The use of a safe, complete, and environmentally benign process is useful in the disposal of chemical weapons (CW) stockpile. The conventional method of disposal uses incineration technology. However, conventional incineration technology faces legal, social, and political obstacles.
The conventional incineration process produces a large volume of off gas, which is further treated with pollution abatement equipment such as a quench tower, a scrubber, a demister, and a baghouse for particulate removal. Hence, incineration plants are not suitable for mobile units. Additionally, incineration plants are typically housed in a building such as a facility relatively close to the stockpile, creating inherent risks for personnel who work at the facility. Alternatively, dangerous stockpile chemicals are transported from the stockpile to the incineration facility, creating risks related to potential transportation accidents.
As a result of the incineration process, harmful dioxins are produced due to poor mixing and short residence time at the operating temperature, as well as prolonged exposure at temperatures that favor the formation of dioxins. The production of dioxins presents a major environmental challenge.
Neutralization is an alternative technology for the destruction of toxic chemicals. However, the neutralization process has been abandoned by the U.S. Army due to its complexity, more problematic waste produced by the process, cost, and analytical problems in certifying the treated waste as agent-free.
Conventional plasma arc technology has also been evaluated for the destruction of such waste. Using conventional plasma arc technology, waste is atomized in a high temperature (e.g., 5,000° C. to 15,000° C.) pyrolysis chamber. The resulting gases are scrubbed and combusted with air. While this process is amenable to a transportable unit, the primary limitation is that high temperature requires high power input and forms undesirable products, as explained above.
Embodiments of a method are described. In one embodiment, the method is a method for oxidizing a combustible material. An embodiment of the method includes introducing a volume of the combustible material into a plasma zone of a gliding electric arc oxidation system and introducing a volume of oxidizer into the plasma zone of the gliding electric arc oxidation system. The volume of oxidizer includes a stoichiometrically excessive amount of oxygen. The method also includes generating an electrical discharge between electrodes within the plasma zone of the gliding electric arc oxidation system to oxidize the combustible material. Other embodiments of the method are also described.
Embodiments of a system are also described. In one embodiment, the system is a system to oxidize a combustible material. An embodiment of the system includes at least one channel to direct the combustible material and an oxidizer into a plasma zone of a plasma generator and an oxygen controller to control an amount of oxygen of the oxidizer into the plasma zone of the plasma generator. The oxygen controller is configured to provide a stoichiometrically excessive amount of oxygen. The system also includes a plurality of electrodes within the plasma zone of the plasma generator. The plurality of electrodes are configured to generate a plasma to oxidize the combustible material. Other embodiments of the system are also described.
Embodiments of an apparatus are also described. In one embodiment, the apparatus is an oxidation apparatus. An embodiment of the oxidation apparatus includes means for introducing a combustible material into a plasma zone of a plasma generator, means for introducing a stoichiometrically excessive amount of oxygen into the plasma zone of the plasma generator, and means for oxidizing substantially all of the combustible material to render a harmful chemical into a safe material for disposal. Other embodiments of the apparatus are also described.
Other aspects and advantages of embodiments of the present invention will become apparent from the following detailed description, taken in conjunction with the accompanying drawings, which are illustrated by way of example of the various principles and embodiments of the invention.
Throughout the description, similar reference numbers may be used to identify similar elements.
In the following description, specific details of various embodiments are provided. However, some embodiments may be practiced with less than all of these specific details. In other instances, certain methods, procedures, components, structures, and/or functions are described in no more detail than to enable the various embodiments of the invention, for the sake of brevity and clarity.
In one embodiment, a material enters the explosion chamber 102 for incineration, or partial combustion. Incineration of particular materials produces off gases that can be toxic or otherwise harmful to people or the environment. For off gases and other incineration products that are combustible, the oxidation system 100 routes the combustible material from the explosion chamber 102 to the gliding electric arc oxidation system 104. In other embodiments, other types of combustible materials such as synthesis gas (also referred to as syngas) are routed to the gliding electric arc oxidation system 104.
