This disclosure relates to burner devices and combustion processes useful in furnaces, and furnaces including and/or using such burner devices. In particular, this disclosure relates to burner devices and combustion processes useful for steam cracking furnaces, hydrocarbon-steam reforming furnaces, and steam boiler furnaces generating a flue gas having a low NOx concentration, and such furnaces including such burner devices. The devices and processes of this disclosure are especially useful for combusting a fuel comprising hydrogen at a high concentration in an industrial furnace such as a steam cracking furnace.
As a result of the interest in recent years to reduce the emission of pollutants from burners used in large industrial furnaces, burner design has undergone substantial changes. In the past, improvements in burner design were aimed primarily at combustion efficiency and effective heat transfer. However, increasingly stringent environmental regulations have shifted the focus of burner design to the minimization of regulated pollutants.
Oxides of nitrogen (NOx) are formed in air at high temperatures. These compounds include, but are not limited to, nitrogen oxide and nitrogen dioxide. Reduction of NOx emissions is a desired goal to decrease air pollution and meet government regulations. In recent years, a wide variety of mobile and stationary sources of NOx emissions have come under increased scrutiny and regulation.
A strategy for achieving lower NOx emission levels is to install a NOx reduction catalyst to treat the furnace exhaust stream. This strategy, known as Selective Catalytic Reduction (SCR), is very costly and, although it can be effective in meeting more stringent regulations, represents a less desirable alternative to improvements in burner design.
Burners used in large industrial furnaces may use either liquid fuel or gas. Liquid fuel burners may mix the fuel with steam prior to combustion to atomize the fuel to enable more complete combustion, and combustion air is mixed with the fuel in the zone of combustion.
Gas fired burners can be classified as either premix or raw gas, depending on the method used to combine the air and fuel. They also differ in configuration and the type of burner tip used.
Raw gas burners inject fuel directly into the air stream, and the mixing of fuel and air occurs simultaneously with combustion. Since airflow does not change appreciably with fuel flow, the air register settings of natural draft burners must be changed after firing rate changes. Therefore, frequent adjustment may be necessary. In addition, many raw gas burners produce luminous flames.
Premix burners mix some or all of the fuel with some or all of the combustion air prior to combustion. Since premixing is accomplished by using the energy present in the fuel stream, airflow is largely proportional to fuel flow. Premixing the fuel and air also facilitates the achievement of the desired flame characteristics. Due to these properties, premix burners are often compatible with various steam cracking furnace configurations.
Premix burners are used in many floor-fired steam crackers and arch/roof-fired steam reformers primarily because of their ability to produce a relatively uniform heat distribution profile in the tall radiant sections of these furnaces. Flames are non-luminous, permitting tube metal temperatures to be readily monitored. Therefore, a premix burner is the burner of choice for such furnaces. Premix burners can also be designed for special heat distribution profiles or flame shapes required in other types of furnaces.
One technique for reducing NOx that has become widely accepted in industry is known as combustion staging. With combustion staging, the primary flame zone is deficient in either air (fuel-rich) or fuel (fuel-lean). The balance of the air or fuel is injected into the burner in a secondary flame zone or elsewhere in the combustion chamber located in a furnace enclosure. A fuel-rich or fuel-lean combustion zone is less conducive to NOx formation than an oxygen-fuel ratio closer to stoichiometry. Combustion staging results in reducing peak temperatures in the primary flame zone and therefore has been found to reduce NOx. Since NOx formation is exponentially dependent on gas temperature, even small reductions in peak flame temperature can dramatically reduce NOx emissions. However, this must be balanced with the fact that radiant heat transfer decreases with reduced flame temperature, while carbon monoxide (CO) emissions, an indication of incomplete combustion, may actually increase as well.
In the context of premix burners, the term primary air refers to the air premixed with the fuel, and secondary air refers to the balance of the air required for proper combustion. In raw gas burners, primary air is the air that is more closely associated with the fuel, and secondary are more remotely associated with the fuel. The upper limit of flammability refers to the mixture containing the maximum fuel concentration (fuel-rich) through which a flame can propagate.
One set of techniques achieves lower flame temperatures by diluting the fuel-air mixture with inert material. Flue gas (the products of the combustion reaction) or steam are commonly used diluents. Such burners are classified as FGR (flue gas-recirculation) or steam-injected, respectively.
