/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 62 The heating value of a fuel oil ... [FREE SOLUTION] | 91Ó°ÊÓ

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The heating value of a fuel oil is to be measured in a constant-volume bomb calorimeter. The bomb is charged with oxygen and \(0.00215 \mathrm{lb}_{\mathrm{m}}\) of the fuel and is then sealed and immersed in an insulated container of water. The initial temperature of the system is \(77.00^{\circ} \mathrm{F}\). The fuel-oxygen mixture is ignited, and the fuel is completely consumed. The combustion products are \(\mathrm{CO}_{2}(\mathrm{g})\) and \(\mathrm{H}_{2} \mathrm{O}(\mathrm{v}) .\) The final calorimeter temperature is \(89.06^{\circ} \mathrm{F}\). The mass of the calorimeter, including the bomb and its contents, is 4.62 \(\mathrm{Ib}_{\mathrm{m}},\) and the average heat capacity of the system \(\left(C_{v}\right)\) is \(0.900 \mathrm{Btu} /\left(\mathrm{b}_{\mathrm{m}} \cdot^{\circ} \mathrm{F}\right)\). (a) Calculate \(\Delta \hat{U}_{\mathrm{S}}^{\circ}\) \(\left(\mathrm{B} \mathrm{tu} / \mathrm{lb}_{\mathrm{m}} \text { oil }\right)\) for the combustion of the fuel oil at \(77^{\circ} \mathrm{F}\). Briefly explain your calculation. (b) What more would you need to know to determine the higher heating value of the oil?

Short Answer

Expert verified
The change in internal energy of the system \(\Delta \hat{U}_{\mathrm{S}}^{\circ}\) during the combustion of the fuel oil at \(77^{\circ} \mathrm{F}\) is \(0.00215 \cdot 0.900 \cdot 12.06 Btu/lb_m\). To determine the higher heating value of the oil, one must know the water content of the oil.

Step by step solution

01

Calculation of Change in Temperature

First, calculate the change in temperature by subtracting the initial temperature from the final temperature. Temporarily ignoring the units of measurement, the change in temperature \(\Delta T\) can be calculated as \(89.06 - 77.00\).
02

Convert Change in temperature to Relevant Unit

For this calculation, it is necessary that all measurements to be in the same units. Therefore we convert the temperatures to Rankine (R) using the formula \(T(R) = T(°F) + 459.67\). This gives \(T_i = 77 + 459.67 = 536.67 R\) and \(T_f = 89.06 + 459.67 = 548.73 R\). Thus, \(\Delta T = T_f - T_i = 548.73 - 536.67 R = 12.06 R\).
03

Calculate the Change in Internal Energy

The change in internal energy \(\Delta \hat{U}_{\mathrm{S}}^{\circ}\) can be calculated using the formula \(\Delta U = m \cdot C_v \cdot \Delta T\). Here, \(m\) is the mass of the fuel, \(C_v\) is the heat capacity of the system and \(\Delta T\) is the change in temperature. Substituting the values, we have \(\Delta U = 0.00215 \cdot 0.900 \cdot 12.06 Btu/lb_m\).
04

Considerations for Determining the Higher Heating Value

To determine the higher heating value of the oil, one would need to know the water content of the oil. This is because higher heating values consider the heat produced when water vapor produced during combustion condenses.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Understand Fuel Oil Combustion in a Bomb Calorimeter
Fuel oil combustion is the process of releasing energy by burning fuel oil in the presence of oxygen. The bomb calorimeter is a device specifically designed to measure the energy release, known as the heating value, during this combustion process. When fuel oil burns completely, it forms carbon dioxide (CO2) and water vapor (H2O). The energy produced from the combustion is transferred to the surrounding environment which, in this scenario, is water.

