/*! 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 54 An ocean thermal energy conversi... [FREE SOLUTION] | 91影视

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An ocean thermal energy conversion system is being proposed for electric power generation. Such a system is based on the standard power cycle for which the working fluid is evaporated, passed through a turbine, and subsequently condensed. The system is to be used in very special locations for which the oceanic water temperature near the surface is approximately \(300 \mathrm{~K}\), while the temperature at reasonable depths is approximately \(280 \mathrm{~K}\). The warmer water is used as a heat source to evaporate the working fluid, while the colder water is used as a heat sink for condensation of the fluid. Consider a power plant that is to generate \(2 \mathrm{MW}\) of electricity at an efficiency (electric power output per heat input) of \(3 \%\). The evaporator is a heat exchanger consisting of a single shell with many tubes executing two passes. If the working fluid is evaporated at its phase change temperature of \(290 \mathrm{~K}\), with ocean water entering at \(300 \mathrm{~K}\) and leaving at \(292 \mathrm{~K}\), what is the heat exchanger area required for the evaporator? What flow rate must be maintained for the water passing through the evaporator? The overall heat transfer coefficient may be approximated as \(1200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\).

Short Answer

Expert verified
The heat exchanger area required for the evaporator in the ocean thermal energy conversion system is approximately \(8516 \mathrm{~m^2}\), while the flow rate for the water passing through the evaporator must be maintained at approximately \(1945 \mathrm{~kg/s}\).

Step by step solution

01

Calculate the heat input

Given that the power plant generates 2 MW of electricity at an efficiency of 3%, we can calculate the heat input (Q_in) as follows: Efficiency = (Electric Power Output) / (Heat Input) => Heat Input = (Electric Power Output) / Efficiency \[Q_{in} = \frac{2 \times 10^6 \mathrm{~W}}{0.03} = 6.67 \times 10^7 \mathrm{~W}\]
02

Calculate the heat transfer rate in the evaporator

The heat transfer rate (Q_evaporator) can be calculated as the difference between the heat input and the electric power output: \[Q_{evaporator} = Q_{in} - P_{output} \] \[Q_{evaporator} = 6.67 \times 10^7 \mathrm{~W} - 2 \times 10^6 \mathrm{~W} = 6.47 \times 10^7 \mathrm{~W}\]
03

Calculate the required heat exchanger area

We are given the overall heat transfer coefficient (U) as 1200 W/m虏路K. To find the heat exchanger area (A), we can use the following equation: \[Q_{evaporator} = U \cdot A \cdot \Delta T_{lm}\] where \(\Delta T_{lm}\) is the log mean temperature difference. We can calculate \(\Delta T_{lm}\) as follows: \[\Delta T_{lm} = \frac{(\Delta T_1 - \Delta T_2)}{\ln(\frac{\Delta T_1}{\Delta T_2})}\] We know that ocean water enters at 300 K and leaves at 292 K, and the working fluid is evaporated at 290 K. So, we have: \[\Delta T_1 = T_{in} - T_{evaporation} = 300 K - 290 K = 10 K\] \[\Delta T_2 = T_{out} - T_{evaporation} = 292 K - 290 K = 2 K\] Now we can calculate \(\Delta T_{lm}\): \[\Delta T_{lm} = \frac{(10 K - 2 K)}{\ln(\frac{10 K}{2 K})} \approx 6.37 K\] Then we can find the heat exchanger area (A): \[A = \frac{Q_{evaporator}}{U \cdot \Delta T_{lm}}\] \[A = \frac{6.47 \times 10^7 \mathrm{~W}}{1200 \mathrm{~W/m^2 \cdot K} \cdot 6.37 \mathrm{~K}} \approx 8516 \mathrm{~m^2}\]
04

Calculate the flow rate for the water

The flow rate (峁) can be calculated using the specific heat capacity (c_p) of the water and the temperature difference. \[Q_{evaporator} = \dot{m} \cdot c_p \cdot \Delta T\] We know that the specific heat capacity of water is approximately 4.18 kJ/kg路K. Therefore, we have: \[6.47 \times 10^7 \mathrm{~W} = \dot{m} \cdot 4.18 \times 10^3 \mathrm{~J/kg \cdot K} \cdot (300 K - 292 K)\] Now we can solve for the flow rate (峁): \[\dot{m} = \frac{6.47 \times 10^7 \mathrm{~W}}{4.18 \times 10^3 \mathrm{~J/kg \cdot K} \cdot 8 K} \approx 1945 \mathrm{~kg/s}\] So, the heat exchanger area required for the evaporator is approximately 8516 m虏 and the flow rate for the water passing through the evaporator is approximately 1945 kg/s.