References of interest include U.S. Pat. Nos. 2,813,578, 2,918,117, 4,004,875, 4,230,445, 4,257,763, 4,575,332, 4,629,413, 4,708,638, 5,092,761, 5,098,282, 5,263,849, 5,269,679, 6,007,325, 6,877,980, 6,869,277, 6,902,390, and 6,846,175.
This disclosure relates to a burner device for combusting a fuel in a furnace enclosure. The burner device can include a primary air chamber configured to receive a primary air and a flue gas to form an air-flue gas mixture in the primary air chamber, a staged air chamber configured to receive a staged air, and a tertiary air chamber configured to receive a tertiary air. The burner device can also include a burner tube having a first tube end and a second tube end. The first tube end can be configured to receive the air-flue gas mixture from the primary air chamber and a fuel to form a fuel-air-flue gas mixture in the burner tube. The burner device also can include a burner tip downstream of the second tube end. The burner tip can include center orifices and side orifices, where the burner tip is configured to discharge a first portion of the fuel-air-flue gas mixture into a first combustion zone in the furnace enclosure via the center orifices and a second portion of the fuel-air-flue gas mixture into a second combustion zone in the furnace enclosure via the side orifices, respectively. The burner device also can include one or more staged air ports configured to discharge the staged air from the staged air chamber into a third combustion zone in the furnace enclosure, and a tile adjacent to the burner tip and configured to form a tile-burner tip gap between the burner tip and the tile. The tile-burner tip gap is in fluid communication with the tertiary air chamber and capable of discharging the tertiary air into the second combustion zone.
The disclosure also relates to a process of combusting a fuel in a furnace or boiler using the above-described burner device, and a furnace (e.g., steam cracking furnace, hydrocarbon-steam reforming furnace, or steam boiler furnace) including the above-described burner device.
This disclosure also relates to a process for combusting a fuel in a furnace. The furnace can include a furnace enclosure and a burner device, where the burner device can include a primary air chamber, a staged air chamber, a tertiary air chamber, a burner tube having a first tube end and a second tube end, and a burner tip having center orifices and side orifices coupled to the second tube end of the burner tube. A tile in proximity to the burner tip defines a tile-burner tip gap between the tile and the burner tip. The first tube end is in fluid communication with the primary air chamber, the furnace enclosure is in fluid communication with the staged air chamber via one or more staged air ports, and the furnace enclosure is in fluid communication with the tertiary chamber via the tile-burner tip gap. The process can include supplying a primary air and a flue gas into the primary air chamber to form an air-flue gas mixture in the primary air chamber, supplying a staged air into the staged air chamber, supplying a tertiary air into the tertiary air chamber, and supplying the fuel into the first tube end. The process also can include receiving the air-flue gas mixture via the first tube end into the burner tube to mix with fuel to form a fuel-air-flue gas mixture in the burner tube, discharging a first portion of the fuel-air-flue gas mixture into a first combustion zone in the furnace enclosure via the center orifices of the burner tip, and discharging a second portion of the fuel-air-flue gas mixture into a second combustion zone in the furnace enclosure via the side orifices of the burner tip. The process also can include discharging the tertiary air into the second combustion zone via the tile-burner tip gap, discharging the staged air from the staged air chamber into a third combustion zone in the furnace enclosure via the one or more staged air ports, and combusting the fuel in at least one of the first combustion zone, the second combustion zone, and the third combustion zone.
These and other features and attributes of the disclosed burner device of the present disclosure and their advantageous applications and/or uses will be apparent from the detailed description which follows.
To assist those of ordinary skill in the relevant art in making and using the subject matter hereof, reference is made to the appended drawings, wherein:
One or more specific embodiments of the present disclosure will be described below. In an effort to provide a concise description of these embodiments, all features of an actual implementation may not be described in the specification. It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions must be made to achieve the developers' specific goals, such as compliance with system-related and business-related constraints, which may vary from one implementation to another. Moreover, it should be appreciated that such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure.
When introducing elements of various embodiments of the present disclosure, the articles “a,” “an,” “the,” and “said” are intended to mean that there are one or more of the elements. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements. All numerical values within the detailed description herein are modified by “about” the indicated value, and take into account experimental error and variations that would be expected by a person having ordinary skill in the art.
