A PILOT PLANT STUDY OF SYNTHESIS INTERMEDIATES FROM FEEDLOT WASTE by ROGER LEE PETERSON, B. S. in Ch.E. A THESIS m CHEMICAL ENGINEERING Submitted to the Graduate Faculty of Texas Tech University in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE IN CHEMICAL ENGINEERING Approved December, 1975 ^0' r ACKNOWLEDGMENTS The Author wishes to thank Don Carlisile, Gerald Grusendorf and the other undergraduates that helped during the construction and operation of the project. My thanks also to Henry Burchett for his help and advice. The financial support of Pioneer Natural Gas CO., The Environmental Protection Agency, and the Texas Cattle Feedlot Association is gratefully acknowledged. A note of thanks also to Phillips Petroleum Co. whose fellowship grant was greatly appreciated. n CONTENTS ACKNOWLEDGMENTS ii LIST OF TABLES v LIST OF FIGURES vi I. INTRODUCTION 1 II. LITERATURE REVIEW 3 III. CONSTRUCTION, MODIFICATIONS AND PROCEDURES 6 Concept 6 Reactor and Feed Hopper 6 ^ 'Char Hopper and Ram Reactor Heaters 10 Preheater 11 Instrumentation and Controls 12 Down-Stream System 1^ Modifications 19 Feed Hopper 15 Cyclone and Filter 20 : Water-Gas Separation 23 Flow Measurement System 24 Operational Procedure 24 Analytical Procedures 25 Preparation of Feedstock 27 m IV... DISCUSSION OF RESULTS V. VI. 28 Feed Considerations 28 Experimental Conditions and Results 31 Reactor Operating Characteristics 33 Downstream Operating Characteristics 51 Feed Particle Size 53 Char Characteristics 55 fluidized Bed and Char Hopper Characteristics 56 Reactor Temperature Control 57 Data Reliability 58 Early Runs 59 Proposed Modifications 61 CONCLUSIONS 65 RECOMMENDATIONS 66 LITERATURE CITED 67 APPENDIX 69 A.. Sample Calculations for Normalization of Data 70 B. Discussion of Proposed Reactor Design 72 C. Raw Data 74 D. Supplemental Data 77 rv LIST OF TABLES Table 1. Typical Operating Values and Results for the Pilot Plant Reactor 32 2. Mass Balances 46 3. First Run Data 60 LIST OF FIGURES Figure 1. Dimensions of Reactor 7 2. Char Hopper and Fluidization Plate 9 3. Electrical System 15 4. Original System Configuration 16 5. Final System Configuration 17 6. Cyclone Dimensions 22 7. Temperature Profiles in Reactor 34 8. Raw Gas Production 37 9. Effect of Temperature on Normalized Gas Production 39 10. Small Scale Reactor Normalized Gas Production 40 11. Raw Gas Composition (Methane and Ethane) 42 12. Raw Gas Composition (Hydrogen and Ethylene) 43 13. Reactor Effluent Gas Composition 44 14. Small Scale Reactor Gas Composition 45 15. Average Temperature Comparison to Small Scale Reactor 49 16. Effect of Particle Size on Degree of Reaction 54 17. Wet Steam Condenser Design 64 18. Proposed Reactor Design 73 VI • INTRODUCTION In the VJest Texas area almost 5 million head of cattle are fed in feedlots annually. manure a day.^ Each cow produces about 5 to 9 pounds of Historically bovine wastes have been returned to the soil by the farmer to act as natural fertilizer. However, syn- thetic fertilizers have become very attractive to the farmer because of the ease of application, the absence of odor, the availability, and the lack of insect pests and weeds. At the same time feedlots have become larger and more centralized so that it may be more eco- f nomical for the farmer to use the more expensive synthetic fertilizers than to pay for hauling the bulky manure to his fields. Thus, the feedlot owner has experienced long periods in the past when he had no economical way to dispose of his waste material depending upon the local price of synthetic fertilizer. In common practice, the manure accumulates in large piles on unused portions of the feedlot. Since the Environmental Protection Agency has pro- mulgated a regulation stating that feedlot runoff cannot be discharged into the waters of the United States except runoff resulting from chronic or catastrophic precipitation, it is probably more economical for the feedlot owner to dispose of his wastes rather than try to contain them. The Chemical Engineering Department has a policy of trying to solve problems of the people and industries within the area served by the University. Thus, an opportunity was seen to solve the feedlot waste problem because the increasing costs of energy have made alternate souces of fuel and raw materials more attractive. Ttris study is the second phase of the manure disposal scheme which has come to be known as the Syn Gas project. The first phase was initiated in 1972 by a paper evaluating the possible uses for manure from a thermochemical standpoint ^ . A project v/as then f3) funded to construct and operate a bench scale reactor^ . The bench scale reactor produced very encouraging results which indicated that the production of ammonia synthesis gas (a 1 to 3 ratio of Nitrogen to Hydrogen) was feasible from feedlot wastes. To determine the actual feasibility of operating on a commercial basis and to provide scale up data, it was decided that a relatively large demonstration plant would be required. The details concerned with the construction and operational characteristics of this reactor system are intended to give a prospective design engineer an insight into the problems and behavior that can be expected in a commercial manure pyrolysis unit. Also, the data obtained from this study indicate some guidelines for the design of future solid waste reactors, along with new prospects for the utilization of manure. ^ LITERATURE REVIEW There are many possible solutions to the cattle feedlot waste problem. (4) A recent Environmental Protection Agency report ^ ' lists approximately 30 different methods including land utilization, containment, various sewage treatment schemes, production of single cell protein, feed recycling, chemical treatment and even production of protein from fly larvae. The work of Herzog ^ ' formed the basis and design criteria for this pilot plant project. Herzog's work is discussed and used for comparison later in this thesis. Herzog concluded that the partial oxidation of cattle manure if followed by desulfurization and reforming steps could result in a gas suitable for the synthesis of ammonia. There are several other studies concerning feedlot waste pyrolysis. The most complete study surveyed was the work of Garner and Smith ^ . This study imployed three, batch, bench-scale re- actors with a maximum temperature of 400-500°C. The mild heating rates (5 to 40^F/min) resulted in a gas production of only 26.1% by weight of the dry manure and 21.5% tarry volatile and low boiling organics. The average gas analysis was 3.6% H2, 10.9% N^, 12.9% CH., 16% CO, 38.9% CO^, 0.3% Zr^^^ and 1.8% CgHg. A complete lab- oratory analysis was done on the pyrolysates which resulted in the identification of a wide variety of alcohols, aldehydes, ketones, acids, amines and phenols as well as polyfunctional compounds. ever, stearic acid was the only significant fraction of the How- 4 pyrolysate recovered in pure enough form to enable positive identification. One interesting fact discovered was the loss of weight by pyrolysis was significantly inhibited when done in a vacuum as compared to an inert atmosphere at 14.7 psia. A cyclonic burner for manure-to-synthesis gas production was built by Natour ^ K The data generated from Natour's experiment is not easily compared to this study because a significant percentage of the generated gas was burned to fuel the pyrolysis. Natour did show that pyrolysis with partial oxidation could be sustained without adding outside heat. Grub indicated that the dry portion of manure consisted largely of undigested cellulose, hemicellulose, lignin and lignoprotein complexes. The pyrolysis of cellulose was studied and several mechanisms were proposed for its step by step degradation (9 10) ^ ' \ With cellulose an aqueous distillate began to form at 200^C and tar and gases were formed at 230-240°C ^^K tion becomes exothermic at 270°C^ ^ The reac- Gas production was greatest between 270-350°C^^^ Lignin from spruce exothermically decomposed at a higher temperature range (350-450°C) than the cellulose ' '. Pyrolysis of this lignin yielded more carbon and tar and less aqueous distillate than cellulose pyrolysis ^ . Young ^ ' has compiled the pyrolysis data for the various components of manure and shown that they can easily be used to fit manure pyrolysis data over a wery wide temperature range. Theoretical studies of manure pyrolysis have been conducted by Young in a parallel investigation with the large scale reector discussed in this thesis. Oiher studies have been directly supported or associated with the greater Syn-Gas project. (12) Khara ^ ' investigated the utilizaf3) tion and disposal of the char and ash obtained form Herzog's ^ ' small reactor. Massie ^ ' utilized a partial oxidation retort with manure as feed in an earlier study. Smith et al ^^^K This work was continued by Al-Haj-Ali ^^^' completed a study of the drying characteristics of manure. Thus, a considerable bulk of data has been assembled toward the development of manure pyrolysis technology. CONSTRUCTION, MODIFICATIONS AND PROCEDURES As with most developmental projects, the equipment and procedures were in a constant state of change throughout the course of the project. As more data becaijje available on the operating characteristics of the system various modifications were initiated to increase reliability, improve the accuracy, remove limitations, and enhance understanding of the data. Concept Manure was added into the top of the hot reactor where it fell to the bottom countercurrent to a stream of steam and air introduced through a distribution plate at the bottom. Gases resulting from tli'3 pyrolysis and partial oxidation of the manure exited with the input gas stream out the