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Key Concepts

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

Ocean Thermal Energy Conversion (OTEC)
Ocean Thermal Energy Conversion (OTEC) is a fascinating process that uses the natural temperature difference between warm surface seawater and cold deep seawater to generate electricity. This method is particularly effective in tropical regions where the surface ocean temperatures are consistently warmer than deeper water levels. In an OTEC system, warm surface water is used to heat and vaporize a working fluid, which then drives a turbine to produce electricity. After passing through the turbine, the vaporized fluid is cooled by deep ocean water, causing it to condense back into a liquid, ready to be used again.

The key advantage of OTEC is that it provides a continuous source of renewable energy, assuming the temperature gradient between surface and deep waters is sufficient. However, successful OTEC systems require careful engineering design, especially in the heat exchanger components, to ensure efficient and effective energy transfer. The goal is to maximize energy extraction while maintaining environmental sustainability.
Power Cycle Efficiency
Power cycle efficiency is a measure of how effectively a power cycle converts heat energy into electric energy. It is defined as the ratio of the electric power output produced by the cycle to the heat energy input into the system. In our exercise, the OTEC plant operates with a power cycle efficiency of 3%, meaning that only 3% of the heat energy from the warm seawater is converted into electricity.

This might seem low compared to other power generation methods, but it reflects the inherent challenges of working with such small temperature differences in OTEC systems. The efficiency is limited by the second law of thermodynamics, which restricts efficiency based on the available temperature range. Improving efficiency could involve optimizing the working fluid properties, enhancing the heat exchanger design, and using advanced materials to minimize energy losses.
  • The formula for efficiency is: \[ \text{Efficiency} = \frac{\text{Electric Power Output}}{\text{Heat Input}} \]
  • Efficiency factors include fluid choice, turbine effectiveness, and heat transfer optimization.
Overall Heat Transfer Coefficient
The overall heat transfer coefficient is a crucial parameter in the design and operation of a heat exchanger. It represents the heat transfer capability of the exchanger and incorporates the effects of conduction and convection on both the inside and outside surfaces of the exchanger. A higher overall heat transfer coefficient signifies more efficient heat transfer between the working fluid and seawater in the OTEC system.

In this exercise, an approximate value of 1200 W/m虏路K is provided for the heat exchanger in the evaporator. This value influences the design, particularly the surface area required to achieve the necessary heat transfer to evaporate the working fluid. The formula used in our solution, \( Q = U \cdot A \cdot \Delta T_{lm} \), connects the transfer rate \( Q \) with the heat transfer coefficient \( U \), heat exchanger area \( A \), and the logarithmic mean temperature difference \( \Delta T_{lm} \). Keeping this value optimal involves selecting appropriate materials and maintaining cleanliness to avoid fouling.

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Most popular questions from this chapter

Consider a concentric tube heat exchanger characterized by a uniform overall heat transfer coefficient and operating under the following conditions: \begin{tabular}{lccrc} \hline & \(\dot{m}\) \((\mathbf{k g} / \mathbf{s})\) & \(c_{p}\) \((\mathbf{J} / \mathbf{k g} \cdot \mathbf{K})\) & \(T_{i}\) \((\boldsymbol{C})\) & \(T_{o}\) \((\mathbf{C})\) \\ \hline Cold fluid & \(0.125\) & 4200 & 40 & 95 \\ Hot fluid & \(0.125\) & 2100 & 210 & \(-\) \\ \hline \end{tabular} What is the maximum possible heat transfer rate? What is the heat exchanger effectiveness? Should the heat exchanger be operated in parallel flow or in counterflow? What is the ratio of the required areas for these two flow conditions?