The bomb calorimeter is a sealed and robust container, where a known amount of fuel oil is ignited in a controlled oxygen-rich environment. As the fuel burns, the resulting increase in temperature within the calorimeter is recorded. This temperature change is directly related to the internal energy released by the combustion of the fuel oil. Therefore, by carefully monitoring the temperature change, we can deduce the energy content of the fuel.
Calculating Heat Capacity
The heat capacity of a system, denoted as Cv, describes how much heat energy is needed to raise the temperature of the system by one degree. To effectively measure the released energy from fuel oil combustion, it’s vital to know the heat capacity of the calorimeter.In our exercise, the heat capacity (Cv) calculation is crucial for determining the amount of heat absorbed by the system. This value typically includes the calorimeter itself and any additional components within it, such as the bomb and water. The value is provided as 0.900 British thermal units per pound-mass-degree Fahrenheit (Btu/(lbm·°F)), indicating the calorimeter's ability to absorb heat. Knowing Cv allows us to calculate the energy change when we multiply it by the mass of the calorimeter and the change of temperature during the combustion.
Determining the Change in Internal Energy
The change in internal energy, denoted as Δ&³ó²¹³Ù;±«S, is a thermodynamic quantity that signifies the total energy change within a system undergoing a process, such as the combustion of fuel oil in a calorimeter. It’s essential for understanding how much usable energy is generated from the fuel.

The internal energy change can be calculated by the product of the mass of the fuel (m), the heat capacity of the system (Cv), and the change in temperature (Δ°Õ). This concept is applied when we use the formula ΔU = m · Cv · Δ°Õ to calculate the change in internal energy due to the combustion process within the calorimeter. The resulting value provides insights into the energy content per unit mass of the fuel oil at the specific initial temperature.
Measuring Higher Heating Value
The higher heating value (HHV) represents the total amount of heat available from the combustion of a fuel, including the condensation heat of vaporized water within the products. It’s an essential factor for determining the maximum potential energy of a fuel.

To measure HHV, additional knowledge about the fuel's water content is necessary. This is because the HHV considers the heat released when water vapor, formed during the combustion, condenses back into liquid water. The condensation releases latent heat, which contributes to the fuel's heating value. Without accounting for the water produced, one can only determine the lower heating value (LHV), which excludes this latent heat. Consequently, for a full HHV determination, experimentation should also measure or account for the moisture in the fuel and the resulting water from combustion.

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Most popular questions from this chapter

