Indian Journal of Chemical Technology Vol. 11, May 2004, pp 410-422 Low temperature oxidation of ethanol S S Verma Department of Physics, Sant Longowal Institute of Engineering and Technology, Longowal, 148 106, India Received 21 September 2002; revised received 28 October 2003; accepted 29 January 2004 Oxidation characteristics of ethanol in the temperature range 200 to 1000 oC suitable to its use in automobiles are studied to highlight the role and optimum values of different combustion controlling parameters for its clean combustion. Sensitivity evaluation of different reaction paths has concluded some important reactions responsible for the ethanol oxidation. It is observed that clean combustion of ethanol can be obtained with a proper combination of combustion parameters viz., temperature, C2H5OH/O2 mole ratio and residence time. IPC Code: C07B 33/00 Keywords: Ethanol, oxidation, high-octane fuel Ethanol is a high-octane fuel with high oxygen content (35% oxygen by weight) and when blended properly in gasoline produces a cleaner and more complete combustion. Recently the interest1-7 in ethanol as a fuel extender, octane enhancer, oxygenate, and a neat fuel has increased dramatically because of the environmental concerns associated with conventional transportation fuels. Currently, ethanol and methyl tetra-butyl ether (MTBE) are the two oxygenated fuels most widely used in a number of developed countries. However, ethanol appears to be an attractive oxygenate over MTBE as it is produced from biomass; which is a renewable fuel and has roughly double the oxygen content than MTBE on an oxygen to carbon basis. Ethanol advocates1-7 base their arguments for promoting the use of this fuel on three main issues: air quality, energy security, and farm income. Ethanol is a quality fuel alternative (anti-knock) rating when blended with gasoline. It improves combustion and keeps fuel systems clean. Ethanol combustion can also contribute towards the control of global warming. As for ethanol and NOx, while there is some difference of opinion, it appears that combustion of ethanol does produce more tailpipe emissions of NOx than gasoline, because the ethanol blend can be burned as a leaner (i.e., with low fuel/air ratio) __________ E-mail: [email protected]; Fax: 01673-84657 mixture, resulting in higher combustion temperatures than with gasoline. With regulations on pollutant emissions becoming strict, the amount of oxygenated fuel like ethanol in gasoline needs to be increased. Therefore, a full understanding of the reaction pathways of oxidation of ethanol and of the pollutant species that may be produced during its combustion is needed. This understanding will allow industry and regulatory agencies to better evaluate the feasibility and relationship between the combustion process and pollutant emissions when using ethanol. Reaction pathway and sensitivity analysis are used to help identify those reactions and accompanying rate constants that exhibit a strong influence on the ethanol oxidation process. The presently considered temperature range (2001000 oC) is drawn from the literature1-4 representing the homogeneous gaseous phase as well as catalytic oxidation of ethanol at low temperatures. The oxidation kinetics of ethanol in this temperature range are investigated in order to highlight the product composition characteristics under different operating conditions such as temperature, fuel/oxygen mole ratio and residence time. Sensitivity evaluation of the chemical reactions involved in the oxidation of ethanol and the reaction involved in the formation of other