Reference is now made to the embodiments illustrated in
Although the present burner device is described for use in connection with a furnace, it will be apparent to one of ordinary skill in the art that the teachings of the present disclosure also have applicability to other process components involving the combustion of a fuel. When in use, the burner devices of this disclosure may be mounted on a floor, a side wall, a ceiling, or any inside and/or outside fixture, of a furnace enclosure. A furnace enclosure in this disclosure can have one or more opening receiving and/or discharging certain materials such as feeds, product, and byproducts, e.g., an opening for discharging at least a portion of the flue gas generated by combustion the fuel. During operation of the burner device, a fuel (e.g., a hydrocarbon fuel such as natural gas, methane, ethane, propane, butane, and the like, hydrogen, and the like, and mixtures thereof) and an oxidant (e.g., air, oxygen, gas-turbine-exhaust and the like, and mixtures thereof) are supplied to the burner device, which facilitates the combustion reactions between components of the fuel and the oxidant, in various combustion zones preferably located in a furnace enclosure, releasing thermal energy and producing a flue gas. The thermal energy can be utilized to drive chemical reactions, producing steam, and the like. In particularly advantageous embodiments, the burner devices and processes of this disclosure can be used in industrial furnaces such as steam cracking furnaces, hydrocarbon-steam reforming furnaces (e.g., methane steam reforming furnaces), and steam boiler furnaces.
The burner devices and processes of this disclosure can have one or more of the following advantages: (i) producing a flue gas comprising NOx at a low level, especially compared to similar burner devices and processes in the prior art, even if a fuel comprising hydrogen at a high concentration (e.g., ≥80 mol %, ≥90 mol %, of even close to 100 mol %) is used, thereby reducing the need of NOx abatement needs for the flue gas; (ii) producing a flue gas comprising CO2 at a low level, if a fuel comprising hydrogen at a high concentration (e.g., ≥80 mol %, ≥90 mol %, of even close to 100 mol %) is used, thereby reducing the carbon footprint of the furnace operation; (iii) combusting a fuel comprising hydrogen at a high concentration stably and reliably without flame flash back, which is associated with the high flame speed of hydrogen combustion, and can significantly reduce burner life; (iv) capability of combusting multiple fuels ranging from pure methane, to any mixture comprising methane and hydrogen, to pure hydrogen, thereby making the operation of the furnace highly flexible and ready for a future dominated by hydrogen fuel; and (v) capability to switch from one fuel (e.g., a fuel comprising hydrogen at high concentration) to an alternate fuel (e.g., any mixture comprising methane and hydrogen, or even pure methane) during operation of the furnace (e.g., after a first time interval, such as a first pre-defined time interval has lapsed), with stable operation, thereby making the furnace highly resilient to fuel supply interruption.
Referring now to the drawings,
The burner tip 22 can be located at and coupled to the second tube end 18 of the burner tube 12 and is surrounded by a tile 24. In some embodiments, the tile 24 has an annular shape. In some embodiments, the burner tip 22 is fastened (e.g., by a thread mechanism) or otherwise attached to the second tube end 18 of the burner tube 12. In certain preferred embodiments, the burner tip 22 can share the longitudinal axis 70 with the inner fluid channel of the burner tube 12. The burner tip 22 can have one or more center orifices and multiple side orifices, noting that the center orifices and side orifices are illustrated in, and described in greater detail with reference to,
A fuel orifice 26, which is located at or in a gas spud 28, can be mounted at a top end of a fuel supply tube 30 (e.g., adjacent to the first tube end 16 of the burner tube 12) and introduces fuel into the burner tube 12, creating a high-velocity fuel jet. In some embodiments, the fuel orifice 26 is inserted into the first tube end 16 of the burner tube 12, while in other embodiments, the fuel orifice 26 is outside of and preferably in proximity to the first tube end 16. In certain preferred embodiments, the center of the gas spud 28, the center of the fuel orifice 26, the center of the fuel jet entering the first tube end 16, and the center of the first tube end 16 are aligned substantially with the longitudinal axis 70 of the inner fluid channel of the burner tube 12. An action caused by the high-velocity fuel jet and the venturi segment 20 of the burner tube 12 can draw air (e.g., ambient air) into a primary air chamber 32 through one or more primary air inlets 34a illustrated in
In certain embodiments, it may be desirable to reduce the flow rate of the primary air through the primary air inlet 34a into the primary air chamber 32 to a lower level (e.g., to substantially zero), by, e.g., adjusting the primary air inlet damper 34b, during the operation of the burner device 10. For example, in certain embodiments, at the startup of the operation of the burner device 10, it may be desirable to open the primary air inlet damper 34b sufficiently to allow a considerable amount of air intake from the primary air inlet 34a into the primary air chamber 32 to facilitate the establishment of a flame and stable combustion in the first combustion zone 60 and the second combustion zone 68 described below in this disclosure. Once a stable combustion flame is established, in certain embodiments, it may be desirable to adjust the primary air inlet damper 34b, or even close it down completely, to reduce air intake into the primary air chamber 32 from the primary air inlet 34a. As described below, a bleed air and a flue gas may be drawn into the primary air chamber 32 as well. The bleed air may constitute a portion of the primary air in the primary air chamber 32. Thus, even if the primary air inlet damper 34b is completely closed, a certain amount of primary air can be nonetheless drawn into the primary air chamber 32, which is then drawn into the burner tube 12 to facilitate combustion of the fuel, as described below. Even in completely closed position, some air leakage through the primary air inlet damper 34b can be tolerated.
