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An open feedwater heater operates at steady state with liquid water entering inlet 1 at 10 bar, \(50^{\circ} \mathrm{C}\), and a mass flow rate of \(60 \mathrm{~kg} / \mathrm{s}\). A separate stream of steam enters inlet 2 at 10 bar and \(200^{\circ} \mathrm{C}\). Saturated liquid at 10 bar exits the feedwater heater at exit 3 . Ignoring heat transfer with the surroundings and neglecting kinetic and potential energy effects, determine the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\), of the steam at inlet 2 .

Short Answer

Expert verified
The mass flow rate of the steam at inlet 2 is 15.9 kg/s.

Step by step solution

01

- Identify the known properties and assumptions

Note the given conditions: Inlet 1: liquid water at 10 bar, 50°C, and mass flow rate of 60 kg/s. Inlet 2: steam at 10 bar and 200°C. Exit 3: saturated liquid at 10 bar. Assume steady-state operation and neglect heat transfer with surroundings as well as kinetic and potential energy effects.
02

- Determine the enthalpies at each state

Use steam tables to find the specific enthalpy for each state. For inlet 1 (compressed liquid at 10 bar, 50°C), approximate it as a saturated liquid at 50°C: \[ h_1 = h_f(50^{\rm{\tiny C}}) \approx 209.3 \frac{\rm{kJ}}{\rm{kg}} \]. For inlet 2 (superheated steam at 10 bar and 200°C), find the specific enthalpy directly from the superheated steam table: \[ h_2 = 2847.5 \frac{\rm{kJ}}{\rm{kg}} \]. For exit 3 (saturated liquid at 10 bar), use the enthalpy of saturated liquid at 10 bar: \[ h_3 = h_f(10 \text{ bar}) = 762 \frac{\rm{kJ}}{\rm{kg}} \].
03

- Apply the conservation of mass

The mass flow rate of the combined streams leaving through exit 3 should equal the sum of the mass flow rates entering through inlets 1 and 2. Let \( \ dot{m}_2 \) be the mass flow rate of steam at inlet 2: \[ \ dot{m}_1 + \ dot{m}_2 = \ dot{m}_3 \]. Given: \( \ dot{m}_1 = 60 \frac{\rm{kg}}{\rm{s}} \). So, \[ 60 \frac{\rm{kg}}{\rm{s}} + \ dot{m}_2 = \ dot{m}_3 \].
04

- Apply the conservation of energy

For a control volume encompassing the feedwater heater at steady state, the energy entering equals the energy leaving: \[ \ dot{m}_1 h_1 + \ dot{m}_2 h_2 = \ dot{m}_3 h_3 \]. Now substitute known values into the equation: \[ 60 \frac{\rm{kg}}{\rm{s}} \times 209.3 \frac{\rm{kJ}}{\rm{kg}} + \ dot{m}_2 \times 2847.5 \frac{\rm{kJ}}{\rm{kg}} = (60 \frac{\rm{kg}}{\rm{s}} + \ dot{m}_2) \times 762 \frac{\rm{kJ}}{\rm{kg}} \].
05

- Solve for the mass flow rate of steam

Simplify the energy balance equation to solve for \( \ dot{m}_2 \): \[ 12558 \frac{\rm{kJ}}{\rm{s}} + 2847.5 \ dot{m}_2 \frac{\rm{kJ}}{\rm{kg}} = 60 \times 762 \frac{\rm{kJ}}{\rm{s}} + 762 \ dot{m}_2 \frac{\rm{kJ}}{\rm{kg}} \]. \[ 12558 + 2847.5 \ dot{m}_2 = 45720 + 762 \ dot{m}_2 \]. \[ 2085.5 \ dot{m}_2 = 33162 \]. Solving for \( \ dot{m}_2 \): \[ \ dot{m}_2 = 15.9 \frac{\rm{kg}}{\rm{s}} \].