important combustion species is also carried out to highlight the possible reaction paths for ethanol oxidation. VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL Computer modeling of reaction kinetics 8-12 Computational methods based on numerical integration of kinetic schemes have played a significant role in advances of reaction kinetics. Chemical systems are always complex, involving many reaction paths and equilibrium. Understanding of these complex processes is needed for application in larger or real systems. Many overall processes comprise complex reaction systems that can be represented by a number of elementary reactions, where numerical integration of the elementary reaction kinetics is used for the analysis. Chemical mechanisms, often involving hundreds of elementary reactions, are routinely used to predict species profiles in relation to time, or to engineer and optimize a given process. Although, it is now considered completely realistic to compute transient combustion schemes that allow combustion events to be studied involving full blown three dimensional thermo-fluid solutions coupled to large scale detailed kinetics schemes. But these said computation study schemes take very large computer times and the results are also not found in much disagreement with the presently adopted simple chemical kinetics scheme. Present software Presently used integration software, REACT for windows11,12 gives the convenience of simulating and modeling chemical mechanisms. It can be used to simulate complex mechanisms to predict the time dependence of reaction species concentrations to optimize synthetic processes or other chemical processes, e.g. atmospheric and combustion chemistry. The REACT code illustrates and applies numerical integration of elementary kinetic reaction equations for analysis of complex (real) chemical systems. REACT is a numerical integrator for variable-sized, simple or complex chemical kinetic systems. Elementary reactions representing a chemical system (series of chemical reactions) and their rate constants can be entered numerically (nonArrhenius form). Initial reaction conditions (times, species concentrations) are specified and REACT then numerically integrates species profiles versus time. The program illustrates the ease with which complex kinetic systems with many elementary reactions can be evaluated, or how parameters (initial concentrations, added reactions, etc.) can be changed for evaluation of sensitivity or optimization. 411 Regarding data Twenty six main chemical species namely H, O, CO, H2, O2, OH, CH3, CH4, CO2, H2O, HCO, HO2, C2H5, CH2O, H2O2, CH2OH, CH3CO, CH3OH, C2H5OH, CH3CHO, CH3CHOH, N, N2, NO, NO2 and N2O were considered in present study. Forward and backward reaction rates for considered reaction mechanism representing the interaction between these chemical species in 71 chemical reactions are given in Table 1. The forward rate coefficients for the considered 71 chemical reactions are drawn from the literature13-18. Efforts are made to include the optimum number of chemical reactions involved in the ethanol oxidation in order to give representation to different possible reaction pathways. Few termolecular reactions given earlier13-18 have been re-written as bimolecular reactions in the present reaction set considering their importance in this form. This is done due to the limitation of presently used chemical kinetic software; which deals only with unimolecular and bimolecular reactions. However, this change is expected to affect the output to a very small extent, as termolecular reactions are slow in nature. The