The primary air (or mixture thereof with other fluids such a flue gas, described in detail below) is drawn into the first tube end 16 of the burner tube 12 to mix with the fuel. One or more steam supply tubes 36 illustrated in
A staged air chamber 40 may receive a staged air (e.g., fresh or ambient air, with or without pretreatment such as filtration or preheating) from a staged air channel 42 via a staged air inlet 42a having one or more staged air inlet dampers 42b, noting that the staged air channel 42, staged air inlet 42a, and staged air inlet dampers 42b are illustrated in
As shown in
Mixing elements 56 (e.g., chevron mixers) illustrated in
A perforated plate 61 beneath the first tube end 16 of the burner tube 12 can be used to enable proper location (e.g., horizontal and/or vertical location) of the gas spud 28 relative to the burner tube 12. In some embodiments, the perforated plate 61 also permits the air-flue gas mixture to be drawn from the primary air chamber 32 into the first tube end 16 of the burner tube 12. Additionally or alternatively, bolted spacers 63 may extend between the perforated plate 61 and the first tube end 16 of the burner tube 12, and gaps between adjacent ones of the bolted spacers 63 may permit the air-flue gas mixture to be drawn from the primary air chamber 32 into the first tube end 16 of the burner tube 12.
The burner tube 12 also receives the fuel via the fuel supply tube 30 (and, in some embodiments, steam via the steam supply tubes 36), thereby generating a fuel-air-flue gas mixture in the burner tube 12. By way of the above-described heat exchanger 58, a temperature of the fuel-air-flue gas mixture in the burner tube 12 can be significantly reduced relative to configurations not employing the heat exchanger 58, thereby lowering the flame temperature at least in the first combustion zone 60 (e.g., primary combustion or flame zone) directly above the burner tip 22 and within the combustion chamber 38, contributing to a lower NOx formation in the first combustion zone 60. In the same way, the temperature of the fuel-air-flue gas mixture exiting the side orifices of the burner tip 22 is reduced, thereby reducing NOx emissions in the second combustion zone 68.
In addition, in certain embodiments, it is highly desirable that the amount of primary air allowed to enter the primary air chamber 32 is limited (e.g., by adjusting the primary air inlet damper 34b to reduce or stop flow of air through the primary air inlet 34a into the primary air chamber 32), such that at least during stable operation of the burner device 10, the amount of oxygen in the fuel-air-flue gas mixture inside the burner tube 12 is significantly below the level required for stoichiometric combustion of the fuel. As discussed above, a portion, preferably a majority, preferably ≥60 mol %, preferably ≥70 mol %, preferably ≥80 mol %, of the fuel-air-flue gas mixture in the burner tube 12 is discharged, via the center orifices of the burner tip 22, into the first combustion zone 60. By combusting at significantly below stoichiometry, the flame in the first combustion zone 60 can have a desirably low temperature, avoiding the generation of substantial quantity of NOx and contributing to an overall low NOx production from the burner device 10 operation.
