exchanger/recuperator [0128] 8a: gas cooling element [0129] 8b: intermediate cooling element [0130] 8c: pre-heating element [0131] 8d: evaporator [0132] 8e: condenser [0133] 9: Exiting condensate [0134] 10: Heat flow [0135] 11: Water [0136] 12: Pump [0137] 13: Hot water/Steam [0138] 14: Hot water [0139] 15: Steam [0140] 16: Steam turbine for power generation