backward rate coefficients are calculated from the forward rate coefficients and the equilibrium constants (Kp). The equilibrium constant (at P=1 atm) for each reaction was calculated from Gibbs free energy polynomials18 for each species using Kp= exp (-ΔG0T /RT). Here, it is emphasized that the rate data and the literature citation considered presently are not necessarily the "best" available data for a given reaction. In many cases, there are other citations giving the same or nearly same rate and other publications, which give a different rate for the same reaction. But, the effect of the variations in data will not change the trend of the interactions. However, it may affect the accuracy of the results. In the present investigations, the aim is just to study the interaction possibility and its dependence on operating parameters e.g., temperature, input values of C2H5OH/O2 mole ratio and residence time etc. Results and Discussion The kinetics of the considered reaction scheme given in Table 1 for ethanol oxidation under the isothermal combustion condition was studied in the lower temperature range from 200-1000 oC in order to highlight the effect of different combustion controlling parameters along with the sensitivity analysis of various reactions involved in the 412 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 Table 1 ⎯ Reaction rate coefficients (K=ATn e-E/RT) for reversible homogeneous gas-phase chemical reactions. Units of K are (cm3/mols), T is temperature and R is the ideal gas constant S.No. Chemical Reaction Forward Backward A n E A n E 1 CH3OH=CH3+OH 3.020E+18 0.00 80000.0 1.778E+11 0.00 -10985.0 2 CH3OH+O2=CH2OH+HO2 3.981E+10 0.00 50910.0 1.459E+04 0.00 37972.0 3 CH3OH+H=CH3+H2O 5.248E+12 0.00 5340.0 2.071E+12 0.00 36950.0 4 CH2OH=CH2O+H 2.511E+13 0.00 29000.0 4.144E+13 0.00 -35030.0 5 CH2OH+O2=CH2O+HO2 1.000E+12 0.00 6000.0 8.736E+17 0.00 -8298.0 6 CH2OH+H=CH2O+H2 3.012E+12 0.00 0.0 7.693E+18 0.00 43410.0 7 CH4=CH3+H 1.995E+17 0.00 88000.0 4.935E+10 0.00 -19920.0 8 CH4+O2=CH3+HO2 7.943E+13 0.00 56000.0 1.040E+13 0.00 -2188.0 9 CH4+H=CH3+H2 2.239E+04 3.00 8750.0 8.571E+03 3.00 8270.0 10 CH4+OH=CH3+H2O 3.467E+03 3.08 2000.0 5.746E+03 3.08 16675.0 11 CH4+O=CH3+OH 1.175E+07 2.08 7630.0 1.975E+06 2.08 505.0 12 CH4+HO2=CH3+H2O2 1.995E+13 0.00 18000.0 1.042E+13 0.00 1448.0 13 CH2O+OH=HCO+H2O 7.586E+12 0.00 170.0 2.623E+12 0.00 29997.0 14 CH2O+H=HCO+H2 3.311E+14 0.00 10500.0 2.644E+13 0.00 25172.0 15 CH2O+O=HCO+OH 5.012E+13 0.00 4600.0 1.758E+12 0.00 17177.0 16 CH2O+HO2=HCO+H2O2 1.000E+12 0.00 8000.0 1.090E+11 0.00 6600.0 17 HCO=H+CO 1.445E+14 0.00 19000.0 6.123E+08 0.00 1558.0 18 HCO+O2=CO+HO2 3.311E+12 0.00 7000.0 7.427E+12 0.00 39290.0 19 HCO+OH=CO+H2O 1.000E+14 0.00 0.0 2.839E+15 0.00 105133.0 20 HCO+H=CO+H2 1.995E+14 0.00 0.0 1.311E+15 0.00 89998.0 21 HCO+O=CO+OH 1.000E+14 0.00 0.0 2.880E+14 0.00 87903.0 22 CO+O=CO2 5.888E+15 0.00 4100.0 4.482E+23 0.00 131780.0 23 CO+O2=CO2+O 2.512E+12 0.00 47690.0 2.221E+13 0.00 53910.0 24 CO+OH=CO2+H 1.513E+08 1.30 -770.0 1.695E+10 1.30 21565.0 25 CO+HO2=CO2+OH 5.754E+13 0.00 22930.0 6.533E+14 0.00 84763.0 26 H2+O2=OH+OH 1.700E+13 0.00 47780.0 5.895E+11 0.00 29570.0 27 OH+H2=H2O+H 1.170E+09 1.30 3626.0 5.066E+09 1.30 18781.0 28 O+OH=O2+H 4.000E+14 -0.50 0.0 5.066E+15 -0.50 16115.0 29 O+H2=OH+H 5.060E+04 2.67 6290.0 2.222E+04 2.67 4195.0 …Contd. 