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Refrigerant \(134 \mathrm{a}\) enters a compressor operating at steady state as saturated vapor at \(0.14 \mathrm{MPa}\) and exits at \(1.4 \mathrm{MPa}\) and \(80^{\circ} \mathrm{C}\) at a mass flow rate of \(0.106 \mathrm{~kg} / \mathrm{s}\). As the refrigerant passes through the compressor, heat transfer to the surroundings occurs at a rate of \(-0.40 \mathrm{~kJ} / \mathrm{s}\). Determine at steady state the power input to the compressor, in \(\mathrm{kW}\).

Short Answer

Expert verified
The power input to the compressor is 3.70 kW.

Step by step solution

01

State the Given Conditions

Identify and list the given conditions: 1. Inlet conditions: - Refrigerant 134a, saturated vapor - Pressure: 0.14 MPa 2. Outlet conditions: - Pressure: 1.4 MPa - Temperature: 80掳C 3. Mass flow rate: 0.106 kg/s 4. Heat transfer rate to surroundings: -0.40 kJ/s
02

Extract Enthalpy Values

Using refrigerant tables, find the specific enthalpy values for the given states: 1. At inlet (saturated vapor at 0.14 MPa): - Enthalpy \( (h_1) = 263.6 \ \text{kJ/kg} \) 2. At outlet (1.4 MPa and 80掳C): - Enthalpy \( (h_2) = 294.7 \ \text{kJ/kg} \)
03

Apply the Steady-State Energy Balance Equation

The energy balance for a control volume at steady state is given by: \[ \dot{Q} + \dot{m}h_{in} + \dot{W}_{in} = \dot{m}h_{out} \] Rearranging to solve for \( \dot{W}_{in} \): \[ \dot{W}_{in} = \dot{m} (h_2 - h_1) - \dot{Q} \]
04

Substitute Values and Calculate

Substitute the known values into the equation: \[ \dot{W}_{in} = 0.106 \ \text{kg/s} \, (294.7 \ \text{kJ/kg} - 263.6 \ \text{kJ/kg}) - (-0.40 \ \text{kJ/s}) \] Calculate the difference in enthalpies and solve: \[ \dot{W}_{in} = 0.106 \ \text{kg/s} \, (31.1 \ \text{kJ/kg}) + 0.40 \ \text{kJ/s} \] \[ \dot{W}_{in} = 3.2966 \ \text{kW} + 0.40 \ \text{kW} \] \[ \dot{W}_{in} = 3.6966 \ \text{kW} \]

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Key Concepts

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

Steady-state energy balance
In a refrigeration cycle, the steady-state energy balance plays a critical role in analyzing system performance. Imagine your compressor as a black box where mass and energy must balance out. In steady-state operations, the energy entering the system is equal to the energy leaving it, plus or minus any heat losses or additions. The key formula used is:
\[ \dot{Q} + \dot{m}h_{in} + \dot{W}_{in} = \dot{m}h_{out} \] Here:
- \( \dot{Q} \) represents the rate of heat transfer
- \( \dot{m} \) is the mass flow rate
- \( h_{in} \) and \( h_{out} \) are the specific enthalpies at the inlet and outlet
- \( \dot{W}_{in} \) stands for the power input
Rearranging for the power input: \[ \dot{W}_{in} = \dot{m}(h_{out} - h_{in}) - \dot{Q} \] When dealing with the compressor's power input, remember this balance ensures you correctly account for all energy changes. Missing out on even one component could lead to errors in calculation.
Refrigerant properties
Understanding the properties of refrigerants is fundamental for solving refrigeration cycle problems. Refrigerant 134a, often just termed as R-134a, is commonly used in automotive and residential air conditioning systems. Key properties include its pressure-temperature relationship, specific enthalpy, and vaporization points.
For this exercise:
- At the inlet, R-134a is a saturated vapor at 0.14 MPa
- At the outlet, the conditions are 1.4 MPa and 80掳C
Use refrigerant property tables or software to find specific values for properties like enthalpy (h) and entropy (s). These values are necessary for energy and mass balance calculations in the refrigeration cycle. Keeping a refrigerant property chart handy can save you a lot of time.
Enthalpy calculation
Enthalpy (h) is a measure of the total energy of a thermodynamic system. It includes internal energy plus the product of pressure and volume. Understanding and calculating enthalpy are crucial in thermodynamics, especially in refrigeration cycles. Here鈥檚 how to find and use enthalpy:
- Use refrigerant tables to extract specific enthalpy values at given pressures and temperatures.
For this exercise:
- At the inlet (saturated vapor at 0.14 MPa), the enthalpy is 263.6 kJ/kg (h1)
- At the outlet (1.4 MPa and 80掳C), the enthalpy is 294.7 kJ/kg (h2)
With these values, you can calculate the change in enthalpy (螖h):
\[ 螖h = h_{2} - h_{1} = 294.7 \text{kJ/kg} - 263.6 \text{kJ/kg} = 31.1 \text{kJ/kg} \] Using this change and the mass flow rate, we then use it in the steady-state energy balance equation to find the required power input for the compressor.
Compressor work
In a refrigeration cycle, the compressor is responsible for raising the pressure of the refrigerant, which in turn increases its temperature. This process requires work, often called compressor work.
The formula to calculate compressor work, using enthalpies, is:
\[ \dot{W}_{in} = \dot{m}(h_{2} - h_{1}) - \dot{Q} \] For our given problem:
- Mass flow rate (\( \dot{m} \)) is 0.106 kg/s
- Enthalpy change (h鈧 - h鈧) is 31.1 kJ/kg
- Heat transfer rate (\( \dot{Q} \)) is -0.40 kJ/s
Substituting these values into the formula:
\[ \dot{W}_{in} = 0.106 \text{kg/s} \times 31.1 \text{kJ/kg} + 0.40 \text{kJ/s} \] \[ \dot{W}_{in} = 3.2966 \text{kW} + 0.40 \text{kW} = 3.6966 \text{kW} \] Therefore, the compressor work required is approximately 3.70 kW. Remember, performing accurate enthalpy calculations leads to correct work evaluations, which are critical for system efficiency and component sizing.