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Key Concepts

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

Thermodynamic properties
In the context of an open feedwater heater, understanding thermodynamic properties is crucial as they define the state and behavior of fluids involved. These properties include pressure, temperature, and specific enthalpy among others.
In this problem, we know the following conditions:
  • Inlet 1: liquid water at 10 bar and 50°C
  • Inlet 2: steam at 10 bar and 200°C
  • Exit 3: saturated liquid at 10 bar
To find specific enthalpy values, steam tables are essential. For example, the specific enthalpy of liquid water at 50°C and 10 bar is approximated as a saturated liquid's specific enthalpy at 50°C:

\[ h_1 = h_f(50^{\circ}C) \approx 209.3 \frac{\text{kJ}}{\text{kg}} \]
Similarly, for superheated steam at 10 bar and 200°C, we use the superheated steam table:

\[ h_2 = 2847.5 \frac{\text{kJ}}{\text{kg}} \]
For the saturated liquid at 10 bar at Exit 3, the enthalpy of saturated liquid is used:

\[ h_3 = h_f(10 \text{bar}) = 762 \frac{\text{kJ}}{\text{kg}} \] Understanding and correctly approximating these properties is vital for accurate calculations.
Mass and energy balance
The principles of mass and energy balance are fundamental in analyzing open feedwater heaters. The mass balance states that the total mass entering the system equals the total mass leaving the system. This principle can be formulated as:

\[ \dot{m}_1 + \dot{m}_2 = \dot{m}_3 \]
Given the known mass flow rate of liquid water at Inlet 1 (60 kg/s), we can write:

\[ 60 \frac{\text{kg}}{\text{s}} + \dot{m}_2 = \dot{m}_3 \]
Energy balance, on the other hand, ensures the total energy entering the system equals the total energy leaving. For steady-state flow processes, this translates to:

\[ \dot{m}_1 h_1 + \dot{m}_2 h_2 = \dot{m}_3 h_3 \]
Substituting the given values and enthalpies, we modify this to:

\[ 60 \frac{\text{kg}}{\text{s}} \times 209.3 \frac{\text{kJ}}{\text{kg}} + \dot{m}_2 \times 2847.5 \frac{\text{kJ}}{\text{kg}} = (60 \frac{\text{kg}}{\text{s}} + \dot{m}_2) \times 762 \frac{\text{kJ}}{\text{kg}} \]
Ensuring these balances is crucial to finding unknowns like the mass flow rate of steam at Inlet 2.
Enthalpy calculation
Enthalpy represents the total heat content of a system and is crucial for energy balance equations in thermodynamics. Calculating specific enthalpy values for different states in an open feedwater heater requires accurate data from steam tables.
In this exercise, we calculate enthalpies at different points.
For Inlet 1, liquid water is approximated using the saturated liquid enthalpy at 50°C, yielding:

\[ h_1 = h_f(50^{\circ}C) \approx 209.3 \frac{\text{kJ}}{\text{kg}} \]
For Inlet 2, the enthalpy is found in superheated steam tables for steam at 200°C and 10 bar:

\[ h_2 = 2847.5 \frac{\text{kJ}}{\text{kg}} \]
Finally, for Exit 3, the enthalpy of saturated liquid at 10 bar is used:

\[ h_3 = h_f(10 \text{bar}) = 762 \frac{\text{kJ}}{\text{kg}} \]
These calculations are integral in solving for unknowns in mass and energy balance equations.
Steady-state flow process
A steady-state flow process assumes that the properties of the system do not change over time. This simplifies calculations, allowing us to use conservation laws effectively. Steady-state assumption implies:
  • The mass flow rate entering and exiting the system is constant.
  • The energy entering and leaving the system is balanced.
  • Properties like temperature, pressure, and enthalpy remain constant over time at any given point.