413 VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL Table 1 ⎯ Reaction rate coefficients (K=ATn e-E/RT) for reversible homogeneous gas-phase chemical reactions. Units of K are (cm3/mols), T is temperature and R is the ideal gas constant ⎯ Continued S.No. Chemical Reaction Forward Backward A n E A n E 30 H+O2=HO2 3.610E+17 -0.72 0.0 1.911E+23 -0.72 49732.0 31 OH+HO2=H2O+O2 7.500E+12 0.00 0.0 9.493E+13 0.00 72863.0 32 H+HO2=OH+OH 1.400E+13 0.00 1073.0 1.798E+13 0.00 56685.0 34 OH+OH=O+H2O 6.000E+08 1.30 0.0 5.915E+09 1.30 17250.0 35 H+H=H2 1.000E+18 -1.00 0.0 1.548E+24 -1.00 107440.0 36 H+OH=H2O 1.600E+22 -2.00 0.0 1.072E+29 -2.00 122593.0 37 O+O=O2 1.890E+13 0.00 -1788.0 1.627E+21 0.00 119672.0 38 H+HO2=H2+O2 1.250E+13 0.00 0.0 3.654E+13 0.00 57708.0 39 HO2+HO2=H2O2+O2 2.000E+12 0.00 0.0 7.980E+12 0.00 41636.0 40 H2O2+H=HO2+H2 1.600E+12 0.00 3800.0 1.172E+12 0.00 19872.0 41 H2O2+OH=H2O+H 1.000E+13 0.00 1800.0 5.992E+07 0.00 -16705.0 42 C2H5OH=CH3+CH2OH 3.020E+18 0.00 75470.0 2.787E+04 0.00 22860.0 43 C2H5OH+O2=CH3CHOH+H2 3.981E+10 0.00 50000.0 3.137E+06 0.00 27702.0 44 C2H5OH+OH=CH3CHOH+H2O 3.020E+13 0.00 5960.0 3.013E+10 0.00 56525.0 45 C2H5OH+H=CH3CHOH+H2 4.365E+12 0.00 4570.0 1.006E+09 0.00 39980.0 46 C2H5OH+O=CH3CHOH+OH 6.760E+12 0.00 1510.0 6.840E+08 0.00 34825.0 47 C2H5OH+HO2=CH3CHOH+H2O2 6.309E+12 0.00 15000.0 1.984E+09 0.00 34338.0 48 C2H5OH+CH3=CH3CHOH+CH4 3.980E+12 0.00 9690.0 2.396E+09 0.00 45580.0 49 CH3CHOH=CH3CHO+H 5.012E+13 0.00 21850.0 4.029E+10 0.00 -31870.0 50 CH3CHOH+O2=CH3CHO+HO2 1.000E+13 0.00 5560.0 4.255E+15 0.00 1572.0 51 C2H5OH+H=C2H5+H2O 5.248E+12 0.00 5000.0 1.565E+12 0.00 34510.0 52 CH3CHO=CH3+HCO 7.079E+15 0.00 81760.0 4.647E+07 0.00 -1898.0 53 CH3CHO=CH3CO+H 5.012E+14 0.00 87860.0 1.428E+08 0.00 -115.0 54 CH3CHO+O2=CH3CO+HO2 1.995E+13 0.50 42200.0 3.008E+12 0.50 3957.0 55 CH3CHO+H=CH3CO+H2 3.981E+13 0.00 4200.0 1.755E+13 0.00 23665.0 56 CH3CHO+OH=CH3CO+H2O 1.000E+13 0.00 0.0 1.908E+13 0.00 34620.0 57 CH3CHO+O=CH3CO+OH 5.012E+12 0.00 1790.0 9.702E+11 0.00 19160.0 58 CH3CHO+CH3=CH3CO+CH4 1.698E+12 0.00 8430.0 1.945E+12 0.00 28375.0 59 CH3CHO+HO2=CH3CO+H2O2 1.698E+12 0.00 10700.0 1.022E+12 0.00 14093.0 ⎯ Contd. 414 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 Table 1 ⎯ Reaction rate coefficients (K=ATn e-E/RT) for reversible homogeneous gas-phase chemical reactions. Units of K are (cm3/mols), T is temperature and R is the ideal gas constant ⎯ Continued S.No. Chemical Reaction Forward Backward A n E A n E 60 CH3CO=CH3+CO 3.020E+13 0.00 17240.0 2.950E+06 0.00 4115.0 61 CO2+N=NO+CO 1.900E+11 0.00 3400.0 4.593E+09 0.00 29130.0 62 HO2+NO=NO2+OH 2.110E+12 0.00 -479.0 8.453E+12 0.00 8238.0 63 NO2+H=NO+OH 3.500E+14 0.00 1500.0 8.860E+12 0.00 32281.0 64 NO2+O=NO+O2 1.000E+13 0.00 600.0 3.206E+12 0.00 47496.0 65 N2O+H=N2+OH 7.600E+13 0.00 15200.0 3.697E+12 0.00 80375.0 66 N2O=N2+O 1.600E+14 0.00 51600.0 1.145E+07 0.00 11430.0 67 N2O+O=N2+O2 1.000E+14 0.00 28200.0 6.161E+13 0.00 109490.0 68 N2O+O=NO+NO 1.000E+14 0.00 28200.0 2.908E+12 0.00 66250.0 69 N+NO=N2+O 3.270E+12 0.30 0.0 1.481E+13 0.30 75190.0 70 N+O2=NO+O 6.400E+09 1.00 6280.0 1.368E+09 1.00 38230.0 71 N+OH=NO+H 3.800E+13 0.00 0.0 1.029E+14 0.00 48065.0 formation/destruction of different chemical species. In the present studies, isothermal calculation at constant pressure condition is considered. Though, with the difficulty in quick removal of heat to keep the temperature constant, particularly, for very small residence times, an adiabatic calculation would be further valuable. A low temperature oxidation study of ethanol reported in literature2,3 is generally in presence of catalysts that involves both homogeneous and heterogeneous reactions with large residence times. Present studies consider only gaseous phase homogeneous reactions and results under these conditions are well in comparison with the quoted results4. Moreover, the