top of the reactor. The gas was stripped of entrained solids, tars and condensables in stages and composition and flow rate data were taken for the gas stream. Char was removed from the bottom of the reactor through an opening in the input gas distribution plate. Reactor and Feed Hopper The reactor was made from schedule 40 stainless steel pipe (see Figure 1). A 6 inch diameter, 5 foot long section composed the main body of the reactor and an 8 inch diameter, 2 foot long section was used at the top of the reactor for a fluidized bed expansion section to allow separation of the solids and gas. In order to 900- RF m flng. stainless steel schedule 40 pipe stainless steel STD. WT. weld cap stainless steel 1'- schedule 40 pipe stainless steel 8" X 6" - concentric reducer stainless steel 8'-0" schedule 40 pipe stainless steel (316 L) collar stainless steel 900- raised faced weld neck flng. w/blind stainless steel Figure 1 . Reactor Diniensions ullow for the more than 2 inch vertical heat expansion, the reactor was welded to horizontal 8 inch I beams at the bottom and guided at the top by triangular ears which moved in slots welded to another set of I beams. A star feeder model R2-653 manufactured by Beaumont Birch Co. was mounted between the manure hopper and the reactor using a Reliance VSD variable speed motor Model B56G3102 with a 12 to 48 sprocket gear ratio. The inlet gas distribution plate at the bot- tom of the reactor consisted of a 3/8th inch stainless steel plate with concentric circles of l/16th inch holes drilled into it around a 1 inch hole in the center. This distribution plate was welded to a thin collar which was welded to the bottom flange of the the reactor in such a way as to provide even inlet gas flow to the bottom of the distribution plate (Figure 2 ) . A one inch OD stainless steel tube passed through the bottom flange and was then welded to the central hole to allow char to exit the reactor. This tube extended about 6 inches through the outside of the bottom flafje where it was connected with swedgelock fittings to the char hopper. The whole distribution plate system and flange was fitted with yery close tolerance into the bottom of the reactor. Char Hopper and Ram The char hopper was constructed in such a way that solids flow could be diverted from one side to the other by moving a semicircular piece of metal (Figure 2 ) . This provided a method reactor fluidization plate swedgelock approximate position of ram in down position ^*^^B ^^ inlet air and steam ^-^ interior ring semicircular pi ate side changing lever pipe guide ram dividing plate between hoppers flange access port ports for ^ driving air Figure L. Lhar hopper and Fluidization Plate of measuring the char flow rate. 10 The original design had a large flange which formed the top of the hopper to provide access to the interior. Because of the awkwardness of removing the whole hojjper after each run to remove solids, the difficulty in removing char from each side without crossover, and the leaks in the thin homemade flange; the upper flange was cut off and a plate was permanently welded on. Access was then provided to each side of the hopper by 4 inch flanged nipples which could be easily removed for cleaning the hoppers. A pipe which served to guide the ram was installed through the center of the hopper. The ram was a polished rod, which in the up position, extended through the distribution plate and effectively plugged the exit port of the plate. In the down position the top of the ram was several inches below the entrance port to the char hopper allowing free flow of solids from the reactor. The ram cylinder was pressed against a lead gasket at the bottom of the char hopper by chains and turnbuckels to provide airtight seal. V Reactor Heaters The heating section of the reactor consisted of two 24 inch long sections. Each section was constructed of 4 pre-formed pieces which were fitted around the pipe and secured with external bands. Each section was rated at 40 amps, 206 volts. Circuit breaker protection was provided for each of the 4 pieces in a section. 11 These heaters, model 50752 type 77-KSD, were manufactured by Lindberg Co. In general, the performance of these heaters was less than satisfactory. Improper electrical installation was one pri- mary cause for repeated failures. The other primary cause was that the heaters were damaged during the early runs by exceeding the voltage and temperature design parameters of the heaters. As time progressed, more and more elements burned out (2 elements to a piece). By the end of run 10, only one element in the lower sec- tion, or 12.5% of the original capacity, was operating. Only about 50% of the upper bank was still operating during the final runs. About 25% of these failures were obviously due to mechanical breaks in the nichrome lead-in wires in places where they could not be repaired. Some of the other failures were apparently due to ox- idation and melting of the nichrome material. Preheater The preheater consisted of a U-shaped loop of stainless steel tubing. The first section was 16 feet of 3/4 inch tubing and the remaining 17 feet was 5/8ths inch tubing. This loop was connected by 3/4 inch braided copper welding leads to a Hobart Model T-5005422, 500 amp welding generator. A government surplus D.C. power supply was originally purchased for this purpose, but was found to be faulty and was used only for its magnetic contactor. To pre- vent a meltdown of the preheater piping, the contactor was controlled by a Thermo Electric model 32142-02-005 Mini Monitor Analog 12 Latching High Temperature Alarm triggered by a thermocouple clamped to the top of the preheater. The tubing of the preheater was en- cased in a sandwich of block type insulation which was held together by duct tape. Because of the large convection surface area of the system and limited power supply, meltdown was not judged to be a problem except in the case of no flow through the preheater. Instrumentation and Controls Type K thermocouples were used to monitor the temperature profiles in the reactor and were attached to a 24 point Leeds and Northrup model number 547 recorder. A Flexapulse pneumatic timer manufactured by Eagle Signal Corp. was used to control the motion of the ram. This unit could be set to independently control both the number of seconds the ram stayed up and the number of seconds down. To control the input air stream, a Brooks type 1110-06F1A1A rotameter was installed. . test meter. The rotameter was calibrated using a wet A Brooks type 1110-OlFlAlA rotameter was connected to the helium input line to measure the flowrate to the feed hopper. However, the helium flow rate required was shown to be beyond the capability of this rotameter. No replacement rotameter was in- stalled because the flow rate was not critical to the operation. The cold product gas exit rate was measured using a Rockwell 2 inch model TP-4 turbometer. 13 An Elison Eagle Eye flowmeter (mechanical manometer) with an •Arnubar semi-pitot type sensor was purchased to measure the steam f^ow rate. This unit proved to be unreliable due to its slow re- sponse time (measured in hours) and the relatively high air content of the steam. A roughly calibrated needle valve was finally in- stalled and the flowrate was checked during each run by diverting the steam flow through a hose placed in a bucket of cold water. The increase in weight of the water bucket resulting from condensed steam was used to calculate the steam flow rate. Pressure taps were provided every six inches along the reactor to measure the pressure drop across the fluidized bed. These taps were manifolded through three 5-way valves to a Honeywell Pneumatic Differential Pressure Transmitter. mitter was hooked to two pressure gauges. The output of the transOne gauge was located on the main control panel and one v/as installed on the pressure tap valve panel on the same level as the star feeder. To provide control over the reactor heaters, tv/o model 1501AG-58-IK proportional temperature controllers were used to drive model PAKlO-0-lX triac contactors. manufactured by Victory Engineering Corp. Both sets of units were The controllers and contactors were not capable of handling the severe load, voltage and temperature conditions. The units incorporated no protection circuits, and had a limited life expectancy because of over heating of the triacs. The heater controls were the most signifi:ant pro- blem encountered during the initial mechanical phase of the 14 operation. After going through several attempts to bring the loads down using large inductors, and a capacitive bypass for surge protection, the original triac contactors were discarded and new silicon controlled rectifiers (SCR's) were ordered from Vectrol. The rectifiers, model VSSC-1020-240-1FAC, were capable of handling 63 amps each at 240 volts with full surge protection. The original proportional controllers were retained and a 2500 ohm variable center tap resistor was installed on the output stage of the controler. The center tap was adjusted to provide voltage through a rectifying bridge to the 15 volt D.C. control circuit of the Vectrol SCR's (Figure 3 ) . A Fisher type 657-ES pressure control valve with a built in Fisher Wizard type 4100ZR controller was installed to regulate the pressure in the system. The sensing tap for pressure control was located just above the reactor exit port for the hot gases in the 2 inch line leading to the cyclone. Down Stream System The configuration"of the downstream system was in a constant state of change. One can appreciate the sweeping nature of the accumulated changes by referring to Figures 4 and 5 which represent the original construction and the present configuration of the system. 