A mixture of methane, ethane, and argon at \(25^{\circ} \mathrm{C}\) is burned with excess air in a power-plant boiler. The hydrocarbons in the fuel are completely consumed. The following variable definitions will be used throughout this problem: \(x_{\mathrm{M}}=\) mole fraction of methane in the fuel \(x_{\mathrm{A}}=\) mole fraction of argon in the fuel \(P_{\mathrm{xs}}(\%)=\) percent excess air fed to the furnace \(T_{\mathrm{u}}\left(^{\circ} \mathrm{C}\right)=\) temperature of the entering air \(T_{\mathrm{s}}\left(^{\circ} \mathrm{C}\right)=\) stack gas temperature \(r=\) ratio of \(\mathrm{CO}_{2}\) to \(\mathrm{CO}\) in the stack gas \(\left(\mathrm{mol} \mathrm{CO}_{2} / \mathrm{mol} \mathrm{CO}\right)\) \(\dot{Q}(\mathrm{k} \mathrm{W})=\) rate of heat transfer from the furnace to the boiler tubes (a) Without doing any calculations, sketch the shapes of the plots you would expect to obtain for plots of \(\dot{Q}\) versus (i) \(x_{\mathrm{M}, \text { (ii) } x_{\mathrm{A}}, \text { (iii) } P_{\mathrm{xs}}, \text { (iv) } T_{\mathrm{a}},(\mathrm{v}) T_{\mathrm{s}}, \text { and }(\mathrm{vi})} r,\) assuming in each case that the other variables are held constant. Briefly state your reasoning for each plot. (b) Take a basis of 1.00 mol/s of fuel gas, draw and label a flowchart, and derive expressions for the molar flow rates of the stack gas components in terms of \(x_{\mathrm{M}}, x_{\mathrm{A}}, P_{\mathrm{xs}},\) and \(r .\) Then take as references the elements at \(25^{\circ} \mathrm{C}\), prepare and fill in an inlet-outlet enthalpy table for the furnace, and derive expressions for the specific molar enthalpies of the feed and stack gas components in terms of \(T_{\mathrm{a}}\) and \(T_{\mathrm{s}}\) (c) Calculate \(\dot{Q}(\mathrm{kW})\) for \(x_{\mathrm{M}}=0.85 \mathrm{mol} \mathrm{CH}_{\mathcal{J}} / \mathrm{mol}, x_{\mathrm{A}}=0.05 \mathrm{mol} \mathrm{Ar} / \mathrm{mol}, P_{\mathrm{xs}}=5 \%, r=10.0 \mathrm{mol}\) \(\left.\mathrm{CO}_{2} / \mathrm{mol} \mathrm{CO}, T_{\mathrm{a}}=150^{\circ} \mathrm{C}, \text { and } T_{\mathrm{s}}=700^{\circ} \mathrm{C} \text { (Solution: } \dot{Q}=-655 \mathrm{kW} .\right)\) (d) Prepare a spreadsheet that has columns for \(x_{\mathrm{M}}, x_{\mathrm{A}}, P_{\mathrm{xs}}, T_{\mathrm{a}}, r, T_{\mathrm{s}},\) and \(\dot{Q},\) plus columns for any other variables you might need for the calculation of \(\dot{Q}\) from given values of the preceding six variables (e.g., component molar flow rates and specific enthalpies). Use the spreadsheet to generate plots of \(\dot{Q}\) versus each of the following variables over the specified ranges: $$\begin{aligned}&x_{\mathrm{M}}=0.00-0.85 \mathrm{mol} \mathrm{CH}_{4} / \mathrm{mol}\\\ &x_{\mathrm{A}}=0.01-0.05 \mathrm{mol} \mathrm{Ar} / \mathrm{mol}\\\ &P_{\mathrm{xs}}=0 \%-100 \%\\\ &T_{\mathrm{a}}=25^{\circ} \mathrm{C}-250^{\circ} \mathrm{C}\\\ &r=1-100 \mathrm{mol} \mathrm{CO}_{2} / \mathrm{mol} \mathrm{CO} \text { (make the } r \text { axis logarithmic) }\\\ &T_{\mathrm{s}}=500^{\circ} \mathrm{C}-1000^{\circ} \mathrm{C}\end{aligned}$$ When generating each plot, use the variable values given in Part (c) as base values. (For example, generate a plot of \(\dot{Q}\) versus \(x_{\mathrm{M}}\) for \(x_{\mathrm{A}}=0.05, P_{\mathrm{xs}}=5 \%,\) and so on, with \(x_{\mathrm{M}}\) varying from 0.00 to 0.85 on the horizontal axis.) If possible, include the plots on the same spreadsheet as the data.

