Regenerative cooling method and apparatus

Abstract

A method of cooling a liner in a plasma chamber. A recycle gas is contacted with or passed through the liner to cool the liner and pre-heat the recycle gas. The pre-heated gas is then recycled through the plasma chamber to become part of the plasma forming process. The method further comprises the liner is graphite, the recycle gas passes through at least one cooling channel present in the liner, at least one of the cooling channels are covered with at least one removable liner/channel cover, carbon deposits are formed from the presence of hydrocarbons in the recycle gas, at least one channel is formed in a spiral cooling channel pattern, at least one channel is formed in a substantially straight cooling channel pattern, and a plenum to aid in the production of an even distribution of cooling gas in the channels.

Description

TECHNICAL FIELD

The field of art to which this invention generally pertains is methods and apparatus for making use of electrical energy to effect chemical changes.

BACKGROUND

There are many processes that can be used and have been used over the years to produce carbon black. The energy sources used to produce such carbon blacks over the years have, in large part, been closely connected to the raw materials used to convert hydrocarbon containing materials into carbon black. Residual refinery oils and natural gas have long been a resource for the production of carbon black. Energy sources have evolved over time in chemical processes such as carbon black production from simple flame, to oil furnace, to plasma, to name a few. As in all manufacturing, there is a constant search for more efficient and effective ways to produce such products. Varying flow rates and other conditions of energy sources, varying flow rates and other conditions of raw materials, increasing speed of production, increasing yields, reducing manufacturing equipment wear characteristics, etc. have all been, and continue to be, part of this search over the years.

The systems described herein meet the challenges described above, and additionally attain more efficient and effective manufacturing process.

BRIEF SUMMARY

A method of cooling a liner in a plasma chamber is described including, contacting the liner with or passing through the liner, at least one recycle gas to be used to create the plasma in the plasma chamber, to cool the plasma chamber liner and pre-heat the recycle gas, and returning the pre-heated recycle gas to the plasma chamber to create the plasma.

Additional embodiments include: the method described above where the liner is graphite; the method described above where the recycle gas passes through at least one cooling channel present in the liner; the method described above where at least one of the cooling channels are covered with at least one removable liner/channel cover; the method described above where the cover is removed to remove any carbon deposits in the channels; the method described above where the carbon deposits are formed from the presence of hydrocarbons in the recycle gas; the method described above where at least one channel is formed in a spiral cooling channel pattern; the method described above where at least one channel is formed in a substantially straight cooling channel pattern; the method described above including more than one channel; the method described above including a plenum to aid in the production of an even distribution of cooling gas in the channels; the method described above including adding an oxidizing gas to the recycle gas to reduce or eliminate the presence of hydrocarbons in the recycle gas and/or reduce the formation of carbon deposits; the method described above where the oxidizing gas is steam and/or carbon dioxide; the method described above including passing an oxidizing gas through at least one of the channels to remove any carbon deposits in the channel; the method described above where the oxidizing gas is steam and/or carbon dioxide; the method described above where the carbon deposits are formed from the presence of hydrocarbons in the recycle gas; the method described above where the liner contains a plurality of perforations providing an ingress for the pre-heated recycle gas; the method described above where the perforations comprise one to six sets of co-planar perforations along the plasma chamber; the method described above where the plasma chamber is cylindrical and the perforations are along the curved sections of the plasma chamber cylinder; the method described above where the perforations allow aspirational cooling; the method described above where the plasma chamber contains a plasma torch annulus, and the gas is recycled to inside and/or outside the torch annulus; the method described above where the plasma is generated using an AC power source; the method described above where the plasma is generated using a DC power source; the method described above including injecting a hydrocarbon feedstock into the chamber such that over 30% of the energy input into the system measured in Joules is transferred to the hydrocarbon feedstock within the first 1 second of injection; the method described above where the hydrocarbon feedstock is natural gas; the method described above where the hydrocarbon feedstock is injected downstream of the plasma creation; and the method described above where the hydrocarbon feedstock is injected upstream of the plasma creation.

These, and additional embodiments, will be apparent from the following descriptions.

BRIEF DESCRIPTION OF THE DRAWINGS

The FIGS. 1, 2 and 3 show schematic representations of typical methods and apparatus described herein.

DETAILED DESCRIPTION

The particulars shown herein are by way of example and for purposes of illustrative discussion of the various embodiments of the present invention only and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the invention. In this regard, no attempt is made to show details of the invention in more detail than is necessary for a fundamental understanding of the invention, the description making apparent to those skilled in the art how the several forms of the invention may be embodied in practice.