15- Vectrol SCR ^w\/w^- to control ^ circuit semicond fuse circuit breaker heaters circuit breaker o—vV\A-c> o v\AA-o%)- 2500j^ 25 W fuses -•a>#-o to thermocouple 1i I control circuit zv zr 5=^ Victory Temperature Controller Figure 3. Electrical System 16 o to c o p:: (1) c: CD O QJ cn •r— 17 18 The filters for the exit gas stream shown in Figure 4 consisted of three AMF-Kuno catalog no 5224301 model 41-0403 cartridge type filters welded on a one inch O.D. stainless steel pipe. These filters have an opening size of 40 microns. Tv/o commercial impingers were used in the system. One was located just after the tar trap and the other was located in the water/gas separation system. These impingers consisted of a wire screen impingment filter and a fixed vane centripetal separator. MODIFICATIONS Although the reactor system operated successfully on the first r'^n, extensive modifications were required to allow a Wider range 0? operating conditions and to solve various problems that developed. Feed Hopper From the wery first run it was apparent that once steam entered the star feeder that the manure flow into the reactor stopped almost immediately. This was due to the moistened manure being packed into a stiff paste by the mechanical action of the star feeder or simply the moist manure particles adhered together to form a plug in the hopper above the star feeder. Initially it was found that backflow could only be prevented by the use of excessively high helium flowrates (one cylinder per hour). A con- centrated program to eliminate leaks was undertaken which ultimately led to the redesign of the 4 inch feed inlet section at the top of the hopper, building a new cone for the bottom of the hopper, redrilling the homemade flange separating the top and the cone of the hopper, rewelding all the joints on the hopper, and silicon sealing the flanges. It was also discovered that hot gas backflow had destroyed the relatively low temperature seals in the star feeder. New seals had to be ordered and replaced before further operation was possible. 19 20 These procedures cut the potential for backflow into the hopper by an order of magnitude. Unfortunately, it was soon ap- parent that this was not enough. During startup as the pressure rose in the reactor because of generation of gas or filter loading, backflow into the feed hopper occurred which equalized the pressure in the dead air above the manure. If backflow occurred faster than the helium purge flow rate, plugging resulted. run series the solution to backflow was found. Later in the A 3/8 inch bypass line was installed between the top of the manure hopper and a point just below the star feeder. This line incorporated a 2 inch by 15 inch water cooled condenser with a small reservoir and blow down valve to condense any steam in the bypass stream. Another problem related to backflow was the condensation of water and tar on the sight glass which picked up manure dust and made observation of the manure flow into the reactor impossible. A second Thermo Electric Mini Monitor Latching High Temperature alarm was ordered and installed with a warning buzzer which was triggered by a type J thermocouple that was placed just below the star feeder and opposite the bypass opening. This alarm detected when backflow was occurring and allowed more conservative helium flow rates. Cyclone and Filter By the end of Run 4, it was apparent that the filter arrangement was not acceptable as a means of removing solids from the 21 product gas. After a few runs, the filter was nearly permanently clvigged with condensed tar and small particles, thus allowing only a minimal flow at high differential pressures. The clogging prob- ably resulted from the small surface area, the dense packing of particles, the unheated design and the large solids carryover. A sample of the carryover scraped from the filter and the residue in the filter housing were sieved,using this particle size distribution, a cyclone was designed (Figure 6 ) . The filter was retained in a position immediately downstream of the cyclone and gas fired heating jackets were provided for both. The cyclone was moved as close to the reactor as possible since heat transfer calculations showed that it was impractical to insulate the original long length of pipe to the degree required. Run 5 proved that the fil- ter problem had not been solved by the addition of the cyclone. Subsequent removal and examination of the filter after the run showed that the filter was covered with a white ash material having no visible porosity and closely resembling a coat of gray latex house paint or fine paper. This material was judged to be unfilterable and of a small enough volume not to cause plugging in the tar trap or water cooled condenser. Therefore, the filter and filter housing were removed. A rather thick accumulation of tar was noted inside the filter cartridges when they were broken apart. During the filter removal, the two inch air cooled heat exchanger before the tar trap was shortened to about 5 feet. This exchanger was operated using 22 8" to 2" swedge blind flange with 8" center r hole 3" 11V 4" Figure 6. Cyclone Dimensions 23 natural convection. After solving the particle carryover problem, the poor tar trap efficiency was investigated. It was found that only small quantities of the tar were condensing in the air cooled heat exchanger line or tar trap. Almost all of the tar was being col- lected in the impinger located immediately after the tar trap. A rolled piece of aluminum screen was alternately dimpled and inserted into the 2h feet of the two inch air cooled line to act as an impinger. The effectiveness of this screen was not ascertained. The impinger still collected most of the tar. However, a certain amount of a somewhat higher melting point tar did accumulate in the tar trap. Both sections of the tar collection system were later steam traced and' a 4 inch diameter 12 inch long reservoir was attached to the impinger. Water-Gas Separation The water-gas separation system was originally constructed with a two inch knock out drum, a shop modified inverted bucket type steam trap converted into a float type and another impinger of the same type as used in the tar trap system (Figure 5 ) . The steam trap did not have the volume throughout required, so it was converted into an emergency overflow which was used frequently. A h inch needle valve was modified into a float valve and installed as the primary valve. This valve was not very successful because the 24 x \h inch wooden float tended to stick in the gummy tar 24 residuals and required a great deal of tapping to reach an equilibrium condition. After a tar trap fire in Run 10, live steam had to be used to unplug tar in the water cooled exchanger. The steam cleared the water cooled exchanger, but it was found that the whole water-gas separation system was filled with tar. The needle valve float assembly would have been very difficult to clean and a larger commercial type float valve was ordered and has been installed. Flow Measurement System It was discovered that oily organic condensates were fouling the turbometer. To prevent fouling, a small water cooled condenser and a glass wool filter were installed. In addition, a small 1% inch diameter cyclone and a bypass around the meter run were added (Figure 5 ) . The small cyclone was observed to have little effect on entrained liquids in the gas. The filter was effective, but the filter media had to be replaced every run. In Runs 9 and 10, cotton was used instead of glass wool in the filter because of availability. Operational Procedure 1. The reactor was heated up to operating temperature using an air purge rate of about 3 SCF/min. 2. After starting the helium purge, steam and air were added at the rates to be used for the run. 3. Once the system became stabilized and the water removal system 25 was functioning, the manure feed was started. A ram cycle of 3 seconds down and 10 seconds up was employed. 4. After the system reached thermal equilibrium the mass balance period was started by switching the flapper in the char hopper sides, dumping the cyclone via the ball, valve, changing the waste water container and drawing off any tar. 5. The mass balance period was ended by switching the flapper in the char hopper back, and collecting the tar, water, and cyclone samples for weighing. 6. Gas samples were taken by connecting a gas sampling bottle across the sample loop (Figure 5) and adjusting the pressure drop across the loop to about one psig. 7. The system was shut down by reversing steps 1, 2, and 3. 