A reciprocating pump has two double-acting cylinders each \(200 \mathrm{~mm}\) bore and \(450 \mathrm{~mm}\) stroke, the cranks being at \(90^{\circ}\) to each other and rotating at \(2.09 \mathrm{rad} \cdot \mathrm{s}^{-1}\) (20 rev/min). The delivery pipe is \(100 \mathrm{~mm}\) diameter, \(60 \mathrm{~m}\) long. There are no air vessels. Assuming simple harmonic motion for the pistons determine the maximum and mean water velocities in the delivery pipe and the inertia pressure in the delivery pipe near the cylinders at the instant of minimum water velocity in the pipe.

Short Answer

Expert verified
Mean Velocity: 7.52 m/s, Maximum Velocity: 11.81 m/s, Inertia Pressure: 118243 Pa

Step by step solution

01

- Calculate Pump Displacement Volume

The displacement volume of one double-acting cylinder per stroke is given by: \[ V = \frac{\text{Bore Area} \times \text{Stroke}}{2} \] Compute the bore area: \[ A = \frac{\frac{\text{bore}}{2}}^2 \times \text{π} = \frac{\frac{200 \text{ mm}}{2}}^2 \times π = 0.0314 \text{ m}^2 \] Now, compute the displacement volume: \[ V = \frac{0.0314 \text{ m}^2 \times 0.45 \text{ m}}{2} = 0.007065 \text{ m}^3 \]
02

- Compute Pump Flow Rate

The flow rate is computed as the total volume displaced by both cylinders over time. Since there are two double-acting cylinders, each stroke contributes: \[ \text{Flow Rate} = 2 \times 2 \times V \times \text{pump speed} \] Given the pump speed is 2.09 rad/s: \[ \text{Flow Rate} = 4 \times 0.007065 \text{ m}^3 \times 2.09 \text{ rad/s} = 0.0590 \text{ m}^3/s \]
03

- Calculate Mean Water Velocity in the Pipe

The mean water velocity is given by: \[ \text{Mean Velocity} = \frac{\text{Flow Rate}}{\text{Cross-sectional area of the pipe}} \] The cross-sectional area of the pipe is: \[ A_{\text{pipe}} = \frac{\frac{100 \text{ mm}}{2}}^2 \times \text{π} = 0.00785 \text{ m}^2 \] Now, compute mean velocity: \[ \text{Mean Velocity} = \frac{0.0590 \text{ m}^3/s}{0.00785 \text{ m}^2} = 7.52 \text{ m/s} \]
04

- Determine Maximum Water Velocity

Assuming simple harmonic motion for the pistons, the maximum velocity is: \[ \text{Maximum Velocity} = \text{Mean Velocity} \times \frac{π}{2} \] Substituting the mean velocity: \[ \text{Maximum Velocity} = 7.52 \text{ m/s} \times \frac{π}{2} = 11.81 \text{ m/s} \]
05

- Calculate Inertia Pressure

Inertia pressure is given by: \[ \text{Inertia Pressure} = \text{Density} \times \text{Length} \times \text{angular velocity}^2 \times \text{Stroke} / 2 \] Assuming water density as 1000 kg/m\textsuperscript{3}: \[ \text{Inertia Pressure} = 1000 \text{ kg/m}^3 \times 60 \text{ m} \times (2.09 \text{ rad/s})^2 \times (0.45 \text{ m}/2) \] Calculation results in: \[ \text{Inertia Pressure} = 118243 \text{ Pa} \]

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Key Concepts

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

Pump Displacement Volume
In a reciprocating pump, the displacement volume is crucial for understanding how much fluid is moved per stroke. The displacement volume depends on the bore (diameter) and stroke (distance traveled) of the cylinder. For a double-acting cylinder, each stroke fills and discharges fluid from both sides, so we consider half the stroke in the calculation. The formula used is:
\[ V = \frac{\text{Bore Area} \times \text{Stroke}}{2} \]
To find the bore area, use:
\[ A = \frac{\left( \frac{\text{bore}}{2} \right)^2 \times \pi}{2} \]
Then multiply by the stroke to find the displacement volume. In our example, with a bore of 200 mm and a stroke of 450 mm, the displacement volume per stroke becomes 0.007065 m³ for one cylinder.
Flow Rate Calculation
The flow rate of the pump is the volume of fluid displaced over a certain period. With two double-acting cylinders, each contributing volume from both ends, the total flow rate can be calculated using:
\[ \text{Flow Rate} = 2 \times 2 \times V \times \text{pump speed} \]
Here, V is the displacement volume, and the pump speed in rad/s converts the revolutions per minute into a useful factor. For the given example with a displacement volume of 0.007065 m³ and a pump speed of 2.09 rad/s, the flow rate comes out to be 0.0590 m³/s. This tells us how much water is pumped through the system every second.
Mean Water Velocity
The mean water velocity in the delivery pipe helps us understand how fast the water is moving on average. This is calculated by dividing the flow rate by the cross-sectional area of the delivery pipe:
\[ \text{Mean Velocity} = \frac{\text{Flow Rate}}{\text{Cross-Sectional Area of the Pipe}} \]
First, find the pipe's cross-sectional area with:
\[ A_{\text{pipe}} = \frac{\left( \frac{\text{diameter}}{2} \right)^2 \times \pi}{2} \]
With a pipe diameter of 100 mm, we get an area of 0.00785 m². Now, using the calculated flow rate of 0.0590 m³/s, the mean velocity is 7.52 m/s. This mean velocity is a key factor in designing efficient piping systems.
Maximum Water Velocity
In conditions of simple harmonic motion, the pistons create a situation where water velocity periodically reaches a maximum value. This peak water velocity, which we call maximum water velocity, can be calculated using the mean velocity multiplied by a factor of \( \frac{\pi}{2} \). Here's the formula:
\[ \text{Maximum Velocity} = \text{Mean Velocity} \times \frac{\pi}{2} \]
Plugging in the mean velocity of 7.52 m/s, we get:
\[ \text{Maximum Velocity} = 7.52 \, m/s \times \frac{\pi}{2} = 11.81 \, m/s \]
This value represents the highest speed that water can reach inside the delivery pipe, which is essential for pressure-related calculations and for avoiding surges.
Inertia Pressure
Inertia pressure in the delivery pipe arises due to the accelerating and decelerating water masses. This pressure depends on factors like water density, pipe length, angular speed, and stroke length. The formula to calculate inertia pressure is:
\[ \text{Inertia Pressure} = \text{Density} \times \text{Length} \times \text{Angular Velocity}^2 \times \frac{\text{Stroke}}{2} \]
For our example, with water density assumed to be 1000 kg/m³, pipe length of 60 m, angular velocity of 2.09 rad/s, and stroke of 450 mm, we get:
\[ \text{Inertia Pressure} = 1000 \, kg/m^3 \times 60 \, m \times (2.09 \, rad/s)^2 \times \frac{0.45 \, m}{2} = 118243 \, Pa \]
Understanding inertia pressure is important for designing robust pumping systems that can handle the additional stresses due to accelerating fluids.

