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To maximize production and minimize pumping costs, crude oil is heated to reduce its viscosity during transportation from a production field. (a) Consider a pipe-in-pipe configuration consisting of concentric steel tubes with an intervening insulating material. The inner tube is used to transport warm crude oil through cold ocean water. The inner steel pipe \(\left(k_{s}=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) has an inside diameter of \(D_{i, 1}=150 \mathrm{~mm}\) and wall thickness \(t_{i}=10 \mathrm{~mm}\) while the outer steel pipe has an inside diameter of \(D_{i, 2}=250 \mathrm{~mm}\) and wall thickness \(t_{o}=t_{i}\). Determine the maximum allowable crude oil temperature to ensure the polyurethane foam insulation \(\left(k_{p}=\right.\) \(0.075 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) between the two pipes does not exceed its maximum service temperature of \(T_{p, \max }=\) \(70^{\circ} \mathrm{C}\). The ocean water is at \(T_{\infty, o}=-5^{\circ} \mathrm{C}\) and provides an external convection heat transfer coefficient of \(h_{o}=500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The convection coefficient associated with the flowing crude oil is \(h_{i}=450 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) It is proposed to enhance the performance of the pipe-in-pipe device by replacing a thin \(\left(t_{a}=5 \mathrm{~mm}\right)\) section of polyurethane located at the outside of the inner pipe with an aerogel insulation material \(\left(k_{a}=0.012 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\). Determine the maximum allowable crude oil temperature to ensure maximum polyurethane temperatures are below \(T_{p, \max }=70^{\circ} \mathrm{C}\).

Short Answer

Expert verified
For the original configuration, the maximum allowable crude oil temperature can be found by calculating the total thermal resistance across the layers and solving for $T_{oil}$. The total thermal resistance is given by $R_{total} = R_{in} + R_{iw} + R_{insulation} + R_{ow} + R_{out}$. After calculating the resistance values, we can find the relationship between the temperature difference and the heat transfer rate, $Q = \frac{(T_{oil} - T_{\infty, o})}{R_{total}}$. Using the given values and solving for $T_{oil}$, we obtain the result for part (a). For the enhanced configuration with an aerogel layer, we modify the total thermal resistance to $R'_{total} = R_{in} + R_{iw} + R_{a} + R_{insulation} + R_{ow} + R_{out}$ and calculate the new maximum allowable crude oil temperature, $T_{oil}'$, producing the result for part (b).

Step by step solution

01

Find Temperature Distribution for Original Configuration

First, we will find the temperature distribution for the original configuration. The total thermal resistance across the layers can be given as: \[R_{total} = R_{in}+R_{iw}+R_{insulation}+R_{ow}+R_{out}\] The thermal resistances for convection at the inside and outside surfaces of the pipe are given by: \[R_{in} = \frac{1}{h_{i}A_{i}}\] and \[R_{out} = \frac{1}{h_{o}A_{o}}\] Here, \(A_{i} = \pi D_{i, 1}\) is the surface area on the inside and \(A_{o} = \pi D_{o, 2}\) is the surface area on the outside. The thermal resistances for both inner and outer pipe wall can be given by: \[R_{iw} = R_{ow} = \frac{t_i}{k_sA_{wall}}\] Here, \(A_{wall} = \frac{(D_{o, 1} + D_{i, 1})}{2}\) is the average of inside and outside wall surface areas of the pipe wall. The thermal resistance for the polyurethane insulation can be given by: \[R_{insulation} = \frac{t_p}{k_pA_p}\] Here, \(A_p = \frac{(D_{i, 2} + D_{o, 2})}{2}\) is the average of inside and outside surface areas of the insulation layer. Once all the resistance values are calculated, we can find the relationship between the temperature difference of the oil and the heat transfer rate as follows: \[Q = \frac{(T_{oil}-T_{\infty, o})}{R_{total}}\] Where the goal is to calculate \(T_{oil}\) such that \(T_{p, max} = 70^{\circ} C\).
02

Calculate Maximum Allowable Crude Oil Temperature

With the given values for the convection coefficients, diameters, thicknesses, and thermal conductivities, we can plug them into the above equations, determine the total thermal resistance, and then find the heat transfer rate. We can now calculate \(T_{p, max}\) using the total thermal resistance (considering only polyurethane insulation layer) and the maximum allowable polyurethane temperature: \[T_{oil} - T_{\infty, o} = (T_{p, max} - T_{\infty, o}) R_{total}\] Solving for the maximum allowable crude oil temperature, \(T_{oil}\), we obtain the result for part (a).
03