present results will help in understanding of concentration characteristics of ethanol combustion species at lower temperatures, which will be useful in optimizing its (ethanol) catalytic oxidation. Effect of temperature Figure 1 shows the combustion characteristics of ethanol left after combustion vs. residence time for different temperatures. It is found from Fig. 1, that significant ethanol combustion does not take place up to a temperature of 300 oC. But for a temperature of 400oC, the combustion of ethanol moves towards complete combustion. Similar trend is observed for higher temperatures also with a drastic reduction in residence time value. The formation and destruction of various combustion species in general and undesired chemical species such as NOx and CO in particular from ethanol combustion was studied in the lower temperature range (i.e., 200-1000oC) as a function of input C2H5OH/O2 mole ratio and residence time. C2H5OH/O2 mole ratio of 0.001/0.20 was found to be optimum in terms of controlled emission of CO and NO from C2H5OH combustion. Table 2 shows the detailed formation characteristics as well as order of magnitude for all 26 chemical species under consideration with combustion temperatures and residence time from ethanol combustion. From the Table 2 it is clear that the orders of magnitude of equilibrium formation for significant chemical species for a temperature rise from 500 to 1000oC change very slowly. Which means that a lower value in the range of 500-1000oC can be set for optimum combustion temperature with minimum/optimized emission of undesired gaseous products. However, the strong influence of combustion temperature on the formation of nitric oxides in the absence of fuel VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL 415 Fig. 1 ⎯ Oxidation profile of ethanol left after combustion with residence time for different combustion temperatures nitrogen as well as the prominence of transit chemical species at higher temperatures have been the basis for the selection of temperature value to 1000oC in the present investigations and C2H5OH/O2 mole ratio of 0.01/02.0 (an optimum value) was taken as input. clear that even with a combustion temperature of 1000oC (highest value selected in temperature range for present investigations), the formation of chemical species viz., NO, N2O, NO2, N and HCO is to a minimum level. Figures 2-5 show the formation/destruction behavior of various considered chemical species with residence time for a temperature of 1000oC and C2H5OH/O2 input value of 0.01/0.20. Figure 2 shows the formation of major chemical species CH4, CO2 and H2O along with CO, CH2OH and CH3CHO. Production of species like CH4 and CH2OH is also predicted4 to be dominant in the considered temperature range. Figure 3 shows formation of semi major chemical species such as C2H5, H2, CH3CHOH and H2O2. Further species viz., CH3OH, CH3 and HO2 formed in minor quantities are shown in Fig. 4. The chemical species formed in small quantities but mainly responsible in chemical kinetics are shown in Fig. 5. Other few left species viz., NO, N2O, NO2, N and HCO are all formed in very small concentrations (i.e., less than 10-10 mole/L) as seen from Table 2. The formation and destruction of these various chemical species shown in Figs 2 to 5, are a strong function of residence time and are shown for larger temperature only in the considered lower temperature range. It is Effect of C2H5OH/O2 ratio The C2H5OH/O2 mole ratio was varied with its values of 0.005/0.205, 0.01/0.20, 0.05/0.16, 0.10/0.11 and 0.15/0.06 keeping nitrogen content