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Ethanol gas \(\left(\mathrm{C}_{2} \mathrm{H}_{6} \mathrm{O}\right)\) is burned with 110 percent theoretical air. During the combustion process, 90 percent of the carbon in the fuel is converted to \(\mathrm{CO}_{2}\) and 10 percent is converted to CO. Determine (a) the theoretical kmols of \(\mathrm{O}_{2}\) required for complete combustion of one kmol of ethanol, (b) the balanced combustion equation for the incomplete combustion process, and \((c)\) the rate of heat transfer from the combustion process, in \(\mathrm{kW},\) when \(3.5 \mathrm{kg} / \mathrm{h}\) of fuel are burned when the reactants and products are at \(25^{\circ} \mathrm{C}\) with the water in the products remaining a gas.

Short Answer

Expert verified
Answer: The theoretical kmols of O2 required for the complete combustion of Ethanol gas is 3 kmols. The rate of heat transfer during the combustion process is approximately 28.4 kW.

Step by step solution

01

Finding the balanced combustion equation for complete combustion of Ethanol gas

For complete combustion of Ethanol gas C2H6O, the balanced combustion equation is as follows: C2H6O + xO2 -> yCO2 + zH2O To balance the equation, we can set up the following relationships based on the coefficients: Carbon: 2y = 2 Hydrogen: 2z = 6 Oxygen: 2y + z = x Solving for y, z, and x, we obtain: y = 1 (for Carbon) z = 3 (for Hydrogen) x = 3 (for Oxygen) Therefore, the balanced combustion equation for complete combustion is: C2H6O + 3O2 -> 2CO2 + 3H2O
02

Find the theoretical kmols of O2 required for complete combustion

Using the balanced combustion equation from Step 1, we can see that one kmol of Ethanol gas requires 3 kmols of O2 for complete combustion. Thus, the theoretical kmols of O2 required for complete combustion is 3 kmols.
03

Find the balanced combustion equation for the incomplete combustion process

According to the given conditions, 90% of carbon is converted to CO2, and 10% is converted to CO. Therefore, we need to modify the complete combustion balanced equation accordingly. Let's replace y with 0.9 and introduce w as the coefficient for CO: C2H6O + xO2 -> 0.9(2)CO2 + wCO + 3H2O We need to balance the equation taking into consideration the incomplete combustion: Carbon: 0.9(2) + w = 2 Oxygen: 2(0.9(2)) + w = x Solving for w and x, we obtain: w = 0.2 (for Carbon) x = 3.4 (for Oxygen) Therefore, the balanced combustion equation for the incomplete combustion is: C2H6O + 3.4O2 -> 1.8CO2 + 0.2CO + 3H2O
04

Calculating the rate of heat transfer from the combustion process

Given, 3.5 kg/h of fuel is burned. First, we need to find the kmol flow rate of fuel. The molar mass of Ethanol gas (C2H6O) is: (2x12.01) + (6x1.008) + 16 = 46.068 kg/kmol Kmols of fuel burned per hour = (3.5 kg/h) / (46.068 kg/kmol) = 0.0759 kmol/h The Higher Heating Value (HHV) of Ethanol gas is approximately 1367 kJ/mol. Therefore, the heat release rate when 0.0759 kmol/h of fuel is burned will be: Heat release rate = (0.0759 kmol/h) * (1367 kJ/kmol) * (1 h / 3600 s) = 28.408 kW Consider that the reactants and products are at 25°C with the water in the products remaining a gas. The actual heat transfer rate might be slightly less than the heat release rate, but for this exercise, we can assume that the heat transfer rate is approximately the same as the heat release rate. Therefore, the rate of heat transfer from the combustion process is approximately 28.4 kW.

