The embodiments presented relate to an expeditionary solid waste disposal system configured to improve logistics and enable it to be readily deployed in a military or civilian environment.
Many workforce camps, humanitarian and refugees' camps and military bases have difficulty safely and efficiently disposing of solid waste. The logistical challenges presented by the austere locations and often severe climatic conditions have made traditionally configured incinerators impractical. Without the option for better methods many have been forced to utilize crude and polluting disposal methods such as burn pits and small, ineffective incinerators that were not purpose-built.
In particular, rural and limited-access regions, have less infrastructure and cannot properly dispose of waste. Land disposal of waste is not appropriate in many areas due to topographic, hydrogeological, and/or climatic conditions. If waste is not properly disposed of, serious health conditions and environmental impacts may arise. Incinerators offer a possible solution. However, many current systems are difficult to transport and require too many resources which are not available in remote locations.
This summary is provided to introduce a variety of concepts in a simplified form that is further disclosed in the detailed description. This summary is not intended to identify key or essential inventive concepts of the claimed subject matter, nor is it intended for determining the scope of the claimed subject matter.
Embodiments described herein provide an expeditionary solid waste disposal system configured to resemble a standard-type shipping container and having the physical characteristics that allow it to meet ISO (international standards organization) transportation requirements (i.e., iso-container) to enable transport using multiple modes and convenient assembly. The presented embodiments provide a portable and readily assemblable apparatus comprised of a plurality of combustion chambers which may be aligned and connected using integrated ISO corner blocks, four-way forklift pockets, container connecting/locking devices and slide rail mechanisms within a portion thereof. The plurality of combustion chambers is configured to provide a multi-stage close coupled gasification, followed by oxidation of the gaseous effluent then direction of the gases to either the main exhaust stack or heat recovery module, if being used.
In one aspect, the front side is approximately 2,438 millimeters in width. Further, the right-side wall is opposite to a left side wall that has a length of 1,969 millimeters and includes a height of approximately 2,438 millimeters.
In one aspect, the apparatus is ISO-certified to allow for 9-high stacking during marine transportation. The apparatus is also able to operate or be stored in harsh conditions including high-moisture, corrosive, extreme heat, extreme cold, desert sands, and windy environments without corrosion or degradation.
In one aspect, the apparatus enables an integrated mating duct between a first and second chamber to allow fluid to flow between a first chamber and second chamber under natural draft created by the exhaust stack or by induced draft created by a variable speed motor blower. A primary burner and a primary blower (i.e., fan) are in communication with the first combustion chamber and a secondary burner and secondary blower (i.e., fan) are in communication with the second combustion chamber.
In one aspect, in some embodiments the control panel includes a switch to turn on or off the blackout operation mode. In blackout mode the no electronic lights will be emitted, and audio sounds will be disabled at a minimum.
In one aspect, the apparatus is configured to be transported by an aircraft, a shipping vessel, a train, or a vehicle. Further, the apparatus can be lifted using a forklift during an operation, transport, or storage configuration.
In another aspect, the exhaust stack is stackable for use and unstackable for storage
The fuel bladder is collapsible for storage and fillable for use, using standard methods of fuel transfer.
Other aspects, advantages, and novel features of the embodiments will become apparent from the following detailed description in conjunction with the drawings.
A more complete understanding of the embodiments and the advantages and features thereof will be more readily understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:
The specific details of the single embodiment or variety of embodiments described herein are to the described system and methods of use. Any specific details of the embodiments are used for demonstration purposes only and not unnecessary limitations or inferences are to be understood therefrom.
Before describing in detail exemplary embodiments, it is noted that the embodiments reside primarily in combinations of components related to the system and method. Accordingly, the system components have been represented where appropriate by conventional symbols in the drawings, showing only those specific details that are pertinent to understanding the embodiments of the present disclosure so as not to obscure the disclosure with details that will be readily apparent to those of ordinary skill in the art having the benefit of the description herein.