The present invention will now be described by reference to more detailed embodiments. This invention may, however, be embodied in different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for describing particular embodiments only and is not intended to be limiting of the invention. As used in the description of the invention and the appended claims, the singular forms “a,” “an,” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. All publications, patent applications, patents, and other references mentioned herein are expressly incorporated by reference in their entirety.

Unless otherwise indicated, all numbers expressing quantities of ingredients, reaction conditions, and so forth used in the specification and claims are to be understood as being modified in all instances by the term “about.” Accordingly, unless indicated to the contrary, the numerical parameters set forth in the following specification and attached claims are approximations that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should be construed in light of the number of significant digits and ordinary rounding approaches.

Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements. Every numerical range given throughout this specification will include every narrower numerical range that falls within such broader numerical range, as if such narrower numerical ranges were all expressly written herein.

Additional advantages of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.

Heat transfer or cooling mechanisms in the past have typically been external to the plasma chamber. For the furnace process, the burner does not need excessive cooling because of the inherent lower temperatures in the furnace process compared to a plasma process. An example of what could be considered as inefficient cooling/pre-heat of recycle gas can be found in published patent application US2014/190,179. The heat exchanger is located external to the plasma chamber resulting in inefficient cool down or lack of cool down in plasma chamber and an insufficiently heated recycle/plasma gas.

As described herein, the use of regenerative cooling enables higher plasma temperatures to be used in chemical processes without generating excessive plasma chamber liner temperatures. Previous uses of plasmas to make carbon black, for example, either limited the plasma temperatures which could be used, or used water cooling to limit the loss of, for example, graphite when used in the process, e.g. as a liner, to sublimation. As described herein, recycle plasma gas is used to cool the lining, e.g. graphite, with the gas ultimately to be used in the plasma chamber.

Energy absorbed in cooling the liner is returned to the process as preheated gas used in the plasma chamber, which can represent significant energy cost savings to the overall process. As mentioned previously, in published patent application US2014/190,179, the heat transfer mechanism is external to the plasma chamber. The system described herein provides for a simultaneously cooled plasma chamber liner and heated recycle/plasma gas by engineering and incorporating the cooling mechanism into the inner skin of the liner itself. The gas cools the liner by heat-transfer contact with the liner along various places in or on the liner. In one embodiment, the gas flows in channels cut into the liner. In another embodiment, the cut channels are covered with a removable cover or seal. This use of a removable liner cover or seal enables easy replacement of the liner should it get too hot, for example, and also allows easy access to the channels for cleaning or whatever other maintenance may be needed. Instead of using recycled plasma gas as described herein and lowering temperatures inside the chamber, an alternative would be to run the torch at higher power density (increased power with the same gas flow). With the recycled plasma gas system as described herein turned on the result would be chamber temperatures similar to the lower power density case without the recycled plasma gas system being used as described herein. The advantage would be the gas leaves the chamber at a higher temperature, giving it more usable enthalpy per unit of power consumed, leading to a more thermally efficient process.

While the perforations are shown in FIG. 3 as regularly spaced circular holes, it should be noted that any openings that provide for the injection of the pre-heated recycle gas (such as hydrogen) into the plasma chamber can be used, e.g., random holes or perforations, zig-zag patterns, slit shaped perforations, etc. Similarly, the plasma chamber can be of any shape, such as cylindrical, and the perforations therefore would be along the curved sections of the cylindrical plasma chamber.

Should the cooling recycle gas contain trace amounts of hydrocarbons or other contaminants which lead to the formation of carbon or other deposits in the cooling channels, such deposits can be easily removed so as not to limit or otherwise interfere with the cooling in the liner which would be otherwise achieved. Steam, carbon dioxide and/or other oxidizing gases can also be added to the recycle gas to help reduce the amount of hydrocarbons or other contaminants which may be present in the recycle cooling gas, again, so as to reduce or eliminate the deposition of carbon or other contaminants in the cooling channels. In addition, if any deposited carbon or other contaminants are deposited in the channels, feeding steam, carbon dioxide and/or other oxidizing gas into the channels can also assist in eliminating any such deposits from the channels.

It is advantageous to obtain as uniform a cooling as possible in the liner, e.g., to avoid formation of “hot spots” in or on the liner. Accordingly, it is beneficial to subject the liner to as uniform and continuous a contact with cooling gas as possible, either externally and/or internally One embodiment for achieving a more even distribution of cooling gas is the use of one or more spiral cooling channels in the liners, although one or more straight, curved, or otherwise non-spiral channels can be used as well, either in combination or instead of spiral channels. If multiple channels are used, the use of a plenum to help provide an even distribution of the cooling gases within the channels is also beneficial.