For the open feedwater heater in this exercise, steady-state assumptions make it possible to set up and solve mass and energy balance equations without considering transient changes.
This means:
  • The mass flow rate equation: \[ \dot{m}_1 + \dot{m}_2 = \dot{m}_3 \]
  • The energy balance equation: \[ \dot{m}_1 h_1 + \dot{m}_2 h_2 = \dot{m}_3 h_3 \]

By solving these equations under steady-state conditions, you find the unknown mass flow rate of steam at Inlet 2, ensuring the cumulative energy and mass in the system remain consistent.

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Most popular questions from this chapter

Nitrogen gas is contained in a rigid \(1-\mathrm{m}\) tank, initially at 10 bar, \(300 \mathrm{~K}\). Heat transfer to the contents of the tank occurs until the temperature has increased to \(400 \mathrm{~K}\). During the process, a pressure-relief valve allows nitrogen to escape, maintaining constant pressure in the tank. Neglecting kinetic and potential energy effects, and using the ideal gas model with constant specific heats evaluated at \(350 \mathrm{~K}\), determine the mass of nitrogen that escapes, in \(\mathrm{kg}\), and the amount of energy transfer by heat, in \(\mathrm{kJ}\).

Steam at a pressure of \(0.08\) bar and a quality of \(93.2 \%\) enters a shell- and-tube heat exchanger where it condenses on the outside of tubes through which cooling water flows, exiting as saturated liquid at \(0.08\) bar. The mass flow rate of the condensing steam is \(3.4 \times 10^{5} \mathrm{~kg} / \mathrm{h}\). Cooling water enters the tubes at \(15^{\circ} \mathrm{C}\) and exits at \(35^{\circ} \mathrm{C}\) with negligible change in pressure. Neglecting stray heat transfer and ignoring kinetic and potential energy effects, determine the mass flow rate of the cooling water, in \(\mathrm{kg} / \mathrm{h}\), for steady-state operation.

Carbon dioxide gas is compressed at steady state from a pressure of \(20 \mathrm{lbf} /\) in. \({ }^{2}\) and a temperature of \(32^{\circ} \mathrm{F}\) to a pressure of \(50 \mathrm{lbf} / \mathrm{in}^{2}\) and a temperature of \(120^{\circ} \mathrm{F}\). The gas enters the compressor with a velocity of \(30 \mathrm{ft} / \mathrm{s}\) and exits with a velocity of \(80 \mathrm{ft} / \mathrm{s}\). The mass flow rate is \(0.98 \mathrm{lb} / \mathrm{s}\). The magnitude of the heat transfer rate from the compressor to its surroundings is \(5 \%\) of the compressor power input. Using the ideal gas model with \(c_{p}=0.21 \mathrm{Btu} / \mathrm{bb} \cdot{ }^{\circ} \mathrm{R}\) and neglecting potential energy effects, determine the compressor power input, in horsepower.

A tank whose volume is \(0.01 \mathrm{~m}^{3}\) is initially evacuated. A pinhole develops in the wall, and air from the surroundings at \(21^{\circ} \mathrm{C}, 1\) bar enters until the pressure in the tank is 1 bar. If the final temperature of the air in the tank is \(21^{\circ} \mathrm{C}\), determine (a) the final mass in the tank, in \(g\), and (b) the heat transfer between the tank contents and the surroundings, in kJ.

A rigid tank whose volume is \(0.5 \mathrm{~m}^{3}\), initially containing ammonia at \(20^{\circ} \mathrm{C}, 1.5\) bar, is connected by a valve to a large supply line carrying ammonia at 12 bar, \(60^{\circ} \mathrm{C}\). The valve is opened only as long as required to fill the tank with additional ammonia, bringing the total mass of ammonia in the tank to \(143.36 \mathrm{~kg}\). Finally, the tank holds a two-phase liquid-vapor mixture at \(20^{\circ} \mathrm{C}\). Determine the heat transfer between the tank contents and the surroundings, in \(\mathrm{kJ}\), ignoring kinetic and potential energy effects.

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