Furthermore, it is known that hydrogen combustion is characterized by very high flame speed, which can cause the flame to enter into the burner tip 22 and even the burner tube 12, a phenomenon called “flash-back.” Flash-back is highly detrimental to the operation life of the burner tip 22 and the burner tube 12 if allowed to occur. Because of this, there has been doubt that a fuel comprising hydrogen at a high concentration, e.g., ≥80 mol %, ≥85 mol %, ≥90 mol %, ≥95 mol %, let alone pure hydrogen, can be safely and reliably combusted in a burner device 10 featuring a mixture of air and fuel in the burner tube 12 upstream of the burner tip 22. Surprisingly, the present inventors have found that, by limiting the amount of primary air drawn into the primary air chamber 32 (e.g., by adjusting the primary air inlet damper 34b to reduce or even stop flow of air through the primary air inlet 34a into the primary air chamber 32), and thus maintaining the oxygen level in the fuel-air-flue gas mixture in the burner tube 12 at significantly lower than required for stoichiometric combustion, flash-back can be substantially prevented and avoided when using the burner device 10 of this disclosure. The present inventors have also found that, surprisingly, a stable flame can nonetheless be maintained in the first combustion zone 60 notwithstanding a low oxygen level in the fuel-air-flue gas mixture, due partly to a high flammability range of hydrogen in case a fuel comprising hydrogen at a high concentration is combusted, and a stable flame that can be produced and maintained in the second combustion zone 68, as described elsewhere in this disclosure.
As described above, a portion, preferably ≤50 mol %, preferably ≤40 mol %, preferably ≤30 mol %, preferably ≤20 mol %, preferably ≤15 mol %, e.g., from 5 mol % to 15 mol %, of the fuel-air-flue gas mixture in the burner tube 12 is discharged, via the side apertures of the burner tip 22, into the second combustion zone 68. The combustion reactions in the second combustion zone 68, aided by additional oxygen supplied from an air chamber separate from the primary air chamber 32 (a tertiary air chamber 62, e.g., described in detail below), can be allowed to combust within the air-fuel flammability range, i.e., closer to stoichiometric ratio than in the first combustion zone 60, thereby producing a flame that can have a high temperature, e.g., higher than the temperature of the flame in the first combustion zone 60, and/or higher than the temperature in the flame in a third combustion zone 78 as described below. The flame temperature in the second combustion zone 68 can be particularly high when a fuel comprising hydrogen at a high concentration is combusted. Since NOx can be produced at exponentially higher amount at higher temperature, NOx production in the second combustion zone 68 can be a significant issue for any burner, especially one combusting a fuel comprising hydrogen at a high concentration. NOx production in the second combustion zone in a conventional burner device that supplies a portion of the heated staged air into the second combustion zone can be particularly undesirably high due to a high flame temperature in the second combustion zone
In the burner device 10 and the processes of this disclosure, a tertiary air is supplied to the second combustion zone 68 via the tertiary air chamber 62 mentioned above. Preferably the tertiary air has a relatively low temperature to produce a flame in the second combustion zone 68 having a relatively low temperature to avoid generation of large quantity of NOx. As shown
As shown in
Staged air ports (hidden from view in
As previously described, the tertiary air damper stopper 64c illustrated in
As described above, the staged air ports configured to discharge the staged air into the third combustion zone 78 of the combustion chamber 38 are hidden from view in
As previously described, the burner tip 22 in
The burner tip 22 may include a larger number of the center orifices 112 than the side orifices 116, such that a larger portion of the fuel-air-flue gas mixture is discharged from the center orifices 112 than the side orifices 116. While the illustrated cross-section depicts a row of the center orifices 112, it should be understood that a circle or ring of the center orifices 112 may be disposed through the recessed portion 114 of the burner tip 22. Likewise, the side orifices 116 may extend annularly about the side wall 118 of the burner tip 22. In certain embodiments, the ratio r of the total combined cross-sectional area A1 of the side orifices 116 to the sum total of A1 and the total combined cross-sectional area A2 of the center orifices 112 can be from 5% and 15%, i.e., 5%≤r=A1/(A1+A2)*100%≤15%, e.g., 5%, 6%, 7%, 8%, 9%, 10%, 11% 12%, 13%, 14%, 15%. In certain embodiments, the total amount of the second portion of the fuel-air-flue gas mixture discharged through the side orifices 116 to the second combustion zone 68 illustrated in
When the fuel is supplied into the first tube end 16 of the burner tube 12, the above-described venturi features of the burner tube 12 can generate pressure gradients and a high efficiency inspirating effect that draws various fluid flows (e.g., flue gas, primary air, steam) into the burner device 10 described above with reference to earlier drawings.