For convenience, references to combustible materials encompass a variety of materials or chemical compositions that may be oxidized by the gliding electric arc oxidation system 104. The combustible material routed to the gliding electric arc oxidation system 104 may be in gas, liquid, or solid form. In one embodiment, the combustible material is a hydrocarbon. In another embodiment, the combustible material is a solid comprising primarily carbon. Additionally, some embodiments of the oxidation system 100 facilitate combining the combustible material with a carrier material. For example, the combustible material may be entrained with a liquid or gaseous carrier material.
It should be noted that some embodiments of the oxidation system 100 exclude the explosion chamber 102. In other words, the gliding electric arc oxidation system 104 may receive the combustible material from another source other than the explosion chamber 102. For example, in some embodiments, the combustible material may be processed directly by the gliding electric arc oxidation system 104, without any prior incineration, combustion, or other processing.
In one embodiment, the gliding electric arc oxidation system 104 is a high energy plasma arc system. Additionally, some embodiments of the gliding electric arc oxidation system 104 are referred to as non-thermal plasma systems because the process employed by the gliding electric arc oxidation system 104 does not provide a substantial heat input for the oxidation reaction.
In order to facilitate the oxidation process implemented by the gliding electric arc oxidation system 104, the oxidizer source 106 supplies an oxidizer, or oxidant, to the gliding electric arc oxidation system 104. In one embodiment, the oxidizer controller 108 controls the amount of oxidizer such as oxygen that is supplied to gliding electric arc oxidation system 104. For example, the oxidizer controller 108 may control the flow rate of the oxidizer from the oxidizer source 106 to the gliding electric arc oxidation system 104. The oxidizer may be air, oxygen, steam (H2O), or another type of oxidizer. Embodiments of the oxidizer controller 108 include a manually controlled valve, an electronically controlled valve, a pressure regulator, an orifice of specified dimensions, or another type of flow controller. Another embodiment of the controller incorporates an oxidant composition sensor feedback system.
In one embodiment, the oxidizer mixes with the combustible material within the gliding electric arc oxidation system 104. Alternatively, the combustible material and the oxidizer may be premixed before the mixture is injected into the gliding electric arc oxidation system 104. Additionally, the oxidizer, the combustible material, or a mixture of the oxidizer and the combustible material may be preheated prior to injection into the gliding electric arc oxidation system 104.
In general, the gliding electric arc oxidation system 104 oxidizes the combustible material and outputs an oxidation product that is free of harmful materials or substantially free of harmful materials. More specific details of the oxidation process are described below with reference to the following figures. It should be noted that the oxidation process depends, at least in part, on the amount of oxidizer that is combined with the combustible material and the temperature resulting from the heat released in the reaction. Partial oxidation, or reformation, of the combustible material produces a reformate product such as syngas. Reformation occurs when the amount of oxygen is less than a stoichiometric amount of oxygen. In some embodiments, 30-40% of stoichiometric oxygen levels are used to implement the reformation process. An exemplary reformation equation is:
Another exemplary reformation equation is:
In contrast, full oxidation (referred to simply as oxidation) of the combustible material produces an oxidation product. Full oxidation occurs when the amount of oxygen is more than a stoichiometric amount of oxygen. In some embodiments, 5-100% excess of stoichiometric oxygen levels are used to implement the oxidation process. An exemplary oxidation equation is:
Other equations may be used to describe other types of reformation and oxidation processes.
While reformation processes may be endothermic or exothermic, the oxidation process is exothermic. Hence, the reactants used in the oxidation process may not need to be preheated. Nevertheless, it may be useful to maintain part or all of the gliding electric arc oxidation system 104 at an operating temperature within an operating temperature range for efficient operation of the gliding electric arc oxidation system 104. In one embodiment, the gliding electric arc oxidation system 104 is mounted within a furnace (refer to
The illustrated oxidation system 110 shown in
In one embodiment, the combustible material (represented by CHn) and the oxidizer (represented by (1+n/4)O2) are introduced into the plasma zone 114, which includes a plasma generator (refer to
After ionization, the reactants pass to the post-plasma reaction zone 116, which facilitates homogenization of the oxidized composition. Within the post-plasma reaction zone 116, some of the reactants and the products of the reactants are oxygen rich while others are oxygen lean. A homogenization material such as a solid state oxygen storage compound within the post-plasma reaction zone 116 acts as a chemical buffering compound to physically mix, or homogenize, the oxidation reactants and products. Hence, the oxygen storage compound absorbs oxygen from oxygen-rich packets and releases oxygen to oxygen-lean packets. This provides both spatial and temporal mixing of the reactants to help the reaction continue to completion. In some embodiments, the post-plasma reaction zone 116 also facilitates equilibration of gas species and transfer of heat.