constant and these values are represented in the figures with scripts 'a', 'b', 'c', 'd' and 'e' respectively. Though the thermodynamic properties of the combustion products may change as the composition changes, while the reactions proceed but are considered to be invariant in the present investigations. The C2H5OH combustion characteristics were studied for a combustion temperature of 1000oC. Fig. 6 shows the C2H5OH combustion characteristics for different input values of C2H5OH/O2 mole ratio for a temperature of 1000oC. Figure 6 indicates the complete combustion of ethanol irrespective to its input value. This trend was found similar for any temperature higher than the minimum required temperature for ethanol combustion. Only there is a reduction in the residence time with the increase in temperature. Fig. 7 and 8 show the dependence of CO and NO formation with 416 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 Fig. 2 ⎯ Concentration of major chemical species with residence time for ethanol oxidation Residence time (μs) Fig. 3 ⎯ Concentration of semi major chemical species with residence time for ethanol oxidation residence time for different input values of C2H5OH/O2 mole ratio. From these figures it is clear that CO formation increases whereas NO concentration decreases with the increase in ethanol concentration in the reactants. This indicates the preference for higher input values of ethanol for low NO output. However, the order of magnitude of nitrogen oxides is small enough even with a VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL 417 Fig. 4 ⎯ Concentration of minor chemical species with residence time for ethanol oxidation Fig. 5 ⎯ Concentration of other minor chemical species with residence time for ethanol oxidation temperature of 1000oC and with minimum input value of ethanol. Whereas the CO and CO2 concentration rise considerably for higher input values of ethanol. From the present studies, therefore, ethanol/oxygen mole ratio between 0.01/0.20 (b) and 0.05/0.16 (c) comes to be an optimum input value in order to balance the output concentrations of CO, CO2 and NO from ethanol combustion in the lower temperature range. Effect of residence time Residence time required for the equilibrium formation/destruction of various chemical species depends largely on temperature of combustion. Table 2 shows that residence time becomes smaller for higher temperatures. Keeping same residence time for different temperature or for same temperature with different residence times will not affect the 418 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 Table 2 ⎯ Variation of concentration (≈) of different chemical species with temperature from ethanol combustion in the lower temperature range with input conditions of C2H5OH=1%, N2=79% and O2=20% Order of concentration (Moles/liter)(≈10-x), x is given in the table below S.No. Temperature (oC) (Residence time) Chemical 1000 Species 200 300 400 500 600 800 (0-10s) (0-10s) (0-0.5s) (0-0.1s) (0-0.003s) (0-0.0001s) (0-2x10-6s) 1 H 30 22 18 15 12 09 07 2 N 30 30 30 30 29 17 14 3 O 30 21 19 17 14 10 07 4 CO 15 04 03 03 03 03 03 5 H2 22 12 09 06 05 04 04 6 N2 * * * * * * * 7 NO 30 30 30 29 25 16 13 8 O2 * 01 01 01 01 01 01 9 OH 30 18 14 13 11 09 07 10 CH3 22 14 12 11 09 08 05 11 CH4 15 05 03 02 02 02 02 12 CO2 25 07 04 03 03 03 03 13 H2O 22 07 04 03 03 03 03 14 HCO 30 24 20 17 16 13 12 15 HO2 14 09 08 07 06 05 05 16 N2O 30 18 16 14 13 11 09 17 NO2 30 30 29 25 22 21 17 18 C2H5 22 12 09 07 06 04 04 19 CH2O 18 15 13 11 10 08 07 20 H2O2 10 04 03 02 02 02 04 21 CH2OH 19 12 09 07 06 04 03 22 CH3CO 21 11 10 09 