Enhance Configuration with an Aerogel layer

For the second part of the question, a layer of aerogel insulation is added to enhance the performance of the pipe-in-pipe device, which means modifying the \(R_{total}\) by considering the aerogel's thermal resistance. To account for this, we will consider a new total thermal resistance \(R'_{total}\) which includes the aerogel insulation layer: \[R'_{total} = R_{in}+R_{iw}+R_{a}+R_{insulation}+R_{ow}+R_{out}\] The thermal resistance for the aerogel layer can be given as: \[R_{a} = \frac{t_a}{k_aA_a}\] Here, \(A_a = \frac{D_{i, 2} + D_{i, 2} + 2 t_a}{2}\) is the average of the aerogel's inside and outside surface areas.
04

Calculate Maximum Allowable Crude Oil Temperature for Enhanced Configuration

Similar to Step 2, we can calculate the heat transfer rate and the maximum allowable crude oil temperature, holding \(T_{p, max} = 70^{\circ} C\), with the added aerogel layer: \[T_{oil}' - T_{\infty, o} = (T_{p, max} - T_{\infty, o}) R'_{total}\] Solving for the new maximum allowable crude oil temperature, \(T_{oil}'\), we obtain the result for part (b).

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Key Concepts

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

Heat Transfer
Heat transfer is a fundamental concept in thermodynamics that involves the movement of heat energy from a region of high temperature to a region of lower temperature. It occurs through three primary mechanisms: conduction, convection, and radiation. In the context of our exercise, the focus is on conduction and convection, which play critical roles in the thermal management of crude oil transportation.

In conduction, heat is transferred through a solid material due to a temperature gradient, where the heat flow is directly proportional to the thermal conductivity of the material and the temperature difference across it. On the other hand, convection involves the transfer of heat through a fluid, which is caused by the movement of the fluid itself, often induced by differences in temperature and density within the fluid. The effectiveness of convection is characterized by the convection heat transfer coefficient.
Conduction and Convection
The interplay between conduction and convection is crucial in systems where heat transfer efficiency is of utmost importance. In the textbook exercise, the oil inside the pipe and the surrounding ocean water are involved in convective heat transfer with the steel pipe and insulation material. The conduction occurs through the steel pipe and insulation material, constituting layers with different thermal resistances.

A good understanding of these processes helps in calculating and maximizing the efficiency of heat transfer systems. For example, the inner steel pipe transfers heat to the polyurethane foam by conduction while the outer surface loses heat to the ocean water through convection. Balancing these mechanisms ensures the crude oil remains at an optimal temperature to reduce viscosity for efficient pumping while not exceeding the maximum service temperature of the insulation material.
Thermal Conductivity
Thermal conductivity, represented by the symbol \(k\), is a measure of a material's ability to conduct heat. It is defined as the quantity of heat, in watts, transmitted through a cube of material 1 meter on each side in a second, for a temperature difference of 1 Kelvins between the sides. Materials with high thermal conductivity, such as steel \(\left(k_s = 35\mathrm{~W/m\cdot K}\right)\), quickly transfer heat, whereas materials with low thermal conductivity, like polyurethane foam \(\left(k_p = 0.075\mathrm{~W/m\cdot K}\right)\), are better at insulating and reduce the rate of heat loss.

In thermal resistance calculations, the thermal conductivity directly affects the resistance of the material layer. The higher the thermal conductivity, the lower the thermal resistance, meaning heat can pass through more easily. This is an important factor when designing insulation for systems like the pipe-in-pipe configuration for transporting crude oil.
Insulation Materials
Insulation materials are crucial for managing and controlling heat transfer in various applications. These materials, such as polyurethane foam and aerogel in our exercise, are selected based on their thermal properties, especially low thermal conductivity. By incorporating insulation with a low thermal conductivity, the rate of heat loss can be controlled, ensuring the crude oil in the pipe maintains the required temperature for efficient transport.

The type of insulation material and its thickness are pivotal in determining the thermal resistance of the system. For example, replacing a section of the polyurethane with aerogel insulation (with lower thermal conductivity \(k_a = 0.012 \mathrm{~W/m\cdot K}\)) demonstrates this. The aerogel provides a higher thermal resistance despite its thinness, which prevents the inner pipe's heat from being lost to the cold surroundings, allowing for higher crude oil temperatures without jeopardizing the insulation's integrity.

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Most popular questions from this chapter

The evaporator section of a refrigeration unit consists of thin-walled, 10-mm- diameter tubes through which refrigerant passes at a temperature of \(-18^{\circ} \mathrm{C}\). Air is cooled as it flows over the tubes, maintaining a surface convection coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and is subsequently routed to the refrigerator compartment. (a) For the foregoing conditions and an air temperature of \(-3^{\circ} \mathrm{C}\), what is the rate at which heat is extracted from the air per unit tube length? (b) If the refrigerator's defrost unit malfunctions, frost will slowly accumulate on the outer tube surface. Assess the effect of frost formation on the cooling capacity of a tube for frost layer thicknesses in the range \(0 \leq \delta \leq 4 \mathrm{~mm}\). Frost may be assumed to have a thermal conductivity of \(0.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). (c) The refrigerator is disconnected after the defrost unit malfunctions and a 2-mm-thick layer of frost has formed. If the tubes are in ambient air for which \(T_{\infty}=20^{\circ} \mathrm{C}\) and natural convection maintains a convection coefficient of \(2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), how long will it take for the frost to melt? The frost may be assumed to have a mass density of \(700 \mathrm{~kg} / \mathrm{m}^{3}\) and a latent heat of fusion of \(334 \mathrm{~kJ} / \mathrm{kg}\).