In open heart surgery under hypothermic conditions, the patient's blood is cooled before the surgery and rewarmed afterward. It is proposed that a concentric tube, counterflow heat exchanger of length \(0.5 \mathrm{~m}\) be used for this purpose, with the thin-walled inner tube having a diameter of \(55 \mathrm{~mm}\). The specific heat of the blood is \(3500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). (a) If water at \(T_{h j}=60^{\circ} \mathrm{C}\) and \(\dot{m}_{h}=0.10 \mathrm{~kg} / \mathrm{s}\) is used to heat blood entering the exchanger at \(T_{c A}=18^{\circ} \mathrm{C}\) and \(\dot{m}_{c}=0.05 \mathrm{~kg} / \mathrm{s}\), what is the temperature of the blood leaving the exchanger? The overall heat transfer coefficient is \(500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) The surgeon may wish to control the heat rate \(q\) and the outlet temperature \(T_{c, 0}\) of the blood by altering the flow rate and/or inlet temperature of the water during the rewarming process. To assist in the development of an appropriate controller for the prescribed values of \(\hat{m}_{c}\) and \(T_{c \jmath}\), compute and plot \(q\) and \(T_{c, \rho}\) as a function of \(\dot{m}_{h}\) for \(0.05 \leq \dot{m}_{\mathrm{h}} \leq 0.20 \mathrm{~kg} / \mathrm{s}\) and values of \(T_{h, l}=50,60\), and \(70^{\circ} \mathrm{C}\). Since the dominant influence on the overall heat transfer coefficient is associated with the blood flow conditions, the value of \(U\) may be assumed to remain at \(500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Should certain operating conditions be excluded?

Water is used for both fluids (unmixed) flowing through a single-pass, cross- flow heat exchanger. The hot water enters at \(90^{\circ} \mathrm{C}\) and \(10,000 \mathrm{~kg} / \mathrm{h}\), while the cold water enters at \(10^{\circ} \mathrm{C}\) and \(20,000 \mathrm{~kg} / \mathrm{h}\). If the effectiveness of the exchanger is \(60 \%\), determine the cold water exit temperature.

Untapped geothermal sites in the United States have the estimated potential to deliver \(100,000 \mathrm{MW}\) (electric) of new, clean energy. The key component in a geothermal power plant is a heat exchanger that transfers thermal energy from hot, geothermal brine to a second fluid that is evaporated in the heat exchanger. The cooled brinc is reinjected into the gcothermal well after it exits the heat exchange, while the vapor exiting the heat exchanger serves as the working fluid of a Rankine cycle. Consider a geothermal power plant designed to deliver \(P=25 \mathrm{MW}\) (electric) operating at a thermal efficiency of \(\eta=0.20\). Pressurized hot brine at \(T_{h i}=200^{\circ} \mathrm{C}\) is sent to the tube side of a shell-andtube heat exchanger, while the Rankine cycle's working fluid enters the shell side at \(T_{c, i}=45^{\circ} \mathrm{C}\). The brine is reinjected into the well at \(T_{h_{i o}}=80^{\circ} \mathrm{C}\). (a) Assuming the brine has the properties of water, determine the required brine flow rate, the required effectiveness of the heat exchanger, and the required heat transfer surface area. The overall heat transfer coefficient is \(U=4000 \mathrm{~W} / \mathrm{m}^{2}\). (b) Over time, the brine fouls the heat transfer surfaces, resulting in \(U=2000 \mathrm{~W} / \mathrm{m}^{2}\). For the operating conditions of part (a), determine the electric power generated by the geothermal plant under fouled heat exchanger conditions.

In a dairy operation, milk at a flow rate of \(250 \mathrm{~L} / \mathrm{h}\) and a cow-body temperature of \(38.6^{\circ} \mathrm{C}\) must be chilled to a safe-to-store temperature of \(13^{\circ} \mathrm{C}\) or less. Ground water at \(10^{\circ} \mathrm{C}\) is available at a flow rate of \(0.72 \mathrm{~m}^{3} / \mathrm{h}\). The density and specific heat of milk are \(1030 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3860 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. (a) Determine the UA product of a counterflow heat exchanger required for the chilling process. Determine the length of the exchanger if the inner pipe has a 50 -mm diameter and the overall heat transfer coefficient is \(U=1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) Determine the outlet temperature of the water. (c) Using the value of \(U A\) found in part (a), determine the milk outlet temperature if the water flow rate is doubled. What is the outlet temperature if the flow rate is halved?

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