The heat transfer zone 118 also facilitates heat transfer from the oxidation product to the surrounding environment. In some embodiments, the heat transfer zone 118 is implemented with passive heat transfer components which transfer heat, for example, from the oxidation product to the homogenization material and to the physical components (e.g., housing) of the gliding electrical arc oxidation system 104. Other embodiments use active heat transfer components to implement the heat transfer zone 118. For example, forced air over the exterior surface of a housing of the gliding electric arc oxidation system 104 may facilitate heat transfer from the housing to the nearby air currents. As another example, an active stream of a cooling medium may be used to quench an oxidation product.
The electrical signals on the electrodes 122 produce a high electrical field gradient between each pair of electrodes 122. For example, if there is a separation of 2 millimeters between a pair of electrodes 122, the electrical potential between the electrodes 122 is about 6-9 kV.
The mixture of the combustible material and the oxidizer enters and flows axially through the plasma generator 120 (in the direction indicated by the arrow). The high voltage between the electrodes 122 ionizes the mixture of reactants, which allows current to flow between the electrodes 122 in the form of an arc 124, as shown in
Due to the flow of the mixture into the plasma generator 120, the ionized particles are forced downstream, as shown in
Eventually, the gap between the electrodes 122 becomes wide enough that the current ceases to flow between the electrodes 122. However, the ionized particles continue to move downstream under the influence of the mixture. Once the current stops flowing between the electrodes 122, the electrical potential increases on the electrodes 122 until the current arcs again, as shown in
In order to introduce the combustible material and the oxidizer into the plasma generator 120, the gliding electric arc oxidation system 130 includes multiple channels, or conduits. In the illustrated embodiment, the gliding electric arc oxidation system 130 includes a first channel 138 for the combustible material and a second channel 140 for the oxidizer. The first and second channels 138 and 140 join at a mixing manifold 142, which facilitates premixing of the combustible material and the oxidizer. In other embodiments, the combustible material and the oxidizer may be introduced separately into the plasma generator 120. Additionally, the locations of the first and second channels 138 and 140 may be arranged in a different configuration.
In order to contain the reactants during the oxidation process, and to contain the oxidation product resulting from the oxidation process, the plasma generator 120 and the housing 134 may be placed within an outer shell 144. In one embodiment, the outer shell 144 facilitates heat transfer to and/or from the gliding electric arc oxidation system 130. Additionally, the outer shell 144 is fabricated from steel or another material having sufficient strength and stability at the operating temperatures of the gliding electric arc oxidation system 130.
In order to remove the oxidation product (e.g., including any carbon dioxide, steam, etc.) from the annular region 146 of the outer shell 144, the gliding electric arc oxidation system 130 includes an exhaust channel 148. In one embodiment, the exhaust channel is coupled to a collector ring manifold 150 that circumscribes the housing 134 and has one or more openings to allow the oxidation product to flow to the exhaust channel 148. In the illustrated embodiment, the oxidation product is exhausted out the exhaust channel 148 at approximately the same end as the intake channels 138 and 140 for the combustible material and the oxidizer. This configuration may facilitate easy maintenance of the gliding electric arc oxidizer system 130 since all of the inlet, outlet, and electrical connections are in about the same place. Other embodiments of the gliding electric arc oxidation system 130 may have alternative configurations to exhaust the oxidation products from the outer shell 144.
The illustrated gliding electric arc oxidation system 160 of
In addition to the heat transfer from the oxidation product to the wall of the housing 134, the gliding electric arc oxidation system 160 also may facilitate heat transfer away from the housing 134 by flowing a coolant through the annular region 146 of the outer shell 144. The coolant may be a gas or a liquid. For example, the coolant may be air. Although not shown in detail, the coolant may be circulated within or exhausted from the outer shell 144.