8. Char was removed and weighed after the reactor cooled. Analytical Procedures Gas samples were collected in 250 ml gas collection bottles. These were then analyzed using a Varian Aerograph Gas Chromatograph with two columns. One was a 12 foot long, l/8th inch diameter column packed with 50/80 mesh Poropak Q. A 4 foot pre- column of l/8th inch tubing packed with 50/80 mesh Poropak R was used in conjunction with the Poropak Q column. These columns were used to quanititatively measure hydrogen, methane, carbon dioxide, ethylene, and ethane. A 12 foot long l/8th inch in 0 diameter column packed with 45/60 mesh 5 A molecular sieve was 26 used to quantitatively measure hydrogen oxygen, nitrogen, methane, and carbon monoxide. Runs 1 through 5 were analyzed through the (II) courtesy of Young ^ ' who was studying the theoretical aspects of the pyrolysis process using a different chromatograph with similar columns. A ser.ies of one ml. volumes of air v/ere in- jected before and after each sample series. The air peaks were averaged and a corrective factor was calculated from a standard peak height which was used to correct the sample peak heights. At least two injections on each column were made for each unknown sample. The peak heights were then converted to moles using stan- dard curves. Any oxygen present in the sample was assumed to be due to air contamination and was subtracted out along with a rationed amount of nitrogen. The two columns were related by the amount of methane measured on each side. This procedure was re- fined, and a computer program was written to calculate the various results. Because of the large sample injection volumes, the program could only be used on runs 8, 9, and 10 because the peak heights for the other runs fell beyond the linear portions of the calibration curves. Sieve studies were done by shaking samples through standard sieves with an automatic sieve shaker for 10 minutes. tions were then weighed. The frac- Moisture content of the manure was found by heating samples in a weighed crucible at 104°C overnight, desiccating, and then reweighing. Ash content was obtained by heating the sample in an air environment at 950 C overnight and 27 then finding the weight differential. Density was measured with e-standard weighing bottle and calibrating the bottle with distiVied water. Because of the small total volume of the weighing bottle, the densities of the large particle sized samples may be fractionally low. Preparation of Feedstock Manure was collected at Lubbock Feedlots located on the Old Slaton Highway. The large feedlot manure pile was surveyed using visual examination and a shovel to find the driest, freshest, loosest, manure that could be found in that order of preference. The feedstock was collected in garbage cans and transported to the Texas Tech Feedlot where a Wildcat Far Hammer Mill and tractor was used to grind the manure. A screen of 1 inch squares was used in the hammer mill because it was the only size available. The manure used in runs 1 through 3 was sun dried for a few hours on a large plastic sheet. not require drying. The manure used for the remaining runs did In Runs 1 through 8 all manure was sieved through a piece of metal lath to remove gross particles prior to loading. This hexagon shaped screen passed all particles smaller than about 3/8ths inch in diameter. For Runs 9 and 10, the manure was sieved to pass through an l/8th inch hail screen. This was done in a hand operated tube sieve constructed for this purpose. DISCUSSION OF RESULTS The primary objective of this study was to provide scale up information for the construction of a commercial plant and to determine the various operating parameters which must be considered in the design and operation of a larger scale system. The pilot plant reactor involved a cross sectional area scale up over (2) Herzog's ^ ' small reactor of 14.2 to 1. Feed Considerations As was expected, the primary problem encountered in operation was solids handling. Extensive efforts were required to keep steam from entering the feed material before it was introduced into the reactor (See Construction, Modifications, Feed hopper). It became apparent after working with this material that moisture co'ttent was of primary importance. The moisture content of manure varies between about. 80% (fresh droppings) and about 3%. It was found that a feed with a moisture content of about 30% ground to pass a l/8th inch screen could hold a perpendicular angle of repose and compacted easily into clumps with applied pressure. However, with vigorous tapping on the side of the hopper this material would flow. feeder pockets. This feed tended to compact in the star Drier feed material flowed without vibration and was more resistant to compaction. The ideal moisture content appeared to be about 10% from a feeding standpoint. From these observations, it is the author's opinion that in a commercial 28 29 operation, once the manure- leaves the hammermill, it should be handled by air transport rather than auger or drag chain. Air transport would help to dry the manure. Drying the feedstock represents a major drawback and a potentially high cost. There are several possible methods for achiev- ing dry feedstock. The first is a char fired rotary kiln or similar arrangement. This is not attractive because of its high capital and operational costs. Also exhaust gases may be a problem. The second alternative is spreading the raw feedstock over a large area of land and allowing the arid weather of West Texas to dry a thin layer. several drawbacks. This would be relatively cheap but has The environmental impact of the manure stor- age problem is intensified by increasing the surface area. Flies, watershed runoff and odor would be worse during wet weather. During dry windy weather, particulate counts would be higher. Ideally the manure would be left in the pens a few weeks after the cattle have been shipped to market, allowing it to dry and then removing it. Unfortunately, the feedlot owner may not be able to afford to keep his pens empty for long periods of time. Finally, atmospheric drying puts the plant operator at the mercy of the weather and requires the construction of large enclosed storage areas to hold feedstock against a rainy day. The author is convinced that the present feedlot practice of piling manure into 20 to 40 foot piles on the corner of the lot will not be able 30 to supply enough dry feedstock on a continuous basis. Weathering soon compacts the pile into a solid non-porous lump and anaerobic bacterial action may generate enough water internally to keep up with the drying rate deep in the pile. This is supported in part by the observation that very large slabs of manure (12" thick or better) were usually too wet to hammermill at the core. Also it was the authors experience, while walking on an old pile of manure at the feedlot where the surface manure was exceptionally dry, to break through the surface crust and obtain a very wet sample approximately knee deep. Ground manure stored in gar- bage cans gained noticeably in moisture content over a several month period if the cans were covered with a tight lid. Thus in any large volume storage bin, air would have to be blown through the material at a low rate to discourage anerobic activity. Larger storage air flow rates would probably have a drying effect. Waste heat from the reactor system could also be employed to assist in drying. A possible alternative to more costly drying schemes is blending. The author's solution to wet manure was to mix drier manure with it during the hammermilling. Since the Syn Gas process should work equally well on any cellulosic material, if a large amount of gin trash, ^'ck hulls, peanut shell, sunflower trash, or many other possible feedstocks could be obtained, then blending would be a very reasonable drying alternative. In fact, the hot char produced by the process could be used as an active blending agent for the lower moisture contents. •31' It is anticipated that the most econonical drying scheme will probably be a combination of two or more of the above methods. Sun dryino is by far the cheapest method and would prob- ably be employed to lower the moisture content as much as possible, If required,one of the other schemes would probably be used to reduce the dried manure to a moisture content that can be handled easily. Some excess drying capacity might be desirable for periods of wet weather. It is doubtful if this process will be economical in areas with extremely wet weather. Experimental Conditions and Results A summary of the range of operating conditions which were employed by the pilot plant study is shown in Table 1. Typical raw gas compositions and densities for the feed and char are also reported. A complete listing of the data and results can be found in the Appendix C. a2 TABLE I TYriCAL OPERATING VALUES AND RESULTS FOR THE PILOT PLANT REACTOR Typical Raw Gas Composition: COr-^.POUND h MOLE % 29 to 11 h 41 to 13 CH4 15 to 7 CO 23 to 14 C02 20 to 11 C3H, 7 to 3.9 2.5to ^2^6 Temperature Range °C Manure Feed Rate Air Feed Rate Steam Feed Rate Raw Gas Production Rate 00. Thermocouple #6 lb BDAF/hr SCF/hr Ib/hr SCF/lb BDAF 810^ 0 27 6 4 to to to to to 920° 40.1 150 10 17 Densities 3 Ib/fV Char from hopper 22.4 (Run 8) Char from Cyclone 17.7 (Run 8) Fine sieved manure feed 30. (10% H2O) Course sieved manure 30. - 40. 33 Reactor Operating Characteristics During the first run 3 to 6% ethylene concentrations were noted in the produced gas stream. This was attributed to the temperature "quenching" effect caused by the lightly insulated top of the reactor. It was decided not to insulate the reactor fir^tner as planned in order to possibly increase the production of -:iiylene. As a result of this light insulation, tremendous heat •osses were sustained which made a heat balance on the system almost impossible. However, studing the temperature pro- files of the hot reactor just before adding manure and during operation provided some insight into the actual operating characteristics. It appeared that most of the combustion was occuring just above the distribution plate, perhaps confined to an area as little as 12 inches high. This can be shown by comparing the temperature profiles of Run 8 and 9. (see Fig. 7) In both of these runs, only one heating element was operational and was at maximum capacity at all times. Run 8. Run 9 had an air feed ratio about 3 times that of All other feed rates were the same. The rapid temperature rise in Run 9 can only be accounted for by the release of heat through combustion. The possibility of a fluidized bed evenly distributing the heat within the lower section was judged to be unlikely because of the noticable dip in the temperature profiles between the heaters where the reactor was very poorly insulated. The differences in the temperature profiles above the heaters 34 -o = <D •r- CO "O •r- O to 4-> c: fO = S- UD "O cr fcs QX LU O -r4-) u (D CO 900 800 CJ 700 o i_ c 600 500 400 _£^ Run 9 O Run 8 |3 No Feed.Startup Run 9 .a\ O V' 300 H—h—I—I—I 4. 