The outer surface of an engine is situated in a place where oil leakage can occur. When leaked oil comes in contact with a hot surface that has a temperature above its autoignition temperature, the oil can ignite spontaneously. Consider an engine cover that is made of a stainless steel plate with a thickness of \(1 \mathrm{~cm}\) and a thermal conductivity of \(14 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The inner surface of the engine cover is exposed to hot air with a convection heat transfer coefficient of \(7 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) at \(333^{\circ} \mathrm{C}\). The outer surface is exposed to an environment where the ambient air is \(69^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(7 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). To prevent fire hazard in the event of oil leak on the engine cover, a layer of thermal barrier coating (TBC) with a thermal conductivity of \(1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) is applied on the engine cover outer surface. Would a TBC layer of \(4 \mathrm{~mm}\) in thickness be sufficient to keep the engine cover surface below autoignition temperature of \(200^{\circ} \mathrm{C}\) to prevent fire hazard?

Short Answer

Expert verified
Answer: Yes, the 4mm thick TBC layer is sufficient to prevent fire hazard because the calculated outer surface temperature (92.55°C) is below the autoignition temperature of 200°C.

Step by step solution

01

Calculate the heat transfer rate

We will first find the heat transfer rate through the engine cover using the given values. The heat transfer rate is given by the formula: \(q = \frac{T_{1} - T_{2}}{\frac{1}{h_{1}A} + \frac{L_{1}}{k_{1}A} + \frac{L_{2}}{k_{2}A} + \frac{1}{h_{2}A}}\) Where: \(q\) is the heat transfer rate (W) \(T_{1}\) and \(T_{2}\) are the temperatures of the inner and outer surface, respectively (K) \(h_{1}\) and \(h_{2}\) are the convection heat transfer coefficients for the inner and outer surface, respectively \((\mathrm{W} / \mathrm{m}^{2}\cdot \mathrm{K})\) \(L_{1}\) and \(L_{2}\) are the thicknesses of the stainless steel plate and TBC layer, respectively (m) \(k_{1}\) and \(k_{2}\) are the thermal conductivities of the stainless steel plate and TBC layer, respectively \((\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\) \(A\) is the surface area for heat transfer (m²) In this case, we are not given the surface area, thus we can rearrange the equation to find the heat transfer rate per unit area: \(q'= \frac{T_{1} - T_{2}}{\frac{1}{h_{1}} + \frac{L_{1}}{k_{1}} + \frac{L_{2}}{k_{2}} + \frac{1}{h_{2}}}\) Substitute the given values into the equation: \(T_{1} = 333^{\circ} \mathrm{C} + 273.15 = 606.15 \mathrm{K}\) \(T_{2} = 69^{\circ} \mathrm{C} + 273.15 = 342.15 \mathrm{K}\) \(h_{1} = h_{2} = 7 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) \(L_{1} = 1 \mathrm{~cm} = 0.01 \mathrm{~m}\) \(k_{1} = 14 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) \(L_{2} = 4 \mathrm{~mm} = 0.004 \mathrm{~m}\) \(k_{2} = 1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) Plugging these values into the formula, we get: \(q'= \frac{606.15 - 342.15}{\frac{1}{7} + \frac{0.01}{14} + \frac{0.004}{1.1} + \frac{1}{7}}\) \(q'= \frac{264}{\frac{2}{7} + \frac{1}{1400} + \frac{4}{1100}}\) Calculate \(q'\): \(q'= 158.81 \frac{\mathrm{W}}{\mathrm{m}^{2}}\)
02

Calculate the surface temperature of the outer surface of TBC layer

Now, we will find the outer surface temperature of the TBC layer (\(T_{out}\)) using the heat transfer rate per unit area and the convection heat transfer coefficient of the outer surface: \(T_{out} = T_{amb} + \frac{q'}{h_{2}}\) Where: \(T_{amb}\) is the ambient temperature (K) Substitute the given values into the equation: \(T_{out} = 342.15 + \frac{158.81}{7}\) Calculate \(T_{out}\): \(T_{out} = 365.7 \mathrm{~K}\) Convert to Celsius: \(T_{out} = 365.7 - 273.15 = 92.55^{\circ} \mathrm{C}\)
03

Compare the surface temperature with the autoignition temperature

Now we must check if the calculated surface temperature of the outer surface of TBC layer (\(T_{out}\)) is below the autoignition temperature (\(T_{auto}\)) of \(200^{\circ} \mathrm{C}\): \(T_{out} < T_{auto}\) \(92.55^{\circ} \mathrm{C} < 200^{\circ} \mathrm{C}\) Since the outer surface temperature of the TBC layer is below the autoignition temperature, the \(4 \mathrm{~mm}\) thick TBC layer is sufficient to prevent fire hazard due to oil leakage.

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Key Concepts

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

Conduction and Convection
Understanding the principles of conduction and convection is essential when analyzing heat transfer in engine covers.

