Thermochemistry of fuel air mixtures Dr. Primal Fernando primal@eng.fsu.edu Ph: (081) 2393608 1 Combustion process • Thermodynamic aspects of particular type process involving chemical reactions, is called combustion • Usually occurs between fuel and an oxygen carrier (air) • Energy stored in the bonds between constituent atoms of fuel and air (form of internal energy) and in the combustion process it will transformed to new molecules of lower energy level combustion products plus release heat (exothermic reaction) 2 Combustion process • • • • Controls the engine power Efficiency Controls the emissions Different for SI and CI engines 3 Flames • A flame is a combustion reaction propagate subsonically through space; motion of gas relative to unburn gas is important. • The existence of flame motion implies that the reaction is confined to a zone which is small in thickness compared to the engine combustion chamber. • The reaction zone is usually called the flame front • Flames can be categorized as premixed and diffusion flame (mixed together at same place where the reaction takes place) • Flames also categorized as laminar (mixing and transport done by molecular process) and turbulent (enhanced by eddies and lumps) • Flames also categorized by whether the flow is steady or unsteady 4 Fuel - fossil fuels mainly consists of H and C By mass Dry Coal Anthracite Bituminous Lignite C 90.27 74.00 56.52 H 3.00 5.98 5.72 O 2.32 13.01 31.89 N+S 1.44 2.26 1.62 Ash 2.97 4.75 4.25 By mass C H S Motor Petrol 85.5 14.4 0.1 Vaporizing oil 86.8 12.9 0.3 Kerosene 86.3 13.6 0.1 Diesel oil (gas oil) 86.3 12.8 0.9 Light Fuel oil 86.2 12.4 1.4 Heavy Fuel oil 86.1 11.8 2.1 By volume Coal gas Producer gas Blast furnace North Sea gas H2 49.4 12.0 2.0 - CO 18.0 29.0 27.0 - CH4 20.0 2.6 93.0 CnHm C4H8 2.0 C2H4 0.4 C2H6 4.8 O2 0.4 - N2 6.2 52.0 60.0 2.0 CO2 4.0 4.0 11.0 0.2 5 Chemical equation and conservation of mass Consider a simple equation C O2 CO2 1 kmol C 1 kmolO2 1 kmolCO2 12 kg C 32 kg O2 44 kg CO2 0 Vol C 1 Vol O2 1 Vol CO2 Note: all gasses occupy equal volume for kmol when they are at same pressure and temperature (exactly true for perfect gases, but for other gasses substantially true). Volume occupied by liquid and solids are negligibly small compared to gasses. 6 Chemical equation and conservation of mass C O2 CO2 1 kmol C 1 kmolO2 1 kmolCO2 12 kg C 32 kg O2 44 kg CO2 If insufficient O2 presents 1 C O2 CO 2 1 CO O2 CO2 2 0 Vol C 1 Vol O2 1 Vol CO2 1 O2 H 2 O 2 1 1 kmol H 2 kmol O2 1 kmolH 2 O 2 H2 2 kg H 2 16kg O2 18 kg H 2O 1 1 Vol H 2 Vol O2 1 Vol H 2 O (Vapour) 2 0 Vol H 2 O (liquid) 7 Necessary Oxygen is mainly obtained by mixing fuel with are Volumetric analysis % Gravimetric analysis % O2 N2 21 79 (20.95) (78.09) 23.3 76.7 Note: Molar mass of N2 is 28 kg/kmol (28.16), and that for air 29 kg/kmol (28.962) 8 Example Determine the stoichiometric air/fuel ratio for a petrol approximating to hexane C6H14. Hence deduce the chemical equation if the petrol is burnt in 20 percent excess air, and the wet volumetric analysis of the products • If all the water vapor is present •If products are cooled to an atmospheric pressure and temperature of 1 bar and 15 °C. •Determine also the dry volumetric analysis. •Estimate the chemical equation if only 80% of the air required for stoichiometric combustion is provided The partial pressure of saturated water