The size and spacing of the channels will of course depend on the temperatures being generated in the plasma and/or reaction chambers, and the amount of cooling desired. Typical temperatures in the plasma chamber range from about 2500° C. to about 6000° C. and about 1200° C. to about 3000° C. in the reaction chamber. The channels are typically machined in as grooves, e.g., using conventional graphite cutting techniques and equipment, and are typically square or rectangular in cross section, and can be any size to accommodate the amount of cooling desired, e.g., 15 to 30 millimeters (mm) across and 50 to 100 mm deep.

Typically, between about 2 and about 20 MegaWatts of power are employed to create the plasma. The energy as measured in Joules will first be employed to create the plasma, and then be subsequently absorbed into the walls of the reactor, transferred to the plasma gas that did not go through the annulus or the plasma zone, and either immediately absorbed by the hydrocarbon or transferred to the injected hydrocarbon from the walls or from the plasma gas. The energy is absorbed by the hydrocarbon in the first one second after injection in the amount of at least 20%, 30%, or 40% or greater as measured in Joules. This energy can be absorbed from the electrodes, the plasma gas, the wall of the reactors, etc.

A perforated liner to enable aspirational cooling of the liner can also be used. Not only could this allow cooling gases to pass through the liner more uniformly, but it could also accelerate passage of gases in the hottest areas to dissipate heat more quickly, again to assist in attaining more uniform cooling. The pores present in the liner could either be drilled into the liner, or their formation incorporated into the process of manufacturing of the (porous) graphite used to form the liner.

Depending on the shape of the plasma assembly, the cooling gases can also be used in the torch annulus and/or outside of the torch annulus. Gas heated in the channels can be added to the plasma chamber or to the plasma gas which then flows through the annulus between the electrodes, i.e., since not all torches have an annulus, the recycle gas can be added to the plasma or mixed into the plasma after the arc. The torch annulus is defined as the space between two nested, concentric hollow cylinders that are used as the positive and negative electrodes of the torch.

As described herein, the cooling gases are used to cool the liner with the gas used in the plasma chamber, and in doing so preheat the gas used in the chamber, thereby reducing the amount of energy required to heat the plasma chamber gases to achieve a given temperature.

Referring to the Figures, which are schematic representations of systems described herein, conventional plasma gas (11, 21 and 31) such as oxygen, nitrogen, argon, helium, air, hydrogen, etc. (used alone or in mixtures of two or more) is injected into a plasma forming zone (12 and 22, and below the perforations 37 in FIG. 3) containing conventional plasma forming electrodes (10, 20 and 30) (which are typically made of copper, tungsten, graphite, molybdenum, silver etc.). The thus-formed plasma then enters into the reaction zone (13, 23 and 33) where it reacts/interacts with a carbon containing feedstock (14, 24 and 34) to generate a carbon black product. The liners (16, 26 and 36) can be any conventionally used material which can withstand the plasma forming temperatures, with graphite being preferred. Materials that can only withstand plasma forming temperatures with cooling may also be used. As shown, the recycle cooling gas flows through the cooling channels (15, 25 and 35), cooling the liner (16, 26 and 36) and heating the gas. The heated gas then flows into the plasma arc (as all or part of stream 11) as demonstrated in FIG. 1 and/or mixes into the plasma gas (formed from stream 21) with the mixing occurring in the plasma zone (22) as demonstrated in FIG. 2, or through the perforations (37) shown in FIG. 3. The mixture then flows into the reaction zone (13, 23 and 33) to contact the feedstock gas (14, 24 and 34).

Adding the heated cooling gas into the plasma gas stream (11) could potentially cause problems for the arc formed between the electrodes (10), so in some cases it may not be desirable. In these instances, all of or a portion of the cooling gas can instead get added to the plasma zone (22 and through perforations 37), preferably along the inside of the liner so that the gas provides additional protection for the liner from the hot plasma gas. The mixture then flows into the reaction zone (23 and 33) to contact the feedstock gas (24 and 34). It should also be noted, that that the direction of flow shown for the cooling gases (15 in FIG. 1) can also be in a direction reverse of that shown. The desired direction of flow will be dependent on the radiation flux on the liner, which is in turn dependent on the actual geometry of the liner. Thus flow can be counter current to plasma gas flow, co-current and/or cross-flow. The pre-heated gas can be injected through a co-planar set of perforations or multiple sets of co-planar perforations. The upper section (38) of the perforated section of FIG. 3 can be cylindrical in shape, with the lower section (39) being a converging cone. Although not shown in FIG. 3, it should also be noted that the perforations can extend above the space in the plasma chamber occupied by the electrodes as well.