Conduction refers to the transfer of heat through a solid material, such as a stainless steel engine cover. This process depends on the material's thermal conductivity, which is a measure of how easily heat passes through it. In our example, the engine cover conducts heat from its hot inner surface to its cooler outer surface.

Convection, on the other hand, involves the movement of heat between a surface and a fluid (like air or water) moving past it. The engine cover in our scenario loses heat to the ambient air through convection. This heat loss is characterized by the convection heat transfer coefficient, which quantifies the efficiency of the cooling process. A higher coefficient means the surface is better cooled by the air passing over it.

These two mechanisms jointly determine the temperature distribution across the engine cover and hence its ability to stay below the autoignition temperature of the oil in case of a leakage.
Thermal Conductivity
The concept of thermal conductivity plays a vital role in heat transfer within engine covers. It is a material property that indicates how well the material can conduct heat. Measured in watts per meter-Kelvin \(\frac{W}{m \cdot K}\), higher thermal conductivity means that heat can pass through a material more quickly.

For instance, the stainless steel of our engine cover has a thermal conductivity of \(14 \frac{W}{m \cdot K}\), while the thermal barrier coating (TBC) applied has a much lower conductivity of \(1.1 \frac{W}{m \cdot K}\). This contrast in conductivity is what allows the TBC to effectively inhibit heat transfer to the outer surface, keeping the temperature in check and preventing potential fire hazards due to oil autoignition.
Autoignition Temperature
The autoignition temperature is a critical safety metric in engineering contexts involving combustible fluids and hot surfaces. It represents the lowest temperature at which a material (in our case, engine oil) will spontaneously ignite without an external flame or spark.

For safety, the surface temperature of an engine cover must remain below the oil's autoignition temperature. In this scenario, we analyze whether the engine cover reaches a temperature higher than \(200^{\text{°}C}\), which is the autoignition point for the oil. By applying a layer of TBC with lower thermal conductivity and calculating the heat transfer process, we can ensure that the cover's temperature stays within safe limits to prevent accidental ignition.
Thermal Barrier Coating (TBC)
A Thermal Barrier Coating (TBC) is an advanced material applied to surfaces that are subjected to high temperatures, such as engine covers, to prevent heat transfer and protect underlying materials.

The TBC's effectiveness lies in its low thermal conductivity, which slows down heat conduction, and in its ability to withstand high temperatures without degradation. In the given case, a TBC layer of \(4 \text{mm}\) thickness is considered for its insulating properties. The use of TBC is a strategic decision aimed at keeping the engine cover's temperature below the oil's autoignition temperature and thereby avoiding potential fire risks.

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Most popular questions from this chapter

Hot water is to be cooled as it flows through the tubes exposed to atmospheric air. Fins are to be attached in order to enhance heat transfer. Would you recommend attaching the fins inside or outside the tubes? Why?

Consider two identical people each generating \(60 \mathrm{~W}\) of metabolic heat steadily while doing sedentary work, and dissipating it by convection and perspiration. The first person is wearing clothes made of 1 -mm-thick leather \((k=\) \(0.159 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) ) that covers half of the body while the second one is wearing clothes made of 1 -mm-thick synthetic fabric \((k=0.13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) that covers the body completely. The ambient air is at \(30^{\circ} \mathrm{C}\), the heat transfer coefficient at the outer surface is \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and the inner surface temperature of the clothes can be taken to be \(32^{\circ} \mathrm{C}\). Treating the body of each person as a 25 -cm-diameter, \(1.7-\mathrm{m}\)-long cylinder, determine the fractions of heat lost from each person by perspiration.

Explain how the fins enhance heat transfer from a surface. Also, explain how the addition of fins may actually decrease heat transfer from a surface.

A row of 3 -ft-long and 1-in-diameter used uranium fuel rods that are still radioactive are buried in the ground parallel to each other with a center-to- center distance of 8 in at a depth of \(15 \mathrm{ft}\) from the ground surface at a location where the thermal conductivity of the soil is \(0.6 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). If the surface temperature of the rods and the ground are \(350^{\circ} \mathrm{F}\) and \(60^{\circ} \mathrm{F}\), respectively, determine the rate of heat transfer from the fuel rods to the atmosphere through the soil.

A total of 10 rectangular aluminum fins \((k=\) \(203 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) are placed on the outside flat surface of an electronic device. Each fin is \(100 \mathrm{~mm}\) wide, \(20 \mathrm{~mm}\) high and \(4 \mathrm{~mm}\) thick. The fins are located parallel to each other at a center- tocenter distance of \(8 \mathrm{~mm}\). The temperature at the outside surface of the electronic device is \(60^{\circ} \mathrm{C}\). The air is at \(20^{\circ} \mathrm{C}\), and the heat transfer coefficient is \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine \((a)\) the rate of heat loss from the electronic device to the surrounding air and \((b)\) the fin effectiveness.

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