5 6 f—f 7 8 • • ^ \ ^ -\ 1 ^ 1 1 9 10 11 12 13 Ther-mocouple ngiire 7. Temperature Profiles in Reactor 3;:. CQjId be due to the higher total gas flowrate of Run 9 because of the extra air. Another possible cause was that the steam and corbon dioxide concentrations varied between the runs, giving the gaS a different emissivity for radiant heat transfer. There appeared to be no clear correlation between air feed rate and exit gas composition except for slight shifts in the C0r>-C0 ratios^, provided the dilution effect of the air was removed mathematically. Appendix. This calculation is explained in the This indicated that the desired synthesis gas reaction was basically pyrolysis as was confirmed by the work of Young. Young indicated that most of the pyrolysis reaction should be over before the manure particle reached the typical highest temperature zone in the reactor, provided that the particle was not heat transfer limited. for small particles. Young indicated this was unlikely This quick reaction theory was also sup- ported by the pilot plant data in that the fines which were collected in the cyclone appeared, on the basis of their ash contents, to be as well or better reacted as the char collected from the bottom of the reactor. Thus the reactor was apparently divided into 3 zones of reaction. In the top zone pyrolysis occurred and in the bottom zone combustion. The middle zone could sustain a number of reactions, the ones of primary interest being: CiH20 -> CO+H-,0 -> H2+CO (1) H2+CO2 (2) 36 (121 Reaction 1 is endothermic and probable not significant.^ ' Reaction 2 is exothermic and proceeds rapidly in the presence (12) of a catalyst.^ It is reasonable to assume, that in the steam diluted atmosphere at the bottom of the reactor, a considerable amount of the oxygen introduced with the air was converted to carbon monoxide. Also since some ashes act as catalysts,^ ' reaction 2 has potential for shifting the exit gas composition. The gas analysis data did not provide any conclusive evidence regarding extent to which these reactions were occurring. The very sizable scatter of the hydrogen percentages compared to temperature could easily have resulted from analytical difficulties and shows no discernable trends. (See Figure 12) From an analysis of the data reported in the Appendix the reactor temperature appeared to be the most critical parameter affecting the observed outputs. The number of standard cubic feet of gas produced per pound of bone-dry, ash-free (BDAF) manure is given in Figure 8. on the figures. duction data. were preferred. Differences in feed particle size are noted There were two methods for obtaining gas proDirect readings from the exit gas turbometer However, fouling of the turbometer occured in some runs so gas production was back calculated using a nitrogen balance comparing the air input rate and the product gas analysis. Turbometer readings were used for all plots in this thesis except fir runs where these data were not available or obviously not correct (Runs 1, 7 and 9 ) . The back calculated flow rate was used for these runs. 37 ii course sieved data 17 - O "fii^e sieved data ii 16 15 f 13 ^ .o 12 ^ LU to c o .a <3P O n 10 £1 8 7 « • I — n. © il ja. 6 O £i 5 ja 4 3 j ^ 1 i 800 850 900 Temperature Figure 8. C 950 Thermocouple # 6 Raw Gas P.oduction 1000 38 Reasonably good agreement can be shown between the calculated and observed flow rates for the other runs. A complete listing of values calculated by each method can be found in the Appendix. In Figure 9 the gas production data were corrected for the dilution effect of the added air and combustion products by removing the nitrogen and a ratioed portion of carbon monoxide (See sample calculation in Appendix A). This calculation assumed that all the oxygen entering into the system with the input air left the system as carbon monoxide. Data which have been treated in this way will be referred to as normalized data. By normal- izing the data the gas flow rates and compositions should only result from the manure pyrolysis reaction which yields a better correlation of the data. " Because several of the samples in Herzog's data^ ' (Figure 10) contained less carbon monoxide than was called for by the calculation, a second calculation was made assumed that all the oxygen entering into the system leaves as carbon dioxide. Both these values were plotted on Figure 10. The real volume correction due to combustion products should fall between these points. This second calculation was also done on Runs 6 and 7 and the maximum difference between the two assumptions was less than 15% of the normalized gas flow rate. Herzog's data obtained from the bench scale reactor were the basis for the design of the large reactor. Comparing Figures 9 and 10 it can be seen that Herzog's reactor potentially generated 39 10 ji Large Sieved Data O Small Sieved Data Q CO 8 to c o •T— 4r> U Z5 O iDto «3 CD -Q. -Q. 5 - H £L "O OD .Q. £L. o 0 750 800 850 900 Temperature Thermocouple #6 Figure 9. Effect of Temperature on .formalized Gas Production 950 40 73 12 =3; Q CQ - 11 10 to § 9 o "§ 8 u a. (/> fo "a 7 ' M E o .5 I 650 Figure 10. 700 CO2 assumption CO assumption 750 800 Average Temperature, °C 850 Small Scale Reactor Normalized Gas Production 41 more pyrolysis gas per pound of manure. However, the small scale reactor temperatures probably may not be directly related to the highest temperature in the large reactor (thermocouple #6). It should be noted that Herzog's reactor was top fed through a standpipe into the top third of the reactor, and most of his solids passed out with the exiting gas stream at the top rather than the bottom as in the large reactor. Herzog's reported temperatures are the average of two thermocouples inserted into the middle of his reactor. The observed differences in gas yields between the large and the small reactors could easily be the result of the gentler temperature profiles in the large reactor. As a manure particle entered the reactor it encountered a temperature of only about 350°C. The temperature rose as the particle fell. Since any volatile molecule resulting from the pyrolysis of the manure particle would immediately be swept into a lower temperature zone by the exiting gas, the large reactor naturally favored large molecules which did not have time to be thermally cracked in the gas phase. This was verified by the larger hydrocarbon percentages shown in Figures 11, 12 and 13 as compared to Herzog's data in Figure 14. This also means that a very significant portion of the total hydrocarbons produced appeared as condensables in the form of tar or lighter organics (see mass balance. Table 2 ) . These tars and organics were not extensively tested by the author, but Del La Garza^^^^ has undertaken this 42 ^ 15 r n J:I^ n 10 ii o n ii SI %L il^ o O o. o C3 eg <s>^og H Methane O Ethane o O 0 800 850 900 950 Temperature °C Thermocouple #6 Fiqure 11. Raw Gas Composition (Methane and Ethane) 1000 43 30^ JQ. jQ. XI XI ID. ^ 20 XI # o o i?- to o n. JQL XL o Hydrogen O Ethylene ja o I 10 G O^0 GO G G 0 800 850 900 950 Temperature Thermocouple -6 Figure 12 Raw Gas Composition (Hydrogen and Ethylene) 1000 44 C\ Methane -^ Ethylene Ethane 30 0-5 o o 20. to o EL E O CJ to CD "O O) M ft3 E S- o 10 ^c^o-cg 0 800 Figure 13. 850 900 950 1000 Temperature, °C Thermocouple #6 Reactor Effluerrt Gas Composition 45 30 r- O Methane Q Ethylene o o 20 to o CI. to CD M o 10 - i^- 0 650 Figure 14. ± 700 750 800 Average Temperature, °C Small Scale Reactor Gas Composition 850 46 TABLE 2 MASS BALANCES RUN NO. 8 Inputs (lbs) Wet Manure Air Steam 28.52 8.51 4.30 39.79 3.78 6.75 Total Input 41.33 50.52 29.43 Gas Out H2O Out 15.60 10.75 12.66 14.19 5.84 7.25 Tar Cyclone Char 0.5 1.63 8.25 0.5 1.38 15.50 0.5 1.25 6.0 36.73 11.13% 44.23 12.45% 20.84 29.19% % HpO 10.00 10.00 10.00 % Ash 19.59 21.54 21.54 46.5% 49.45% 50.24% 55.50% 53.27% 60.2% 22.28 2.88 4.27 Outputs (lbs) Total Output Unaccounted for Other Measured Data Manure Feed Ash Contents Char Cyclone 47 MASS BALANCES(CONTINUED) RUN NO. Output Product Distribution (Mass Percent) 9 8 7 Np Free Gas 41.65 32.00 25.29 2.09 1.83 2.89 15.07 18.47 12.67 28.32 4.30 15.93 3.44 2.24 2.84 Tar Light Organics & Produced HpO (input steam subtracted) Ash Free Char Ash Free Char from Cyclone Accumulation and/or experimental error Totals Total Char Total possible produced tar and liquids including accumulation Np Free Gas *SEE DISCUSSION •k 19.29 22.90 48.79 100.01 100.01 99.99 21.91 30.56 18.77 * 36.45 41.65 37.40 32.00 55.93 25.29 48 project for his Master's thesis. Preliminary results showed that •further cracking of,the tar produces a variety of unsaturated compounds of which ethylene, propylene, and various four carbon compounds comprised a major portion. Thus, while thetotal normalized pyrolysis gas generation in the larger reactor may, in general, lower than that produced by Herzog, the gas and tar produced in the larger reactor may be potentially more valuable. It should be noted that the differences in reported temperatures between the large and the small scale data were not significant. In the large scale reactor there were 12 thermo- couples spaced evenly along the reactor. Any of the thermocouples in the upper section (6 through 12) could be used to relate the data and a reasonable correlation was obtained. However, thermo- couple 6 seemed to relate the data as well as any of the others and was considerably easier to read from the strip charts because it was usually the highest temperature in the reactor. The average temperature of the pyrolysis zone would probably be the best temperature to correlate the data. Unfortunately the exact location and length of this zone was unknown. By averag- ing all 12 thermocouple readings in the reactor and the temperature of the inlet gas through the distribution plate, the raw,.large scale data can be shifted to nearly aline with Herzog's raw gas production data (Figure 15). 