The Figures demonstrate liners with curved channels contained therein. However, it should be understood that the cooling of the liners can take place by simply passing the cooling recycle plasma gas along one or more surfaces of the liners (depending on liner design), or through the liner by virtue of the presence of one or more straight, curved, spiral or other shaped channels. Since there are numerous advantages associated with uniformity of cooling by and/or within the liner, if multiple channels are present in the liner, a plenum can be used to assist in leveling the flow into the respective channels to help produce more even heat distribution within the liner. The liners can also contain pores, or be porous, such that the cooling can take place as aspirational cooling. The size and shape of the liners, the pores and the cooling surfaces or channels will depend on the size and shapes of the plasma forming zone and reaction zone, the temperatures desired in each zone, the amount and rate of cooling desired, the specific plasma gas being used, etc. For example, the generation and use of plasma at temperatures in excess of 1000° C. are not uncommon, which is one reason temperature control can be important to the process.

The Figures show a narrowing plasma chamber that then expands to a larger area downstream of plasma generation. An alternative configuration can entail a plasma chamber that does not narrow, but can or cannot expand downstream of plasma generation. The regenerative cooling would still take place in the general vicinity of the plasma generation (plasma chamber). Additionally, the hydrocarbon injection can occur either upstream or downstream of the plasma generation and can be centrally injected rather than the side injection that is depicted in FIGS. 1, 2, and 3.

Acceptable hydrocarbon feedstock includes any chemical with formula C_nH_x or C_nH_xO_y where n is an integer, and x is between 1 and 2n+2, and y is between 0 and n. For example simple hydrocarbons such as: methane, ethane, propane, butane, etc. can be used, as well as aromatic feedstock such as benzene, toluene, methyl naphthalene, pyrolysis fuel oil, coal tar, coal, heavy oil, oil, bio-oil, bio-diesel, other biologically derived hydrocarbons, or the like. Also, unsaturated hydrodcarbon feedstocks can also be used, such as: ethylene, acetylene, butadiene, styrene and the like. Oxygenated hydrocarbons such as; ethanol, methanol, propanol, phenol, ether, and similar are also acceptable feedstocks. These examples are provided as non-limiting examples of acceptable hydrocarbon feedstocks which can further be combined and/or mixed with other acceptable components for manufacture. Hydrocarbon feedstock referred to herein, means that the majority of the feedstock is hydrocarbon in nature. A preferred hydrocarbon feedstock for this process is natural gas.

The recycle plasma gas is flowed through the channels in the liner which in addition to reducing the temperatures in the plasma and/or reaction chambers, raises the temperature of the cooling gas as well. After being heated, the recycle plasma gas is then used as is or mixed with the plasma gas being injected into the plasma zone. As can be appreciated, this pre-heating of the plasma gas can provide significant energy costs savings to the process.

In one embodiment, the channels are open and accessible, but covered or sealed during use. This accessibility facilitates such things as repair and replacement of the liners, and/or cleaning of the channels. For example, the plasma gas can contain hydrocarbons or other contaminants. At the high temperatures experienced in typical plasma processes, carbon or other deposits can end up on the liner or in the channels or pores. A removable cover or seal can facilitate the cleaning of such deposits. The covers are typically made of the same material as the liners, but can also be made of a porous material (e.g., carbon fibers, graphite foam, etc).

Even without the covers or seals described above, another way to reduce or eliminate such deposits from the channels, is to add an oxidizing gas to the plasma forming gas prior to entry into the cooling channel. Similarly, an oxidizing gas can be simply run through the channels for the same purpose. Exemplary oxidizing gases could be steam and/or carbon dioxide, for example.

In some cases, the plasma forming zone may contain a conventional plasma torch annulus, as shown schematically in FIG. 1, e.g., having a cathode (11), anode (12), plasma or carrier working gas (10) and plasma jet region (13). In such cases, the cooling recycle plasma gas may be flowed inside or outside the torch annulus, i.e., the plasma recycle gas can be added to the carrier working gas stream (10), or added to the plasma jet region (13).