In the production of many microelectronic devices, continuous chemical vapor deposition (CVD) processes are used to deposit thin and exceptionally uniform silicon dioxide films on silicon wafers. One CVD process involves the reaction between silane and oxygen at a very low pressure. $$\mathrm{SiH}_{4}(\mathrm{g})+\mathrm{O}_{2}(\mathrm{g}) \rightarrow \mathrm{SiO}_{2}(\mathrm{s})+2 \mathrm{H}_{2}(\mathrm{g})$$ The feed gas, which contains oxygen and silane in a ratio \(8.00 \mathrm{mol} \mathrm{O}_{2} / \mathrm{mol} \mathrm{SiH}_{4},\) enters the reactor at 298 \(\mathrm{K}\) and 3.00 torr absolute. The reaction products emerge at \(1375 \mathrm{K}\) and 3.00 torr absolute. Essentially all of the silane in the feed is consumed. (a) Taking a basis of \(1 \mathrm{m}^{3}\) of feed gas, calculate the moles of each component of the feed and product mixtures and the extent of reaction, \(\xi\) (b) Calculate the standard heat of the silane oxidation reaction (kJ). Then, taking the feed and product species at \(298 \mathrm{K}\left(25^{\circ} \mathrm{C}\right)\) as references, prepare an inlet-outlet enthalpy table and calculate and fill in the component amounts (mol) and specific enthalpies (kJ/mol). (See Example 9.5-1.) Data $$\left(\Delta \hat{H}_{\mathrm{f}}\right)_{\mathrm{SiH}_{4}(\mathrm{g})}=-61.9 \mathrm{kJ} / \mathrm{mol}, \quad\left(\Delta \hat{H}_{\mathrm{f}}^{\mathrm{o}}\right)_{\mathrm{SiO}_{2}(\mathrm{s})}=-851 \mathrm{kJ} / \mathrm{mol}$$ $$\left(C_{p}\right)_{\mathrm{SiH}_{4}(g)}[\mathrm{k} \mathrm{J} /(\mathrm{mol} \cdot \mathrm{K})]=0.01118+12.2 \times 10^{-5} T-5.548 \times 10^{-8} T^{2}+6.84 \times 10^{-12} T^{3}$$ $$\left(C_{p}\right)_{\mathrm{SiO}_{2}(\mathrm{s})}[\mathrm{kJ} /(\mathrm{mol} \cdot \mathrm{K})]=0.04548+3.646 \times 10^{-5} T-1.009 \times 10^{3} / T^{2}$$ The temperatures in the formulas for \(C_{p}\) are in kelvins. (c) Calculate the heat ( \(k\) J) that must be transferred to or from the reactor (state which it is). Then determine the required heat transfer rate ( \(\mathrm{kW}\) ) required for a reactor feed of \(27.5 \mathrm{m}^{3} / \mathrm{h}\).

A gaseous fuel containing methane and ethane is burned with excess air. The fuel enters the furnace at \(25^{\circ} \mathrm{C}\) and 1 atm, and the air enters at \(200^{\circ} \mathrm{C}\) and 1 atm. The stack gas leaves the furnace at \(800^{\circ} \mathrm{C}\) and 1 atm and contains 5.32 mole\% \(\mathrm{CO}_{2}, 1.60 \%\) CO, \(7.32 \%\) O \(_{2}, 12.24 \% \mathrm{H}_{2} \mathrm{O}\), and the balance \(\mathrm{N}_{2}\). (a) Calculate the molar percentages of methane and ethane in the fuel gas and the percentage excess air fed to the reactor. (b) Calculate the heat (kJ) transferred from the reactor per cubic meter of fuel gas fed. (c) A proposal has been made to lower the feed rate of air to the furnace. State advantages and a drawback of doing so.