49 XI Course Sieved Runs O Fine Sieved Runs Small Scale Reactor 30 t- o CQ 20 O ^^ A o u -o o sQ_ lo CD- 10 0 600 1. 700 Temperature, °C 800 Figure 15. Average Temperature Comparison to Small Scale Reactor 50 The increase in the normalized gas generation rate with temperature, suggested that, at higher temperatures some of the larger pyrolysis products did not have time to be generated and escap- from the particle before it entered a higher temperature zone that could cause secondary cracking. A study of the effect of higher fluidization gas velocities, which would further verify this hypothesis, should be a part of the next phase of investigation. The above analysis of the data indicated that the reactor as it was operated, produced a significant amount of tars and liquids at the expense of the total gas rate. If the objective of the process is to obtain unsaturated organic compounds, it may well be that two stage pyrolysis would produce higher yields by allowing more precise control, and possibly the use of a catalyst during the second cracking of the tars and organic liquids. However, such an operation could require a considerable increase in capital investment. If the ethane and ethylene are removed from the observed exit gas stream and the CO2 is scrubbed out, a producers gas with about 500 BTU/SCF (see appendix) still remains which could be sold as fuel. If ammonia synthesis gas is desired, then any production of tars or liquids is undesirable. The solution in this case would be to very heavily insulate the reactor as was originally planned for this study. This would bring the top temperature of the reactor to as high a value as possible. By experimenting with 51 intermediate insulation thicknesses, it should be possible to optimize the production of ethylene. The data illustrated in Figures 9 and 13 indicate that an increase in the exit gas ethylene concentration is unlikely, but the volume of the gas could be increased significiently. (3) From the development of the bench scale reactor^ '' it was found that a manure feeding arrangement on top of the reactor was much superior to all the other systems tried. However, on a larger scale it may be feasible to build a bottom fed reactor which would increase the probability of complete cracking which would require less reforming to produce ammonia synthesis gas. A design and discussion of such a reactor has been included in Appendix B. Downstream Operating Characteristics The gas stream produced in the large reactor contained 5 to 21% of the total solid char by weight. These small particles ranged in size from those caught in the cyclone (about 250ym to 20ym) down to sub micron sizes. The appearance of the exit gas was a dense grey smoke with a slightly green tinge and an unpleasant odor. Tar began to condense significantly from this stream at approximately 320^0. The tar condensed at different temperatures had a noticeably different appearance and characteristics. The highest boiling point tar was found to form grainy deposits which did not flow well at steam tracing temperatures. The grainy ap- 52 pearance could be due to fractional crystalization. The observed appearance of this tar was that of a nearly cold lava flow filling the bottom quarter of the pipe and consisting of 95% solids. However, the ash content of this tar was considerably less than one percent, so little char was present. It was easier to use a ham.mer and chisel to shatter the high temperature tar out of the tar trap than to melt it out using steam tracing and positive pressure. Only one large sample of this tar was taken because it tended to accumulate in the lines leading to the tar trap. An internal fire in the downstream system in Run 9 caused the accumulated tar to move down into the tar trap. A peak temperature of 900"c was registered just above the tar trap during this fire. The tar tended to condense on the entrained solids forming an aerosol. Thus, wery little tar was collected in the tar trap. However, the tar impinger apparently worked well and removed a large amount of the entrained tar from the gas. There was a noticableable relationship between pliancy of the tar and collection temperature. This varied from a very soft material similar to taffy at low temperatures (approx. 110°C) to a hard and relatively brittle material at high temperatures, (approx. 300°C). The product stream from the water-cooled condenser was a brown to yellow, murky, foul-smelling liquor with a very high total solids content and colloidal organics. Over a period of 53 weeks, the liquid settled into three phases; a foamy organic layer, a somewhat darker water layer, and a layer of solids. Closer temperature control in the condensers would reduce the amount of organics in the water stream by collecting the water and light organic streams separately. The waste water would still be heavily polluted, but because the process produces a potential activated-charcoal as a by-product, a serious problem with organic-contaminated wastewater may not exist. One major problem was that the wastewater stream tended to cause severe sticking problems with the float control valves. The separated gas stream was clear of suspended solids, but a problem was encountered with condensing liquids and aerosols which tended to foul the turbometer. Several of the reported gas flow rates had to be back calculated form the nitrogen content of the exit gas because of obviously faulty readings. Feed Particle Size Prior to Run 9 the char contained visibly unreacted manure particles. A representative sample of the char from Run 8 was sieved using a set of standard sieves, and the ash content of each fraction was determined (see Figure 16). If it is assumed that the original ash content of all the various sized particles was the same, then approximately one third of the reactable mass of all the particles over 2 mm was unreacted. Young's data^^^ indicated that raw manure particles smaller than about 0.25 mm 54 60 +-> CD 50 00 40 o o >> t-J o I o r^ r^ o I o A I I o C>J Figure 16. Effect of Particle Size on Degree of Reaction 55 show higher ash contents than larger particles. This phenomenon could explain the higher ash contents in the first and second points on Figure 11. Since the size distribution in any given ground manure sample used in the large reactor varied considerably, it-was decided finer sieving would be required. The closest, com- mercially available screen size was l/8th inch hail screen. There- fore this screen was used to construct a portable tube sieve which could be transported to the grinding site which was located several miles away from the reactor. The effect of particle size is confirmed in part by examining Figure 9. The finely sieved runs show much less scatter between individual samples and apparently define a more precise relation. Char Characteristics Once a thoroughly reacted char had been obtained, the problem of unwanted fires arose. The problem was not how easily this char would burn, but how to keep it from burning. In Run 9 the hot char from the cyclone was ignited by a plastic bag left in the collection bucket. After noting the glowing fire on the sur- face of the material, the fines were stirred with a steel pipe and then dumped on a steel plate in a pile about 2 to 3 inches deep. This material which had an average particle size of about 70 ym continued to burn for hours and visually appeared to be converted to almost pure ash. The combination of high heat cap- .55 acity, low conductivity, and high porousity was thought to account for such good combustion characteristics. The char burns hot av.i clean without any odor. A siipplemental test of the char in a large, two-stage cotton-v;dste-furnace showed no problems with combustion other than the large amount of ash left in the bottom of the furnace. In actual operation, some care will have to be taken to prevent exposing' the char to air until it has been cooled below its ignition point. Another small fire was maintained in the char hopper in wery limited oxygen for longer than 24 hours after the run. Fluidized Bed and Char Hopper Characteristics There was no evidence to indicate that a fluidized bed was ever obtained in the reactor. The pressure tap system which was designed to measure the pressure drop across the bed, never showed more than a gentle pulsing which could be related visually to the slugs of feed. This further supports the rapid reaction theory mentioned earlier. What the instrumentation did show strongly, was a large negative flow down the reactor which could be related to the dropping of the ram. the process involved. It is easy to reconstruct When the ram was in the up position, the exit was essentially blocked. Hot gas above the char had time to cool through contact with the uninsulated walls creating a partial vacuum. When the ram dropped, the hot char above the distri- bution plate was carried downward with an explosive burst of gas. 57 As the char fell through the hopper it once again heated the gas which equalized and the ram shut starting the cycle again. This w<i;i a very effective method for removing solids, but as a result the whole process was more like a batch reactor cycling every 13 seconds than a fluidized bed. No studies were made on the ef'ect of the cycle time. It is projected that for longer cycle times that a fluidized bed of char would be built up, but this could be detrimental because of the accumulation and more complete combustion of some of the particles. This in turn could lead to the ash fusion problems encountered by the cyclonic manure burning study. ^ ^ Reactor Temperature Control Only a short range of temperatures were studied. limit was set by the skin temperature of the reactor. The upper In the early runs, the stainless steel skin temperature was not monitored and the temperature of the reactor was controlled by attaching the top thermocouple in each bank of heaters to the power controllers. The thermocouples were not shielded and read a composite of both radiation and gas temperature. This pro- vided a very loose coupling between the reactor's interior temperature and the heater control. As a result skin temperatures very close to the softening point of the steel were obtained. 