As used herein, relational terms, such as “first” and “second” and the like, may be used solely to distinguish one entity or element from another entity or element without necessarily requiring or implying any physical or logical relationship or order between such entities or elements.
Specifically, the apparatus enables gasification and oxidation using a plurality of proprietary combustion chambers connected via an air duct and controlled using burners, variable speed blower, air dampers and microprocessor-controlled automation which enables two-stage gasification and oxidation.
The embodiments provide a highly portable and readily assemblable containerized waste conversion apparatus which enables recovered heat from gaseous effluent to be converted to a plurality of energy sources using releasably attached energy generation systems. The apparatus includes at least a primary and secondary combustion chamber, breech/control chamber, and heat recovery module chamber which are releasably secured to one another using a locking mechanism and collectively affixed to an integrated skid type base. The apparatus is designed to enable a single person with a forklift operator to releasably attach each iso-container using the container connecting devices, and releasably attach each interconnecting air duct, and blower and burner using an integrated slide rail system, quick connection cables and hoses without the need for a crane.
The apparatus is controlled by a microcontroller having integrated storage and remotely connected to the main control panel housed within the control chamber. During operations, an operator may batch load up to 1000 pounds of waste per day within the first combustion chamber which provides for over a 96 percent reduction of the load waste mass. Upon completion of the time gasification/oxidation (i.e., burn cycle), the apparatus initiates a cool-down mode, once completed an operator is allowed to open the door to remove the ash collected. The door, in some embodiments includes a temperature-controlled door lock that prevents a person from being able to open the door until the internal temperature is below 90 degrees Celcius. The waste can include mixed, unsorted, non-hazardous solid waste on a consecutive daily basis including time for cooling between batches and routine maintenance such as ash removal activities.
In contrast to the present embodiments, traditional mobile waste processing systems are typically housed within a single 20-foot iso container and often require manual sorting of the solid waste before it is placed within a shredder for further mass reduction and homogeneity. The traditional system, which is constructed then housed within a commercial shipping container, is not able to utilize to entire shipping envelope as space for waste processing capacity or the oxidation of the gases. Therefore, inherent to the traditional design is a loss of up a minimum of 10% and up to 40% of the available shipping volume due to the redundancy of the outer shipping container. The apparatus has a unique construction whereby the wall of the primary and secondary combustion chambers are also the outer wall of the container and it is outfitted with all of the required shipping container features but without the addition of an outer shipping container, maximizing the internal volumes for the device allowing it process more waste and oxidize more gaseous by-products than is possible within the traditional configuration.
Referring now to the drawings wherein like referenced numerals designate identical or corresponding parts throughout the views. There is shown in
The plurality of chambers 12 further includes at least a first combustion chamber 20, a second combustion chamber 40, a control chamber 30. Each of the plurality of equilateral dimensioned chambers 12 is approximately 8.0 feet wide, 6′ feet and 5½ inches long, and 8.0 high with a steel exterior for strength coupled with lightweight insulating materials which reduce the weight of each compartment to 7,500-10,000 lbs.
The first combustion chamber 20 includes a ceramic fiber refractory lining 23 (further illustrated in
A fuel tank which supplies the primary burner 24 and secondary burner 41 collapsible fuel tank that stores within the first combustion chamber 20.
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During the gasification process, the loaded solid waste is first dried to remove any moisture within the waste and then begin to decompose any contained organic molecules to form a gas vapor composed of water, carbon monoxide, carbon dioxide, hydrogen, methane, and ethane, etc. Once the gasification process is complete, any remaining solid waste is removed along with the ash collected along the ceramic firebrick floor surface 27 and under the removable metal grate 28.
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In some embodiments, the main exhaust stack 50 emits no visible emissions during operation and is shown to have low in-stack emissions. When the waste mixture is thermally destroyed, the remaining ash has no toxicity characteristics as defined by the US Environmental Protection Agency (EPA) regulations when subjected to the toxicity characteristic leachate procedure (TCLP).