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Most popular questions from this chapter

Methane \(\left(\mathrm{CH}_{4}\right)\) is burned completely with 80 percent excess air during a steady-flow combustion process. If both the reactants and the products are maintained at \(25^{\circ} \mathrm{C}\) and 1 atm and the water in the products exists in the liquid form, the heat transfer from the combustion chamber per unit mass of methane is \((a) 890 \mathrm{MJ} / \mathrm{kg}\) (b) \(802 \mathrm{MJ} / \mathrm{kg}\) \((c) 75 \mathrm{MJ} / \mathrm{kg}\) \((d) 56 \mathrm{MJ} / \mathrm{kg}\) \((e) 50 \mathrm{MJ} / \mathrm{kg}\)

Gaseous E10 fuel is 10 percent ethanol \(\left(\mathrm{C}_{2} \mathrm{H}_{6} \mathrm{O}\right)\) and 90 percent octane \(\left(\mathrm{C}_{8} \mathrm{H}_{18}\right)\) on a kmol basis. This fuel is burned with 110 percent theoretical air. During the combustion process, 90 percent of the carbon in the fuel is converted to \(\mathrm{CO}_{2}\) and 10 percent is converted to CO. Determine \((a)\) the balanced combustion equation, (b) the dew-point temperature of the products, in \(^{\circ} \mathrm{C}\), for a product pressure of \(100 \mathrm{kPa}\) (c) the heat transfer for the process, in \(\mathrm{kJ}\), after \(2.5 \mathrm{kg}\) of fuel are burned and the reactants and products are at \(25^{\circ} \mathrm{C}\) with the water in the products remaining a gas, and (d) the relative humidity of atmospheric air for the case where the atmospheric air is at \(25^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\) and the products are found to contain \(9.57 \mathrm{kmol}\) of water vapor per kmol of fuel burned.

The furnace of a particular power plant can be considered to consist of two chambers: an adiabatic combustion chamber where the fuel is burned completely and adiabatically, and a heat exchanger where heat is transferred to a Carnot heat engine isothermally. The combustion gases in the heat exchanger are well mixed so that the heat exchanger is at uniform temperature at all times that is equal to the temperature of the exiting product gases, \(T_{p} .\) The work output of the Carnot heat engine can be expressed as $$ w=Q \eta_{c}=Q\left(1-\frac{T_{0}}{T_{p}}\right)$$ where \(Q\) is the magnitude of the heat transfer to the heat engine and \(T_{0}\) is the temperature of the environment. The work output of the Carnot engine will be zero either when \(T_{p}=T_{\mathrm{af}}\) (which means the product gases will enter and exit the heat exchanger at the adiabatic flame temperature \(T_{\mathrm{af}}\), and thus \(Q=0\) ) or when \(T_{p}=\) \(T_{0}\) (which means the temperature of the product gases in the heat exchanger will be \(T_{0}\), and thus \(\eta_{c}=0\) ), and will reach a maximum somewhere in between. Treating the combustion products as ideal gases with constant specific heats and assuming no change in their composition in the heat exchanger, show that the work output of the Carnot heat engine will be maximum when $$T_{p}=\sqrt{T_{\mathrm{af}} T_{0}}$$ Also, show that the maximum work output of the Carnot engine in this case becomes $$W_{\max }=C T_{\mathrm{af}}\left(1-\sqrt{\frac{T_{0}}{T_{\mathrm{af}}}}\right)^{2}$$ where \(C\) is a constant whose value depends on the composition of the product gases and their specific heats.

A gaseous fuel with a volumetric analysis of 45 percent \(\mathrm{CH}_{4}, 35\) percent \(\mathrm{H}_{2},\) and 20 percent \(\mathrm{N}_{2}\) is burned to completion with 130 percent theoretical air. Determine \((a)\) the air-fuel ratio and ( \(b\) ) the fraction of water vapor that would condense if the product gases were cooled to \(25^{\circ} \mathrm{C}\) at 1 atm.

Develop an expression for the higher heating value of a gaseous alkane \(C_{n} H_{2 n+2}\) in terms of \(n\).

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