58 After analyzing the problems before Run 7, the control points were shifted to thermocouples which monitored the skin temperature of the steel beneath the heaters. This change tightened up the control linkage resulting in less temperature oscillation and better control. at 1000 C. The maximum allowable skin temperature was set This limited the internal temperature to approximately 900''C. Data Reliability The collection and anaylsis of data for this system was difficult and time consuming. The reliability of the data in- creased significantly as this study progressed because of better techniques and improved equipment. For this reason Run 10 is listed first in the data tables and the other runs follow in descending order. The temperatures listed for the various gas samples were estimated by approximating the residence time of the gas in the system and then reading the appropriate temperature off the recorder chart paper. The residence time was usually approximated by observing the lag time between an upset in temperature and the corresponding change in the recorded exit gas flow rate. This time varied from 10 to 15 minutes. Because of the difficulty in estimating lag time and averaging effects over the sample period, the temperatures were very reliable for the stable runs and were just rough estimates from the runs where the temperature and the exit gas flow rate oscillated rapidly. 59 If the manure feed was subject to compaction or bridging the manure feedrate became erratic due to local bridging and partial plugging of the star feeder's pockets. had this problem. Run number one obviously All the later successful runs used a dryer manure which flowed easily. Ash balances calculated for Runs 7 through 9 indicate that the listed feed rate was not more than about 10% high on most runs. However, Run number 7 which is listed in the mass balance (table 2 ) , shows a large discrepancy between calculated ash input and measured ash output. Therefore the actual manure flowrate in is probably much lower than what is listed. Early Runs As with many experiments the least reliable data are always the most critical. The first run was also the highest tempera- ture run (Table 3 ) . Data gathering was rather poor because of typical start up problems such as leak detection, and trying to determine the effectiveness and range of various equipment. The gas analysis was also somewhat in doubt as the chromatograph was still being calibrated at the time. Most of the listed feedrates are just approximate values. In spite of all this, the results show rather large effluent gas rates. In fact, the maximum rates listed could be conservative since problems with the manure feed did cause sporadic flow. Even allowing for gross error, the data indicated that at higher upper 60 cn O • o C-.I cy» tn i \r-i tn • tvj o P CVJ •• o cn CO rH rH r^ 1 «=f o cn CVJ to rH r ^ CM r>. CO CM cn CM CM r H CO in rH 00 CO tn tn CM tn o I • to <? o e • CVJ I—1 tn o CO cn CT>. O CO rH 00 CO in o « * CO in CO CM CM CM rH rH o cn r H CM CO , to r>s o o CO CM rH <o • cn rH 27.317.9- O rH o• CM rH tn 1 o CM • 1*-^ 00 rH CO tn in f—4 CO to in CO 00 to */) CM * d CM i. <u +-> u. 0 <c tn r^ <u o «;!o •^ CD • 00 o CO cn in • • CM CM rH 1 o ^ to • r^ e ^ r^ in •vfCM CO r^ t n <y\ CM to CM "s*CM CM CM 0 cr> c n CM CO 0 r H CM r^ ^ cn CM CO v o «v^ CM CT> r^ tn in CM o^ CM in CO rH CO CM «-< CVJ «=*• i-H rH -c: in CD zs o o ^ cn tn • r>» CM 1—1 1 cr> • 'sr CVJ I jc: CU cu 4J o <u cj> o E E CO CU -o cu cu i- 4I— t o c rs a: X O <u i~ n. ex cu I— s- ex e x 13 ex o JC cu Lt. i- • < 3 Q C CQ ra JD s : i— s-o cu (U s(U 4-> ra S•o <u (U ME-c: fO ^>» <U E 4-> j Q OO r— XJ a O •r- U_ 4 - > < C •-< o a 13 CQ O E a. I— to u. CD OO sa» +j cu £ o JQ XIS 4-> '1— +n-> o 13 O E O <_) ^ to (U ex r^ ca o ';h CD U S fO (D'l• 0 t 5 fO 1— O) 0 0 s- r j $t o <u to > ra ra to Mol o E •f— o > X c mption of age of two O O CM 00+^ :3 M- C O-rE ex EP^ CU +-» c: t qas s take *-^ ID CiiCM 1 i— t-H to (X. tion LU —J CO <j; 1- E CO CD o CO ex rH C3^ 0 QJ CM m CM 2: re t j 0 c_) '^ito CM r e IC 0 CM CM 0 CJ c_> C 0 £= 0 "OTJ CU (U to to fO 03 JO-Q «CM 61 and lower reactor temperatures a significant increase in gas production can be achieved. The temperature at the top of the reactor (thermocouple 12) during the first run varied from 400° to 490° as compared to Run 9 which had a top temperature of 370 C. All the other runs had lower measured temperatures at the top of the reactor. No data were reported for Runs 2 through 5. In general these were very short runs lasting from 8 to 60 minutes and were characterized by feed problems, heater failures and plugged filters The data were not judged to be of value since the reactor conditions were changing too rapidly to accurately measure. Most of the runs were not long enough to assure purging of the system. Proposed Modifications A major problem with the unit in its present configuration was the accumulation of tars in various parts of the system. A wet steam cooled condenser for the tar collection system has been designed and construction is underway (Figure 17). This vertical condenser employs an annular cooling tube design to solve the expansion problems and to prevent plugging with the high viscosity tar that might occur around any obstruction such as a U tube connection. Superheated steam from the Texas Tech system will be mixed with an atomized water stream to obtain the desired cooling media. A boiling water condenser was rejected upon the basis that it would slow down start up prohibitively. 62 In order to make the process capable of continuous operation three two inch ball valves have been ordered. Two will be in- stalled on top of the feed hopper with a small vessel in between to form a pressure tight lock hopper allowing manure to be added to the hopper during operation. The other valve will be in- stalled in one of the inspection ports of the char hopper. Internal pressure should force the char out similarly to the operation of the ball valve dump on the cyclone. However, it may be necessary to install a manual ram that can be inserted through the open valve to unstop any blockages. At higher gas flow rates it will probably be necessary to construct a larger knockout drum in the water gas separation system. The present drum was constructed of two inch pipe be- cause it was the largest size that was readily available. Since gas flow rates are so important, a backup flowmeter of the pi tot type with a recorder would be useful. A reliable flowmeter for the steam input should also be purchased, doing away with the time consuming and error prone hose and bucket teahnique. As the amount of feed used during a single run will be in excess of 150 pounds at the higher feed rates, a large storage bin has been designed and is under construction. This bin has a capacity of 96 ft^ or about 2800 lbs of ground manure. The bin will be equipped with an air distribution system to force air through the stored manure which will prevent an aerobic decom- 63 position and probably do some drying. The bin will be vented through the stack of the steam plant. This storage facility should cut down the amount of time lost processing feedstock and allow feed collection during drier periods of weather. 64 4" flange TOP VIEW swedgelock fittings^ fittings ^" tubing exit steam 4" flange gas from cyclone 4" pipe k" line to J^" pipe 1^" rod plug welded to end DETAIL OF END OF COOLING TUBE M \•^r'J^ 17 Steam Condens -r Design CONCLUSIONS 1. The operation of the large scale reactor demonstrated that the basic partial oxidation technology developed on the small scale reactor can be applied at a larger scale to produce a useful synthesis gas. 2. The composition of the effluent gas was influenced by the reactor temperature profile. 3. On the basis of average reactor temperatures, the raw gas generation rates from the large and small reactors were similar. 65 RECOMMENDATIONS 1. The various modifications already initiated, such as the installation of a wet steam tar condenser, modifications to allow continuous operation, and storage facilities should be completed. 2. A series of runs should be made to define the maximum feedrate that the reactor system is capable of processing. 3. A study on the effect of fluidization velocity on product distribution should be undertaken. 4. A study using reacted char as feed should be done to determine the extent or importance of water gas shift. 5. The properties and potential of the tar and water streams should be investigated more thoroughly. 6. An attempt should be made to determine the thermodynamics of the system through measured heats of combustion, heat capacities, etc. of the reactants and products. 7. The kinetics of the system should be studied by collecting gas samples from the various zones of the reactor through the pressure tap ports. 