Once the close-coupled gasification within the first 20 and second combustion chambers 40 are complete, the microcontroller 16 initiates a pre-programmed cool down cycle using the primary blower 25 and secondary blower 42 to exhaust any residue gas. Similar to the burn cycle which is operated with a countdown timer, the cool-down mode may be pre-programmed for a pre-selected period of time-based on factors such as operational tempo, climate, and operating conditions. For example, if the apparatus 10 is transported to a cold environment with minimal waste, both the burn cycle and cool down period may be shortened to preserve fuel consumption. Conversely, if transported to a tropical environment, the cooldown period may be extended to account for the warmer temperatures. Suitable fuels include diesel, or JP-8 fuel stored within the self-contained fuel system. The fuel bladder can be folded into the interior of the apparatus 10 during transportation.
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Each iso-container utilized for the apparatus 10 is a certified ISO shipping container which meets all ISO 1496 requirements and U.S. Coast Guard requirements for safe containers. Each container can be transported via air, sea, rail, and ground and can be stacked nine containers high according to ISO standards. Each corner fitting conforms to ISO 1161 standards.
In some embodiments, the apparatus 10 is capable of being shipped by C-130 aircraft, CH-47D helicopter, CH-53 helicopter, or a sealift. The apparatus 10 may also be transported via integration with a military flat rack and loading onto a transport vehicle. To facilitate air transportation, the apparatus 10 is suitably balanced to facilitate lifting.
The apparatus 10 includes pressure regulation devices to control pressure differential during transportation. The apparatus 10 can regulate pressure during rapid decompression while in-flight, such a pressure drop of 8.3 PSI within 0.5 seconds or less.
The configuration of the apparatus 10 allows for full assembly by two or more untrained individuals within 8 hours.
In some embodiments, once fully assembled the apparatus 10 can be position in an area measuring 20 feet by 40 feet or less. The area includes a buffer zone for waste loading, safety, and fuel storage. The ground where setup is executed should be less than a 6 percent grade.
In some embodiments, the apparatus 10 includes vapor-proof and shatterproof lighting to allow nighttime operation and maintenance. The apparatus 10 further includes internal blackout capability to allow operation during blackout conditions. The blackout lighting components are capable of being set as a default operation mode.
In some embodiments, the apparatus 10 is provided with a plurality of fire extinguishers equipped with a tamperproof seal. The fire extinguishers may be rated for temperatures between −65-120° F.
In some embodiments, the exterior surface of each iso-container is chemical agent resistant painted to limit degradation and enhance safety. The apparatus 10 is capable of maintaining full operation during transportation, while stationary, or following long-term storage in harsh environments, such as a marine salt fog environment, without experiencing corrosion, rust, or similar forms of degradation. The apparatus 10 can withstand exposure to high-moisture environments without experiencing swelling, structural deterioration, operational failures, alterations, or other deformations.
Surfaces which experience temperatures above 140° F. as a result of inadvertent contact or 125° F. during handling as a result of incinerator function are appropriately guarded for contact by personnel.
Many different embodiments have been disclosed herein, in connection with the above description and the drawings. It will be understood that it would be unduly repetitious and obfuscating to literally describe and illustrate every combination and subcombination of these embodiments. Accordingly, all embodiments can be combined in any way and/or combination, and the present specification, including the drawings, shall be construed to constitute a complete written description of all combinations and subcombinations of the embodiments described herein, and of the manner and process of making and using them, and shall support claims to any such combination or subcombination.
An equivalent substitution of two or more elements can be made for any one of the elements in the claims below or that a single element can be substituted for two or more elements in a claim. Although elements can be described above as acting in certain combinations and even initially claimed as such, it is to be expressly understood that one or more elements from a claimed combination can in some cases be excised from the combination and that the claimed combination can be directed to a subcombination or variation of a subcombination.
It will be appreciated by persons skilled in the art that the present embodiment is not limited to what has been particularly shown and described hereinabove. A variety of modifications and variations are possible in light of the above teachings without departing from the following claims.