In another set of cases, AC or DC power can be used to form the plasma. Examples of an AC plasma system can be found in U.S. Pat. No. 7,452,514, for example. The AC system can utilize a plurality of electrodes that has the advantage of more efficient energy consumption as well as reduced heat load at the electrode surface. Examples of a suitable DC plasma system can be found, for example, in U.S. Pat. No. 7,462,343, and the references therein.

Example 1

Hydrogen gas is run through a conventional plasma torch electrode assembly in a plasma forming zone. Graphite liners with cooling channels line the plasma forming zone. As can be seen in the Table below, the average temperature of the plasma chamber wall is 2640 K and the maximum temperature is 3210 K. Through the diversion of 10%, 20%, and 30% of the total recycle gas, which is greater than 90% H₂, the following examples B, C, and D show a significant decrease in plasma wall temperature. For diversion of 30% of the total recycle gas the average temperature at the plasma wall is reduced from 2640 K to 2450 K and the maximum temperature is reduced from 3210 K to 3040 K. Each of these examples is with a heat input through the plasma torch of 750 KW (kilo watts) and a plasma gas flow rate of 340 Nm³/hr (normal cubic meter/hour) of hydrogen.

TABLE
	Hydrogen Gas at %	Average	Maximum
Example	of total	Temperature (K)	Temperature (K)
A	0	2640	3210
B	10	2490	3140
C	20	2470	3090
D	30	2450	3040

Thus, the scope of the invention shall include all modifications and variations that may fall within the scope of the attached claims. Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.

Claims

1. A method of cooling a liner in a plasma chamber, comprising: providing at least one recycle gas from the plasma chamber;contacting the liner with or passing through the liner the at least one recycle gas to cool the liner and pre-heat the at least one recycle gas to generate a pre-heated recycle gas; anddirecting the pre-heated recycle gas to the plasma chamber to create a plasma.

2. The method of claim 1, wherein the liner is graphite.

3. The method of claim 1, wherein the at least one recycle gas passes through at least one cooling channel present in the liner.

4. The method of claim 3, wherein a cooling channel of the at least one cooling channel is covered with at least one removable liner cover or channel cover.

5. The method of claim 4, wherein the at least one removable liner cover or channel cover is removed to remove any carbon deposits in the cooling channel.

6. The method of claim 5, wherein the carbon deposits are formed from a presence of hydrocarbons in the at least one recycle gas.

7. The method of claim 3, wherein a cooling channel of the at least one cooling channel is formed in a spiral cooling channel pattern.

8. The method of claim 3, wherein a cooling channel of the at least one cooling channel is formed in a substantially straight cooling channel pattern.

9. The method of claim 3, including more than one cooling channel.

10. The method of claim 9, including a plenum to aid in the production of an even distribution of cooling gas in the more than one cooling channel.

11. The method of claim 3, including adding an oxidizing gas to the at least one recycle gas to reduce or eliminate a presence of hydrocarbons in the at least one recycle gas and/or reduce the formation of carbon deposits.

12. The method of claim 11, wherein the oxidizing gas is steam and/or carbon dioxide.

13. The method of claim 3, including passing an oxidizing gas through a cooling channel of the at least one cooling channel to remove any carbon deposits in the cooling channel.

14. The method of claim 13, wherein the oxidizing gas is steam and/or carbon dioxide.

15. The method of claim 13, wherein the carbon deposits are formed from a presence of hydrocarbons in the at least one recycle gas.

16. The method of claim 1, wherein the liner contains a plurality of perforations providing an ingress for the pre-heated recycle gas.

17. The method of claim 16, wherein the perforations comprise one to six sets of co-planar perforations along the plasma chamber.

18. The method of claim 16, wherein the plasma chamber is cylindrical, and wherein the perforations are along curved sections of the plasma chamber cylinder.

19. The method of claim 16, wherein the perforations allow aspirational cooling.

20. The method of claim 1, wherein the plasma chamber contains a plasma torch annulus, and wherein the at least one recycle gas is recycled to inside and/or outside of the plasma torch annulus.

21. The method of claim 1, wherein the plasma is generated using an AC power source.

22. The method of claim 1, wherein the plasma is generated using a DC power source.

23. The method of claim 1, including injecting a hydrocarbon feedstock into the plasma chamber such that over 30% of the energy input into the system measured in joules is transferred to the hydrocarbon feedstock within the first 1 second of injection.

24. The method of claim 23, the hydrocarbon feedstock is natural gas.

25. The method of claim 23, the hydrocarbon feedstock is injected downstream of the plasma creation.

26. The method of claim 23, wherein the hydrocarbon feedstock is injected upstream of the plasma creation.