8. In order to determine the effect of temperature gradient upon the product distribution, experimentation with removable sections of insulation on the upper part of the reactor should be undertaken. 66 LITERATURE CITED 1. Halligan, James E. and Sweazy, Robert M. "Thermochemical Evaluation of Animal Waste Conversion Processes". Paper presented at the 72nd National AIChE Meeting, St. Louis, Mo. (May 21-24, 1972). 2. U. S. Congress. House. Control of Pollution from Animal Feedlots and Reuse of Animal Wastes. House Report 1012, 93rd Congress, 1974. 3. Herzog, Karl L. "Ammonia Synthesis Gas From Manure". M.S. thesis, Texas Tech University, Lubbock, Texas (1973). 4. U.S. Environmental Protection Agency, Feedlots, Point Source Category, EPA-440/l-74-004-a, January 1974. 5. Garner, William and Smith, Ivan C. The Disposal of Cattle Feedlot Wastes by Pyrolysis. Environmental Protection Agency Report, EPA-R2-73-096, January, 1973. 6. Natour, Ibrahim, Parker, Harry M. and Halligan, James E. "Production of Ammonia Synthesis Gas from Manure in a Cyclonic Burner". Paper presented at 79th National Meeting AIChE, Houston, Texas (March 16-20, 1975). 7. Grub, W., Albin, R. C , Wells, D. M. and Wheaton, R. 1. Animal Waste Management. Cornell University Conference on Animal Waste Management, Ithaca, N. Y. (1969). 8. Nilitin, N. I. Chemistry of Cellulose and Wood. New York: Davey 1944. 9. Coppick, S. "Degradation of Cellulose". Flameproofing Textile Fabrics. New Yrok: Reinhold (1947) P.p. 13-75. 10. Shafizadeh, F. "Pyrolysis and Combustion of Cellulosic Materials". Advances in Carbohydrate Chemistry. New York: Academic pp. 419-474. 11. Young, Hall, Personal Communication on Thesis in Progress, Texas Tech University, Lubbock, Texas (1975). 12. Hougen, Olaf: Watson, Kenneth; and Ragatz, Roland. Process Principles. New York, John Wiley (1959). 67 Chemical 68 13. Khara, Bakulesh Hiralal, "By Product Utilization from processed Manure". M.S. thesis, Texas Tech University, Lubbock, Texas (1975). 14. Mvssie, John Richard. "Continuours refuse Retort-A Feasibility Investigation". M.S. thesis, Texas Tech University, Lubbock, Texas (1972). 15. Smith, G. L.; Albus, C. J.; and Parker, H. W. "Products and Ooerating Characteristics of the TTU Retort". Paper 35e, 76th National AIChE Meeting, Tulsa, Okla. March 10-13 (1974). 16. Al-Haj-Ali, N. S. "Reaction Kinetics and Thermophysical Properties of Feedlot Waste During Drying and Pyrolysis". M.S. thesis, Texas Tech University, Lubbock, Texas (1974). 17. Del-La-6arza, Edward. Personal Communication on Thesis in Progress. Texas Tech University, Lubbock, Texas (1975). APPENDIX A. Sample Calculations for Normalization of Data B. Discussion of Proposed Reactor Design C. Raw Data D. Supplemental Data 69 70 APPENDIX A Sample Calculations for Normalization of Data Raw Gas Composit ion (Mole %) Correct Mole % COp assumption Correct Mole % CO assumption H^ 27.43 44.14% 39. 97 CO 17.57 7.07 25. 60 CO^ 17.62 31.55 18 97 CH,, 7.82 12.58 11 39 CpHyj 2.89 4.65 4 .21 99.99 100.14 N^ 24.78 100.1 CO assumpt ion 1. 24.78 (N2 Cone.) 2C+02->2C0 .21O2AIR 2C0 .79N2AIR 0, Calculated CO = 13.17 due to combustion Subtracting out the nitrogen and the CO due to combustion & recalculating percentages 9 ^' ( 17.57-13.17 ) 100% = 7.08% Corrected CO percentage (100.1-(13.17+24.78) ) Corrected , H, ^-\iMk^r^)^^^°''-''-^'°'' percentage and so forth to yield column 2 in the above table C + 0^ -> 002 for the CO2 assumption thus 4. 24.78 (N^conc.) .2IO2AIR .79N2AIR CO 2 0, calculated C0« = 6.59 due to combustion 71 The nitrogen and the CO2 generated through combustion are then subtracted out and the composition percentages recalculated in a manner similar to the CO assumption to yield column 3 in the above table. It should be noted that except for the percentages of CO2 and CO there is not a drastic change in the percentages from column 2 to column 3. Combustion corrected flow rates For simplicity only the CO assumption will be demonstrated, from equation 1 Total nitrogen & CO subtracted = 24.78 + 13.17 = 37.95 ^ • . . . fraction remaining 100.1 - 37.95 -. _= .6209 ^..^Q 100.1 observed gas rate = 12.96 SCF/lbBDAF normalized gas rate = (12.96) .6209 = 8.05 ^^^^IbBDAF 72 APPENDIX B: DISCUSSION OF PROPOSED REACTOR DESIGN This bottom fed design (Figure 13) depends upon heat transfer through relatively small (2 to 6 inch) stainless steel riser tu^dS. It is not anticipated that heat transfer will be a great problem since at 900°C most of the heat transfer will be by radiation. The external firing allows more control and flexibility in that the BTU's which are added by combustion are not rigidly linked to the nitrogen percentage in the exit gas. High temperature pyrolysis in the reactor with concurrent flow in the presence of steam should convert most of the organics to gas resulting in a higher hydrogen content with less extra processing required. Heat economy is obtained by immediately using the hot char, which has a high heat capacity, in the external furnace. All flows through the reactor are well above the minimum transport velocity to avoid buildup of dense particles. The feed would have to be ground very fine to allow good heat transfer. The actual size distribution needed would probably be a function of residence time and temperature gradient. One possible problem area is at the bottom of the reactor where the manure transport line makes a bend into the reactor. This bend would have to be a much gentler bend than is shown or impingement and build up of manure could occur. 73 CO, Condensers r^ Hydrogen from CO re ormer r\ rS 0 cu ex ex <u j:i. ex s- to 105o <J OO 950 \J ^ 25°C [ ^ wa* waste light water irganicSp C\ o CD t-> : T to CO reformer cyclone cyclone Reactor to demethanizer T and synthesis unit hot char to CO reformer feed hopper solids lock star feeder r^ S- Q rU CX steam purge —53- • € o 1 air input To CO reformer Figure 18. ^ Proposed Keactor Design to Stack 74 • • • 00 CD to CM tn t—1 I en tn CO 00 CD 0 0 . • • 00 CD to CM tn T-H CM I cn CD C-) • CO 00 00 CM 0 0 0 • tf) cn r^ CM 00 in I o CM rH 00 . CM s_ •r— -»-> to « - ^ rH 1-H CM • 00 CM VO r—i rH CD 0 • • 0 to in O) CU if-. O CM . 00 CM • 00 T-H CD • rCvJ CM • 00 o CM rH 00 CM • 00 t-H CM • CO c_^ X I-H CM I CD CD •-H 00 CM • 00 »-l CD • r->. CM CM • 00 CM *H CO CM • 00 rH CD • r^ CM CM • CO • r-» CM ex. CX I CD =^ -"^ U- O E %. CU .C CD OQ CX -c; O 2: o I— O Q •a: ^3 O ex 01 CX <C c s- "I<C 0 crv CO rH t-H I I I I I I I I 00 CO CO 00 CO T-H CM CO t-H CM r^ *5h C3^ . 'd- CO CM ry\ ^;*- r^ 0 CM CM CM cr» «^ cr> 1^ in «*j- 0 CM CO CM T-H t-H CO CM i-H t-H CO in CM cn 0 CM rH CM r—» CO CM t-H CO tn "* a 00 . CO r-i CO r«* CM • "Si- '^ S^ "--s. JD +.> T-H tn t-H CM T-H to 0 r-i «sf CM CM to CM t-H t-H CM 0 0 00 0 tn 0 cn in in CO tn 0 "s*- in tn in 0 CM CO tn 0 tn t-H r—i rH fO u jQ S- _l^ tJ 1— CQ fc cu o s: +J fO S- o C o O to o CX Lt, XJ cu cu M- J- < : CX CD CQ I/) E fO X J CD I— cu CM 0 a tn tn rH r— rH cr> in cu CM in 0 1-H I-H scu •4-> rH CD t-H rH s_ -o 4-> 00 vo 'd• r«-. 3 fO 2: CO 00 fO cu U. CM tn 0 00 CO CU cu S~ r-H CM <^ rH i- X3 cu CD rH Z3 4-> CD X 0 ex: •sd- tn O) 4-> $- CD CM to o •!-M <u cu M- 0 to r>^ I— cu J— to cr> 0 00 tn to U. C_> to fO CM CT> • C^ 0 jQ cu +J CO CO CO i. JC - ^ XJ 0 t-H XI r- E CO rH rH rs < ra CO t-H rH rH o rs o cn CO tn .E S.. 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CD CO • cn en VO CM CM CO I CM CD o CD o tn -!*• cn CO <>t- tn vo t-H cn o• o 00 tn to cn 00 CO • 00 00 CM 00 *:*• CM I O o o CO cn vo CO o in to to in CM CM CD cn rH cn t-H to t-H CD CM CM to CM CM CO CD t-H tn in • CO CM I-H t-H CM CM TH t-H CO CM CM • CM tn CO en • en CO r«» o tn CM 00 • CO CM cn vo t-H 00 o vo CM in CM 00 00 en• en I-H CM CO CO CM 00 rH VO CO • vo to r^ CO rH rH i-H «;:*• • I-H cn 'sf CD 00 CO t-H to tn cn cn in t-H cn • o CM CM • CO 1-H cn CD CM rD i>o CM I O cts. X O 00 • CO CM CM 00 • CM cn r^• CO CM CO • 00 r >. CO cn •N^ vo rH t-H CO CM • CO CM o CO CO • vo o VO CO 00 CM vo rH CO o • CM CO • CO CM CO vo• 00 00 00 •N,,^^^ o CO vo• CM Q o o LU __l CX s: to tn • 00 tn CO cn CO 'd' rH CM 1^ CO CM 00 T-H CO tn in t-H 00 o 4. 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CO 1 CO *;^ to 17.84 CM rH 0 VO «;*• CO vo CO to CM CM ^ CD « in 00 CO CM en vo rH VO CM in CO 0 t-H ^ CM t-H tn CO CM CM VO CO CM 00 CM en CO CM in vo T-H tn CM CO CM 00 t-H tn en CO vo to 0 t-H t-H T-H rH rH 0 t-H CO CM 0 CM 00 cn CO ^ CO CM • CM in 00rt ^ to *;f ^ • CM CM to 00 0 • rH to CO CM * 0 CM t-H cn cn CM CvJ 00 in 00 CO en 00 0 cn CM rH r>. r^ 0 «vj- CM to «d- 00 CO CO CO t-H CM cn 00 • CO to CO • « « CO CO tn CM C3D 0 CO in r^ CM en T-H o CD CM 1 Q 00 0 CM • tn CM ><: H- 2: LU i-H 1 CO tu —J CX CD CO • T-H CM T-H rH *;»- in • 0 rH • CO tn CO rH • CO CM rH CO tn • CO 00 CO CO CO • cn LD • t-H t-H CO o_ ID 00 tn I cn en CM • tn CM CO CM • cn cn CM CO CO • tn 00 cn in T-H in 00 Li_ <: CD CQ E .Q '^ LU _J Cu s: <x. to 03 to 5 ra cd -^-> 2: CD a: to ra • CD 3: 5 X3 CU > 0 E CU on ra 0 • Cd CM CD 1 — 0 Li_ s: • c u > <c CD CO CU S« ra CD CD CO ' • * ^ , CD 1— CQ oQ to CM 0 CU r— ra 0 cd s: VO XJ c u N •rr- r— ra CD o CD CM CM O CD CM CD rc CM CD to ra CD XJ CU N F i0 2: ra E o 79 o o CD .>Of. CO UJ LU —J CX CX CD to CO I p>. rH CM CO O CM en en t-H rH CO «;*• tn CO CM tn to tn CO 00 CD 00 CO 00 to CO in CM 00 en •sd- CO CM CO «Nt• • • CO to CO CM r>. o CO tn CM O CM to in CO 00 I-H vo CM VO CO tn cn vo CM CM to CM in CO CM CD CQ E X) to ro CD CX <; ra Cd t/O to ro CD 03 ro Od U_ CD OO CU > CD C/> CU 4-> ro CU rD CQ X> CU > o E CU Cd CM o CD c3 -to CM CD O Od X3 CU N •rr- -"vtDC (O O E o CM O CD CM rc O O sj- rc CM CD to rc CM o to ro CD XJ CU N ro E S- o 80 LENGTH OF RUNS Run Number Total Length of Time Manure Added hours 1 0.60 6 2.13 7 1.62 8 2.27 9 2.08 10 2.08