09 08 07 23 CH3OH 30 15 12 11 10 08 07 24 C2H5OH * 03 03 ** ** ** ** 25 CH3CHO 10 05 03 03 03 03 03 26 CH3CHOH 18 08 06 05 05 04 04 *-Indicates species concentration changed by less than 0.001% during the reaction **-Shows overall consumption of species concentration VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL Fig. 6 ⎯ Profiles of ethanol combustion as a function of C2H5OH/O2 input ratio Fig. 7 ⎯ Formation characteristics of CO with residence time as a function of C2H5OH/O2 input ratio 419 420 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 Fig. 8 ⎯ Formation characteristics of NO with residence time as a function of C2H5OH/O2 input ratio equilibrium values of species but only expedite or slow their (species) formation/destruction for higher or lower temperatures respectively. Further studies indicate that residence time for the equilibrium values of species does not depend on the input value of C2H5OH/O2. Sensitivity evaluation Sensitivity analysis of the various chemical reactions related to the ethanol dissociation and formation of end products viz., CO, CO2 and NO was carried out to highlight the reaction paths responsible for oxidation. The input conditions were taken with C2H5OH/O2 mole ratio equal to 0.15/0.06 (that means the fuel-rich condition) and combustion temperature of 1000oC. With these input conditions, ethanol combustion can act as a low source of nitric oxides. Ethanol combustion Sensitivity evaluation of chemical reactions R42, R43, R44, R45, R46, R47, R48 and R51 involved in the ethanol consumption was carried out and it is concluded that the presence of all these reactions contribute towards 100% combustion of ethanol at temperature ≥ 400oC. However, the main chemical reactions, which contribute towards 90% combustion of ethanol are R42 and R48. Chemical reaction (R42) individually contribute towards 50% consumption of ethanol. C2H5OH=CH3 + CH2OH … (R42) C2H5OH + CH3 = CH3CHOH + CH4 … (R48) CH3CO formation Sensitivity evaluation of chemical reactions R53, R54, R55, R56, R57, R58 and R59 involved in the dissociation of CH3CHO into CH3CO show that the combination of R54 and R55 is mainly responsible for the formation (about 90%) of CH3CO. CH3CHO + O2 = CH3CO + HO2 … (R54) CH3CHO + H = CH3CO + H2 … (R55) CO formation Almost all the CO formation during ethanol combustion in the lower temperature range takes place through chemical reaction CH3CO= CH3 + CO (R60) CO2 formation Sensitivity evaluation of chemical reactions R22, R23, R24 and R25 involved in the CO2 formation from CO shows that a combination of R22 and R24 is VERMA: LOW TEMPERATURE OXIDATION OF ETHANOL responsible for about 74% conversion of CO into CO2 and rest 25% is being converted with help of R23 and R25. 421 CO and CH2OH; however, for large residence times and with the rise in temperature chemical species CH4 and CH2OH further oxidize into final equilibrium species like CO, CO2 and H2O CO + O = CO2 … (R22) CO + OH = CO2 + H … (R24) • Sensitivity evaluation of main chemical reactions R69 and R71 involved in production of NO pointed out that the main reaction responsible in NO formation in the lower temperature range is the reverse reaction of R69 and contributes alone towards 99.9% formation of NO at T = 1000oC Sensitivity analysis shows that the ethanol combustion proceeds in the following manner with reaction paths mainly responsible given in the brackets C2H5OH [R42 + R48] → CH3CHO [R54 + R55] → CO [R60] → CO2 [R22 + R24] • In the lower temperature range clean combustion (i.e., less formation of CO and CO2) of ethanol can be achieved with leaner-fuel conditions