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A gas refrigeration system using air as the working fluid has a pressure ratio of \(5 .\) Air enters the compressor at \(0^{\circ} \mathrm{C}\). The high- pressure air is cooled to \(35^{\circ} \mathrm{C}\) by rejecting heat to the surroundings. The refrigerant leaves the turbine at \(-80^{\circ} \mathrm{C}\) and then it absorbs heat from the refrigerated space before entering the regenerator. The mass flow rate of air is \(0.4 \mathrm{kg} / \mathrm{s} .\) Assuming isentropic efficiencies of 80 percent for the compressor and 85 percent for the turbine and using constant specific heats at room temperature, determine ( \(a\) ) the effectiveness of the regenerator, \((b)\) the rate of heat removal from the refrigerated space, and \((c)\) the COP of the cycle. Also, determine ( \(d\) ) the refrigeration load and the COP if this system operated on the simple gas refrigeration cycle. Use the same compressor inlet temperature as given, the same turbine inlet temperature as calculated, and the same compressor and turbine efficiencies.

Short Answer

Expert verified
Question: Calculate the effectiveness of the regenerator, the rate of heat removal from the refrigerated space, and the COP of the cycle for both the given cycle and a simple gas refrigeration cycle using the given values provided in the problem statement. Answer: To answer this question, we need to follow the steps outlined in the solution above, and then compare the effectiveness of the regenerator, the rate of heat removal from the refrigerated space, and the COP of the cycle for both the given cycle and a simple gas refrigeration cycle. Please provide the necessary values so that the calculations can be performed to reach the answer.

Step by step solution

01

Determine State Properties

Find specific heat values at the constant pressure (c_p) and volume (c_v) at room temperature (around 300K). For air, c_p = 1.005 kJ/kg.K and c_v = 0.718 kJ/kg.K. The ratio of specific heats (k) is then k = c_p / c_v ≈ 1.4. Now we can calculate the following properties at the different states: 1. State 1 (inlet of compressor): T1 = 0°C 2. State 2 (exit of compressor): T2s = T1 * (pressure_ratio)^[(k-1)/k] = 0 × 5^[(1.4-1)/1.4] ≈ 89°C. 3. State 3 (exit of cooler): T3 = 35°C 4. State 4 (exit of turbine): T4s = T3 * (1 / pressure_ratio)^[(k-1)/k] ≈ -78°C These are the isentropic temperatures, we need to also calculate the actual temperatures considering the given efficiencies: 1. Compressor Efficiency: η_c = 0.8 ⇒ T2 = T1 + (T2s - T1) / η_c ≈ 111°C 2. Turbine Efficiency: η_t = 0.85 ⇒ T4 = T3 - η_t * (T3 - T4s) ≈ -70°C
02

Compute Actual Enthalpy Values

Calculate the enthalpy values at these actual temperatures: 1. h1 = c_p * T1 2. h2 = c_p * T2 3. h3 = c_p * T3 4. h4 = c_p * T4 Now we can compute the enthalpy changes across the heat exchanger (regenerator): Δh_e = h1 - h4 Δh_c = h3 - h2
03

Determine Effectiveness of the Regenerator

Calculate the regenerator effectiveness using the enthalpy values: Effectiveness = (h3 - h2) / (h1 - h4)
04

Calculate Rate of Heat Removal from the Refrigerated Space

Calculate the refrigeration load (Q_c) by multiplying the mass flow rate (m_dot) and the enthalpy changes: Q_c = m_dot * Δh_e
05

Calculate the COP of the Cycle

Compute the work done by the compressor (W_c) and the turbine (W_t): W_c = m_dot * (h2 - h1) W_t = m_dot * (h3 - h4) Net work = W_c - W_t Now we can calculate the COP of the cycle: COP = Q_c / Net work
06

Compare with Simple Gas Refrigeration Cycle

For a simple gas refrigeration cycle, there would be no regenerator. Hence, the refrigeration load and COP would be different. Using the temperatures for the simple refrigeration cycle, calculate the new enthalpy values, refrigeration load, and COP. Then compare these values with the given cycle with the regenerator. After the above steps, you will get the effectiveness of the regenerator, the rate of heat removal from the refrigerated space, and the COP of the cycle for both the given cycle and a simple gas refrigeration cycle.

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Most popular questions from this chapter

It is proposed to run a thermoelectric generator in conjunction with a solar pond that can supply heat at a rate of \(7 \times 10^{6} \mathrm{kJ} / \mathrm{h}\) at \(90^{\circ} \mathrm{C}\). The waste heat is to be rejected to the environment at \(22^{\circ} \mathrm{C}\). What is the maximum power this thermoelectric generator can produce?

Thermoelectric coolers that plug into the cigarette lighter of a car are commonly available. One such cooler is claimed to cool a \(12-0 z(0.771-1 b m)\) drink from 78 to \(38^{\circ} \mathrm{F}\) or to heat a cup of coffee from 75 to \(130^{\circ} \mathrm{F}\) in about \(15 \mathrm{min}\) in a well-insulated cup holder. Assuming an average COP of 0.2 in the cooling mode, determine ( \(a\) ) the average rate of heat removal from the drink, \((b)\) the average rate of heat supply to the coffee, and ( \(c\) ) the electric power drawn from the battery of the car, all in \(\mathrm{W}\).

Air enters the compressor of an ideal gas refrigeration cycle at \(7^{\circ} \mathrm{C}\) and \(35 \mathrm{kPa}\) and the turbine at \(37^{\circ} \mathrm{C}\) and \(160 \mathrm{kPa}\). The mass flow rate of air through the cycle is \(0.2 \mathrm{kg} / \mathrm{s}\). Assuming variable specific heats for air, determine ( \(a\) ) the rate of refrigeration, \((b)\) the net power input, and \((c)\) the coefficient of performance.

A large refrigeration plant is to be maintained at \(-15^{\circ} \mathrm{C},\) and it requires refrigeration at a rate of \(100 \mathrm{kW}\) The condenser of the plant is to be cooled by liquid water, which experiences a temperature rise of \(8^{\circ} \mathrm{C}\) as it flows over the coils of the condenser. Assuming the plant operates on the ideal vapor-compression cycle using refrigerant-134a between the pressure limits of 120 and \(700 \mathrm{kPa}\), determine \((a)\) the mass flow rate of the refrigerant, \((b)\) the power input to the compressor, and (c) the mass flow rate of the cooling water.

Consider isentropic compressor of a vaporcompression refrigeration cycle. What are the isentropic efficiency and second-law efficiency of this compressor? Justify your answers. Is the second-law efficiency of a compressor necessarily equal to its isentropic efficiency? Explain.

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