Consider the conditions of Problem \(3.149\) but now allow for a tube wall thickness of \(5 \mathrm{~mm}\) (inner and outer diameters of 50 and \(60 \mathrm{~mm}\) ), a fin-to-tube thermal contact resistance of \(10^{-4} \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\), and the fact that the water temperature, \(T_{w}=350 \mathrm{~K}\), is known, not the tube surface temperature. The water-side convection coefficient is \(h_{w}=2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the rate of heat transfer per unit tube length \((\mathrm{W} / \mathrm{m})\) to the water. What would be the separate effect of each of the following design changes on the heat rate: (i) elimination of the contact resistance; (ii) increasing the number of fins from four to eight; and (iii) changing the tube wall and fin material from copper to AISI 304 stainless steel \((k=20\) \(\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\) ?

A firefighter's protective clothing, referred to as a turnout coat, is typically constructed as an ensemble of three layers separated by air gaps, as shown schematically. The air gaps between the layers are \(1 \mathrm{~mm}\) thick, and heat is transferred by conduction and radiation exchange through the stagnant air. The linearized radiation coefficient for a gap may be approximated as, \(h_{\text {rad }}=\sigma\left(T_{1}+T_{2}\right)\left(T_{1}^{2}+T_{2}^{2}\right) \approx 4 \sigma T_{\text {avg }}^{3}\), where \(T_{\text {avg }}\) represents the average temperature of the surfaces comprising the gap, and the radiation flux across the gap may be expressed as \(q_{\text {rad }}^{\prime \prime}=h_{\text {rad }}\left(T_{1}-T_{2}\right)\). (a) Represent the turnout coat by a thermal circuit, labeling all the thermal resistances. Calculate and tabulate the thermal resistances per unit area \(\left(\mathrm{m}^{2}\right.\). \(\mathrm{K} / \mathrm{W}\) ) for each of the layers, as well as for the conduction and radiation processes in the gaps. Assume that a value of \(T_{\mathrm{avg}}=470 \mathrm{~K}\) may be used to approximate the radiation resistance of both gaps. Comment on the relative magnitudes of the resistances. (b) For a pre-ash-over fire environment in which firefighters often work, the typical radiant heat flux on the fire-side of the turnout coat is \(0.25 \mathrm{~W} / \mathrm{cm}^{2}\). What is the outer surface temperature of the turnout coat if the inner surface temperature is \(66^{\circ} \mathrm{C}\), a condition that would result in burn injury?

Circular copper rods of diameter \(D=1 \mathrm{~mm}\) and length \(L=25 \mathrm{~mm}\) are used to enhance heat transfer from a surface that is maintained at \(T_{s, 1}=100^{\circ} \mathrm{C}\). One end of the rod is attached to this surface (at \(x=0\) ), while the other end \((x=25 \mathrm{~mm})\) is joined to a second surface, which is maintained at \(T_{s, 2}=0^{\circ} \mathrm{C}\). Air flowing between the surfaces (and over the rods) is also at a temperature of \(T_{\infty}=0^{\circ} \mathrm{C}\), and a convection coefficient of \(h=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is maintained. (a) What is the rate of heat transfer by convection from a single copper rod to the air? (b) What is the total rate of heat transfer from a \(1 \mathrm{~m} \times 1 \mathrm{~m}\) section of the surface at \(100^{\circ} \mathrm{C}\), if a bundle of the rods is installed on 4 -mm centers?

A 40-mm-long, 2-mm-diameter pin fin is fabricated of an aluminum alloy \((k=140 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). (a) Determine the fin heat transfer rate for \(T_{b}=50^{\circ} \mathrm{C}\), \(T_{\infty}=25^{\circ} \mathrm{C}, h=1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and an adiabatic tip condition. (b) An engineer suggests that by holding the fin tip at a low temperature, the fin heat transfer rate can be increased. For \(T(x=L)=0^{\circ} \mathrm{C}\), determine the new fin heat transfer rate. Other conditions are as in part (a). (c) Plot the temperature distribution, \(T(x)\), over the range \(0 \leq x \leq L\) for the adiabatic tip case and the prescribed tip temperature case. Also show the ambient temperature in your graph. Discuss relevant features of the temperature distribution. (d) Plot the fin heat transfer rate over the range \(0 \leq h \leq 1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) for the adiabatic tip case and the prescribed tip temperature case. For the prescribed tip temperature case, what would the

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