The illustrated gliding electric arc oxidation system 160 also includes a homogenization material 166 located in the channel 136 of the housing 134. The homogenization material 166 serves one or more of a variety of functions. In some embodiments, the homogenization material 166 facilitates homogenization of the oxidation product by transferring oxygen from the oxidizer to the combustible material. In some embodiments, the homogenization material 166 also provides both spatial and temporal mixing of the reactants to help the reaction continue to completion. In some embodiments, the homogenization material 166 also facilitates equilibration of gas species. In some embodiments, the homogenization material 166 also facilitates heat transfer, for example, from the oxidation product to the homogenization material 166 and from the homogenization material 166 to the housing 134. In some embodiments, the homogenization material 166 may provide additional functionality.
The illustrated gliding electric arc oxidation system 160 also includes a ceramic insulator 168 to electrically insulate the electrodes 122 from the housing 134. Alternatively, the gliding electric arc oxidation system 160 may include an air gap between the electrodes 122 and the housing 134. While the dimensions of the air gap may vary in different implementations depending on the operating electrical properties and the fabrication materials used, the air gap should be sufficient to provide electrical isolation between the electrodes 122 and the housing 134 so that electrical current does not arc from the electrodes 122 to the housing 134.
In some embodiments, the bottom mounting plate 184 may be removed from the flanges 172 and 174 to remove the mixing manifold 142 and the electrodes 122 from the housing 134 and the outer shell 144. Additionally, in some embodiments, one or more notches 190 are formed in the bottom mounting plate 184 to facilitate proper alignment of the mixing manifold 142 with the channels 138 and 140.
As an example of operation of an embodiment of the gliding electric arc oxidation system 130, a gas composition containing 35% hydrogen, 30% carbon monoxide, 20% nitrogen, 5% methane, and 8% carbon dioxide may be used as a combustible material. This gas composition is representative of at least some incineration products resulting from chemical munitions explosions.
In one embodiment, the gliding electric arc oxidation system 130 is initially heated by introducing a mixture of a gaseous hydrocarbon and air. Exemplary gaseous hydrocarbons include natural gas, liquefied petroleum gas (LPG), propane, methane, and butane. Once the temperature of the gliding electric arc oxidation system 130 reaches an operating temperature of about 800° C., the flow of the gaseous hydrocarbon is turned off and raw gas is introduced. The flow rates of air and raw gas are adjusted to maintain proper stoichiometric ratio, while the total flow is adjusted to maintain the plasma generator 120 at a particular operating temperature or within an operating temperature range.
As an alternative, oxygen may be used instead of air in order to lower the overall volume of oxidized gas. Additionally, air may be used to cool the gliding electric arc oxidation system 130 while oxygen is introduced with the combustible material to fully oxidize the combustible material.
Reference throughout this specification to “one embodiment,” “an embodiment,” or similar language means that the described feature, operation, structure, or characteristic may be implemented in at least one embodiment. Thus, the phrases “in one embodiment,” “in an embodiment,” and similar phrases throughout this specification may, but do not necessarily, refer to the same embodiment.
Furthermore, the described features, operations, structures, or characteristics of the described embodiments may be combined in any suitable manner. Hence, the numerous details provided here, such as examples of electrode configurations, housing configurations, substrate configurations, channel configurations, catalyst configurations, and so forth, provide an understanding of several embodiments of the invention. However, some embodiments may be practiced without one or more of the specific details, or with other features operations, components, materials, and so forth. In other instances, well-known structures, materials, or operations are not shown or described in at least some of the figures for the sake of brevity and clarity.
Although specific embodiments of the invention have been described and illustrated, the invention is not to be limited to the specific forms or arrangements of parts so described and illustrated. The scope of the invention is to be defined by the claims appended hereto and their equivalents.
This application claims the benefit of U.S. Provisional Application No. 60/807,363, filed on Jul. 14, 2006, which is incorporated by reference herein in its entirety.
Number | Date | Country | |
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60807363 | Jul 2006 | US |