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Most popular questions from this chapter

A water pump operating at steady state has \(76 \mathrm{~mm}\) diameter inlet and exit pipes, each at the same elevation. The water can be modeled as incompressible and its temperature remains constant at \(20^{\circ} \mathrm{C}\). For a power input of \(1.5 \mathrm{~kW}\), plot the pressure rise from inlet to exit, in \(\mathrm{kPa}\), versus the volumetric flow rate ranging from \(0.015\) to \(0.02 \mathrm{~m}^{3} / \mathrm{s}\).

Ammonia enters a control volume operating at steady state at \(p_{1}=14\) bar, \(T_{1}=28^{\circ} \mathrm{C}\), with a mass flow rate of \(0.5 \mathrm{~kg} / \mathrm{s}\). Saturated vapor at 4 bar leaves through one exit, with a volumetric flow rate of \(1.036 \mathrm{~m}^{3} / \mathrm{min}\), and saturated liquid at 4 bar leaves through a second exit. Determine (a) the minimum diameter of the inlet pipe, in \(\mathrm{cm}\), so the ammonia velocity does not exceed \(20 \mathrm{~m} / \mathrm{s}\). (b) the volumetric flow rate of the second exit stream, in \(\mathrm{m}^{3} / \mathrm{min} .\)

Air enters a compressor operating at steady state with a pressure of \(100 \mathrm{kPa}\), a temperature of \(27^{\circ} \mathrm{C}\), and a volumetric flow rate of \(0.57 \mathrm{~m}^{3} / \mathrm{s}\). Air exits the compressor at \(345 \mathrm{kPa}\). Heat transfer from the compressor to its surroundings occurs at a rate of \(48 \mathrm{~kJ} / \mathrm{kg}\) of air flowing. If the compressor power input is \(78 \mathrm{~kW}\), determine the exit temperature, in \({ }^{\circ} \mathrm{C}\).

Propane vapor enters a valve at \(1.6 \mathrm{MPa}, 70^{\circ} \mathrm{C}\), and leaves at \(0.5 \mathrm{MPa}\). If the propane undergoes a throttling process, what is the temperature of the propane leaving the valve, in \({ }^{\circ} \mathrm{C} ?\)

Liquid water at \(20^{\circ} \mathrm{C}\) enters a pump though an inlet pipe having a diameter of \(160 \mathrm{~mm}\). The pump operates at steady state and supplies water to two exit pipes having diameters of \(80 \mathrm{~mm}\) and \(120 \mathrm{~mm}\), respectively. The velocity of the water exiting the \(80 \mathrm{~mm}\) pipe is \(0.5 \mathrm{~m} / \mathrm{s}\). At the exit of the \(120 \mathrm{~mm}\) pipe the velocity is \(0.1 \mathrm{~m} / \mathrm{s}\). The temperature of the water in each exit pipe is \(22^{\circ} \mathrm{C}\). Determine (a) the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\), in the inlet pipe and each of the exit pipes, and (b) the volumetric flow rate at the inlet, in \(\mathrm{m}^{3} / \mathrm{s}\).

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