because the order of different nitrogen oxides (NO, NO2 and N2O) formation up to a temperature of 1000oC is less than 10-10 moles/liter. NO formation N+NO=N2+O … (R69) From this sensitivity evaluation of various chemical reactions responsible for the formation and destruction of different chemical species, the overall reaction chain responsible for the ethanol combustion can be laid down as: Acknowledgement C2H5OH [C2H5OH=CH3 + CH2OH (R42); C2H5OH + CH3 = CH3CHOH + CH4 (R48)] → CH3CHO [CH3CHO + O2 = CH3CO + HO2 (R54); CH3CHO + H = CH3CO + H2 (R55)] → CO [CH3CO= CH3 + CO (R60)] → CO2 [CO + O=CO2 (R22); CO + OH=CO2 + H (R24)] References The financial support by the Council of Scientific and Industrial Research (CSIR), Govt. of India as a research project no. 22(0317)/EMR-II is highly acknowledged. 1 Marinov N M, Int J Chem Kinet, 31 (1999) 183. 2 Borisov A A, Zamanskii V M, Konnov A A, Lissyanskii V V, Rusakov S A & Skachkov G I, Sov Hem Phys, 8 (1991) 121. 3 Bell-Parikh L C & Guengerich F P, J Biol Chem, 274 (34) (1999) 23833. 4 Park J, Zhu R S & Lin M C, J Chem Phy, 117(7) (2002) 3224. 5 Das A K, Nandini Chem J, 7 (2000) 4. 6 McGraw-Hill Encyclopedia of Science & Technology, 18th edn (McGraw-Hill Publishing House, USA), 1997. 7 Website: http://www.yahoo.com/ethanol combustion. Conclusions From the present investigations related to ethanol oxidation in the lower temperature range following conclusions are drawn: • Combustion of ethanol takes combustion temperature ≥ 400oC • Further rise in temperature leads to a complete combustion of ethanol in a reduced residence time place at a • Combustion with higher input values of ethanol in the reactants, increases CO and CO2 but decreases NO concentration in the combustion products 8 Glarborg P, Kee R J, Grcar J F & Miller J A, PSR: A Fortran Program for Modeling Well-Stirred Reactors, Sandia National Laboratories Report SAND 86-8209 (1986). • The order of magnitude of species viz., CO and CO2 concentrations in the combustion products is more dependent on the input value ethanol as compared to the combustion temperature 9 Lutz A E, Kee R J & Miller J A, SENKIN: A Fortran Program for Predicting Homogeneous Gas Phase Chemical Kinetics with Sensitivity Analysis, Sandia National Laboratories Report SAND 87-8248 (1988). 10 Kee R J, Rupley F M & Miller J A, CHEMKIN-II: A Fortran Chemical Kinetics Package for the Analysis of Gas-Phase Chemical Kinetics, Sandia National Laboratories Report SAND 89-8009 (1989). 11 Bozzelli J W, J Chem Edu, 77 (2000) 165. 12 Manka M J, REACT for windows: A Software for Chemical Kinetics and Reactivity, Alchemy software, 1610 Clearglades Drive, Wesley Chapel, FL 33543 (USA). • • For combustion temperatures higher than its minimum required value, complete oxidation of ethanol takes place irrespective to its (ethanol) input value Major species of ethanol combustion products in the lower temperature range are CH4, H2O, CO2, 422 INDIAN J CHEM TECHNOL, VOL 11, MAY 2004 13 Westbrook C K & Dryer F L, Prog Energy Combust Sci, 10 (1984) 57. 14 Pitz W J & Westbrook C K, Combust Flame, 63 (1986) 113. 15 Dagant P, Combust Sci Tech, 56 (1987) 23. 16 Warnatz J, Mass U & Dibble R W, Combust, 2nd edn (Springer, USA), 1999. 17 Feitelberg A S & Corream S M, J Engineering for Gas Turbines and Power (Transactions of the ASME), 122 (2000) 287. 18 Burcat A, Third millennium ideal gas and condensed phase thermodynamical database for combustion. Technion Aerospace Engineering (TAE) Report #867, http://ftp.technion.ac.il/pub/supported/aetdd/thermodynamics, 2001.
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