As shown in
The burner device of this disclosure can combust many different combustion fuels efficiently, reliably, and safely.
One aspect of this disclosure relates to a furnace, such as an industrial furnace including one or more of the burner devices of this disclosure as described and illustrated above.
A particularly advantageous industrial furnace of this disclosure is a steam cracking furnace including one of more of the burner devices installed, e.g., on the floor of the furnace enclosure, in proximity to a plurality of tubes (called “radiant tubes”) acting as pyrolysis reactors. During the operation of the steam cracking furnace, a preheated mixture of steam with a steam-cracking hydrocarbon feed (e.g., methane, ethane, propane, butane, naphtha, gas oil, and even crude oil, and mixtures thereof) passes through the radiant tubes. The burner device combusts the combustion fuel (e.g., methane, natural gas, ethane, propane, butane, and the like, hydrogen, and mixtures thereof) with an oxidant such as air, releasing thermal energy in the form of radiation from the flame and a hot flue gas. The radiant tubes are heated by the released thermal energy to an elevated temperature, which, in turn, heats the steam-steam cracking feed mixture inside the tubes, to an elevated temperature to effect pyrolysis reactions of the hydrocarbons in the steam cracking feed, producing a steam cracker effluent comprising hydrogen, C1-C4 hydrocarbons including ethylene, propylene, and other olefins, naphtha, gas oil, and steam cracker tar. The steam cracker effluent can be quenched, processed, separated, and treated to produce one or more valuable products such as ethylene, propylene, butenes, butadiene, steam cracker naphtha, and one or more byproducts such as steam cracker hydrogen, a tail-gas comprising methane and hydrogen, an ethane-rich stream, and the like. The hydrogen, the tail gas, and/or the ethane-rich stream can be advantageously supplied to the burner devices in the steam cracker furnace (or another furnace such as steam boiler furnace), as at least a portion of the combustion fuel. By supplying the steam cracker hydrogen and/or tail-gas to the burner devices as burner fuel, one can reduce the amount of CO2 produced from operating the steam cracker significantly.
Another advantageous industrial furnace of this disclosure is a hydrocarbon-steam reformer furnace including one of more of the burner devices installed, e.g., on the roof and/or side walls of the furnace enclosure, in proximity to a plurality of catalyst-loaded tubes (called “reforming tubes”) acting as hydrocarbon-steam reforming reactors. During the operation of the hydrocarbon-steam reforming furnace, a preheated mixture of steam with a reforming hydrocarbon feed (e.g., methane, ethane, propane, butane, naphtha, and mixtures thereof) passes through the reforming tubes and contacts the catalyst. The burner device combusts the combustion fuel (e.g., methane, natural gas, ethane, propane, butane, and the like, hydrogen, and mixtures thereof) with an oxidant such as air, releasing thermal energy in the form of radiation from the flame and a hot flue gas. The reforming tubes are heated by the released thermal energy to an elevated temperature, which, in turn, heats the steam-reforming feed mixture inside the reforming tubes, to an elevated temperature to effect reforming reactions of the hydrocarbons in the steam cracking feed in the presence of the catalyst, producing a reforming effluent comprising hydrogen, CO, CO2, and steam. The reforming effluent can be cooled, shifted, separated, and treated to produce one or more products such as hydrogen, hydrogen-methane mixture, and CO2. The hydrogen and/or the hydrogen/methane mixture can be advantageously supplied to the burner devices in the hydrocarbon-steam reforming furnace (or another furnace such as steam boiler furnace), as at least a portion of the combustion fuel. By supplying the hydrogen and/or hydrogen-methane mixture to the burner devices as combustion fuel, one can reduce the amount of CO2 produced from operating the hydrocarbon-steam reforming furnace significantly.
This written description uses embodiments/examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other embodiments/examples that occur to those skilled in the art. Such other embodiments/examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims. Many alterations, modifications, and variations will be apparent to those skilled in the art in light of the foregoing description without departing from the spirit or scope of the present disclosure and that when numerical lower limits and numerical upper limits are listed herein, ranges from any lower limit to any upper limit are contemplated.
This application claims priority to and the benefit of U.S. Provisional Application No. 63/495,788 having a filing date of Apr. 13, 2023, the disclosure of which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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63495788 | Apr 2023 | US |