In a surface-coating operation, a polymer (plastic) dissolved in liquid acetone is sprayed on a solid surface and a stream of hot air is then blown over the surface, vaporizing the acetone and leaving a residual polymer film of uniform thickness. Because environmental standards do not allow discharging acetone into the atmosphere, a proposal to incinerate the stream is to be evaluated. The proposed process uses two parallel columns containing beds of solid particles. The air-acetone stream, which contains acetone and oxygen in stoichiometric proportion, enters one of the beds at \(1500 \mathrm{mm} \mathrm{Hg}\) absolute at a rate of 1410 standard cubic meters per minute. The particles in the bed have been preheated and transfer heat to the gas. The mixture ignites when its temperature reaches \(562^{\circ} \mathrm{C}\), and combustion takes place rapidly and adiabatically. The combustion products then pass through and heat the particles in the second bed, cooling down to \(350^{\circ} \mathrm{C}\) in the process. Periodically the flow is switched so that the heated outlet bed becomes the feed gas preheater/combustion reactor and vice versa. Use the following average values for \(C_{p}\left[\mathrm{kJ} /\left(\mathrm{mol} \cdot^{\circ} \mathrm{C}\right)\right]\) in solving the problems to be given: 0.126 for \(\mathrm{C}_{3} \mathrm{H}_{6} \mathrm{O}, 0.033\) for \(\mathrm{O}_{2}, 0.032\) for \(\mathrm{N}_{2}, 0.052\) for \(\mathrm{CO}_{2},\) and 0.040 for \(\mathrm{H}_{2} \mathrm{O}(\mathrm{v})\) (a) If the relative saturation of acetone in the feed stream is \(12.2 \%,\) what is the stream temperature? (b) Determine the composition of the gas after combustion, assuming that all of the acetone is converted to \(\mathrm{CO}_{2}\) and \(\mathrm{H}_{2} \mathrm{O},\) and estimate the temperature of this stream. (c) Estimate the rates ( \(\mathrm{kW}\) ) at which heat is transferred from the inlet bed particles to the feed gas prior to combustion and from the combustion gases to the outlet bed particles. Suggest an alternative to the two-bed feed switching arrangement that would achieve the same purpose.

A coal contains \(73.0 \mathrm{wt} \% \mathrm{C}, 4.7 \% \mathrm{H}\) (not including the hydrogen in the coal moisture), \(3.7 \% \mathrm{S}, 6.8 \% \mathrm{H}_{2} \mathrm{O}\) and \(11.8 \%\) ash. The coal is burned at a rate of \(50,000 \mathrm{lb}_{\mathrm{m}} / \mathrm{h}\) in a power-plant boiler with air \(50 \%\) in excess of that needed to oxidize all the carbon in the coal to \(\mathrm{CO}_{2}\). The air and coal are both fedat \(77^{\circ} \mathrm{F}\) and 1 atm. The solid residue from the furnace is analyzed and is found to contain \(28.7 \mathrm{wt} \% \mathrm{C}, 1.6 \% \mathrm{S},\) and the balance ash. The sulfur oxidized in the furnace is converted to \(\mathrm{SO}_{2}(\mathrm{g}) .\) Of the ash in the coal, \(30 \%\) emerges in the solid residue and the balance is emitted with the stack gases as fly ash. The stack gas and solid residue emerge from the furnace at \(600^{\circ} \mathrm{F}\). The higher heating value of the coal is \(18,000 \mathrm{Btu} / \mathrm{b}_{\mathrm{m}}\). (a) Calculate the mass flow rates of all components in the stack gas and the volumetric flow rate of this gas. (Tgnore the contribution of the fly ash in the latter calculation, and assume that the stack gas contains a negligible amount of CO.) (b) Assume that the heat capacity of the solid furnace residuc is \(0.22 \mathrm{Btu} /\left(\mathrm{lb}_{\mathrm{m}} \cdot^{\circ} \mathrm{F}\right),\) that of the stack gas is the heat capacity per unit mass of nitrogen, and \(35 \%\) of the heat generated in the furnace is used to produce electricity. At what rate in \(\mathrm{MW}\) is electricity produced? (c) Calculate the ratio (heat transferred from the furnace)/(heating value of the fuel). Why is this ratio less than one? (d) Suppose the air fed to the furnace were preheated rather than being fed at ambient temperature, but that everything else (feed rates, outlet temperatures, and fractional coal conversion) were the same. What effect would this change have on the ratio calculated in Part (c)? Explain. Suggest an economical way in which this preheating might be accomplished. Exploratory Exercises - Research and Discover (e) At least three components of the stack gas from the power plant raise significant environmental concerns. Identify the components, explain why they are considered problems, and describe how the problems can be addressed in a modern coal-fired power plant. (f) Several minor constituents of coal were not mentioned in the problem statement, and yet they may be part of the stack gas. Identify one such species and, as in Part (e), explain why it is a problem and how the problem cither is or could be addressed in a modern coal-fired power plant.

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