vapor at 15 °C is 0.01704 bar 9 Solution Products C6 H14 O2 CO2 H 2O C 6 H 14 19 O2 6CO2 7 H 2 O 2 C6 H14 9.5 O2 6CO2 7H 2 O 86kg C6 H14 304kg O2 264kg CO2 126kg H 2O 23.3 kg of O2 containin 100kg of air 320 kg of O2 contain in 100 304 kg of air 23.3 100 304kg st ochiometric air/fuel ratio 23.3 15.17 86kg 10 Solution Wet volumetric analysis of the Products including N2 C 6 H 14 9.5 O2 79 9.5 N 2 6CO2 7 H 2 O 21 79 C6 H 14 1.29.5 O2 9.5 N 2 6CO2 7 H 2 O 21 79 79 C6 H 14 1.29.5 O2 9.5 N 2 6CO2 7 H 2 O 0.2 9.5 O2 1.2 9.5 N 2 21 21 1Vol C 6 H 14 1.2 9.5Vol O2 1.2 79 79 9.5 Vol N 2 6Vol CO2 7 Vol H 2 O 0.2 9.5Vol O2 1.2 9.5 Vol N 2 21 21 Amount-of-substance in the product 6CO2 7 H 2 O 0.2 9.5 O2 1.2 6 7 0.2 9.5 1.2 79 9.5 N 2 21 79 9.5 57.79 kmol or 57.79 Vol 21 11 Solution 1Vol C 6 H 14 1.2 9.5Vol O2 1.2 79 79 9.5 Vol N 2 6Vol CO2 7 Vol H 2 O 0.2 9.5Vol O2 1.2 9.5 Vol N 2 21 21 Amount-of-substance in the product 6CO2 7 H 2 O 0.2 9.5 O2 1.2 6 7 0.2 9.5 1.2 79 9.5 N 2 21 79 9.5 57.79 kmol or 57.79 Vol 21 The wet volumetric analysis 6 CO2 100 10.38% 57.5 N2 79 9.5 21 100 74.22% 57.79 1.2 7 H 2O 100 12.11% 57.79 O2 0.2 9.5 100 3.29% 57.79 12 Solution If products are cooled to an atmospheric pressure and temperature of 1 bar and 15 °C. Part of water will be condensed, if new amount of water is y, total substance is = 50.79 + y Volume fraction=Mole fraction=partial pressure/total pressure molefraction 0.01704 y 1 50.79 y y 0.88km ol totalvolume 50.79 y 50.79 0.88 51.67 Above volumetric analysis repeats base on the total volume of 51.67 CO2 11.61%; H 2O 1.7%;O2 3.68%; N2 83.01% 13 Solution Determine also the dry volumetric analysis Analysis is done by assuming no water present, then the amount of substance becomes = 50.79 Above volumetric analysis repeat base on total volume of 50.79 CO2 11.81%; O2 3.74%; N2 84.45% 14 Solution Chemical reaction with insufficient air (80%) 79 79 C6 H 14 1.29.5 O2 9.5 N 2 6CO2 7 H 2 O 0.2 9.5 O2 1.2 9.5 N 2 21 21 When insufficient O2 is given there will be unburned C and H2. H2, However, has a greater affinity for O2. If mixture is not too rich in fuel, it is reasonable to assume that all the H2 will be burnt. Some of C will be burnt to CO and other to CO2. 79 79 C6 H14 0.89.5 O2 9.5 N 2 aCO2 bCO 7 H 2O 0.8 9.5 N 2 21 21 6 ab 0.8 9.5 2 a 2 b 7 a 2.2 and b 3.8 79 79 C6 H14 0.89.5 O2 9.5 N 2 2.2CO2 3.8CO 7 H 2O 0.8 9.5 N 2 21 21 15 General combustion stoichiometry 79 79 C6 H14 9.5 O2 9.5 N 2 6CO2 7 H 2O 9.5 N 2 21 21 79 79 C6 H 14 9.5 O2 N 2 6CO2 7 H 2 O 9.5 N 2 21 21 79.05 79.05 C a H b .......... O2 N 2 ............CO2 .........H 2 O ............ N 2 20.95 20.95 Ca Hb ..........O2 3.773 N2 ............CO2 .........H 2O 3.773 ............ N2 b b b Ca H b a O2 3.773 N 2 aCO2 H 2O 3.773 a N 2 4 2 4 16 General combustion stoichiometry b b b Ca H b a O2 3.773 N 2 aCO2 H 2O 3.773 a N 2 4 2 4 b a O2 3.773 N 2 4 A Ca H b F s b a 32 3.773 28.16 4 A 12.011 a 1.008 b F s Take, y=b/a = ratio of H2 to C 34.56(4 y) A F s 12.011 1.008y 17 Energy balance QR-P Initial state reactants TR, PR, VR, UR WR-P Combustion process; heat and work transfer interaction Final state products TP, PP, VP, UP Systems changes from reactants to products (since mass constant, can apply first law for a close system) P QRP WRP U P U R WR P PdV P(VP VR ) R QRP PVP PVR U P U R PVP U P PVR U R H P H R H P,T heat of reactionat constantpressure 18