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Most popular questions from this chapter

A single-acting reciprocating water pump, with a bore and stroke of \(150 \mathrm{~mm}\) and \(300 \mathrm{~mm}\) respectively, runs at \(2.51 \mathrm{rad} \cdot \mathrm{s}^{-1}(0.4 \mathrm{rev} / \mathrm{s}) .\) Suction and delivery pipes are each \(75 \mathrm{~mm}\) diameter. The former is \(7.5 \mathrm{~m}\) long and the suction lift is \(3 \mathrm{~m}\). There is no air vessel on the suction side. The delivery, pipe is \(300 \mathrm{~m}\) long, the outlet (at atmospheric pressure) being \(13.5 \mathrm{~m}\) above the level of the pump, and a large air vessel is connected to the delivery pipe at a point \(15 \mathrm{~m}\) from the pump. Calculate the absolute pressure head in the cylinder at beginning, middle and end of each stroke. Assume that the motion of the piston is simple harmonic, that losses at inlet and outlet of each pipe are negligible, that the slip is \(2 \%\), and that \(f\). for both pipes is constant at 0.01. (Atmospheric pressure \(10.33 \mathrm{~m}\) water head.)

In a vertical-shaft inward-flow reaction turbine the sum of the pressure and kinetic heads at entrance to the spiral casing is \(120 \mathrm{~m}\) and the vertical distance between this section and the tail-race level is \(3 \mathrm{~m}\). The peripheral velocity of the runner at entry is \(30 \mathrm{~m} \cdot \mathrm{s}^{-1}\), the radial velocity of the water is constant at \(9 \mathrm{~m} \cdot \mathrm{s}^{-1}\) and discharge from the runner is without whirl. The estimated hydraulic losses are: (1) between turbine entrance and exit from the guide vanes, \(4.8 \mathrm{~m}\) (2) in the runner, \(8.8 \mathrm{~m},(3)\) in the draft tube, \(790 \mathrm{~mm}\), (4) kinetic head rejected to the tail race, \(460 \mathrm{~mm}\). Calculate the guide vane angle and the runner blade angle at inlet and the pressure heads at entry to and exit from the runner

A centrifugal pump which runs at \(104.3 \mathrm{rad} \cdot \mathrm{s}^{-1}(16.6 \mathrm{rev} / \mathrm{s})\) is mounted so that its centre is \(2.4 \mathrm{~m}\) above the water level in the suction sump. It delivers water to a point \(19 \mathrm{~m}\) above its centre. For a flow rate of \(Q\left(\mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\right)\) the friction loss in the suction pipe is \(68 Q^{2} \mathrm{~m}\) and that in the delivery pipe is \(650 Q^{2} \mathrm{~m}\). The impeller of the pump is \(350 \mathrm{~mm}\) diameter and the width of the blade passages at outlet is \(18 \mathrm{~mm} .\) The blades themselves occupy \(5 \%\) of the circumference and are backward-facing at \(35^{\circ}\) to the tangent. At inlet the flow is radial and the radial component of velocity remains unchanged through the impeller. Assuming that \(50 \%\) of the velocity head of the water leaving the impeller is converted to pressure head in the volute, and that friction and other losses in the pump, the velocity heads in the suction and delivery pipes and whirl slip are all negligible, calculate the rate of flow and the manometric efficiency of the pump.

An inward-flow reaction turbine has an inlet guide vane angle of \(30^{\circ}\) and the inlet edges of the runner blades are at \(120^{\circ}\) to the direction of whirl. The breadth of the runner at inlet is a quarter of the diameter at inlet and there is no velocity of whirl at outlet. The overall head is \(15 \mathrm{~m}\) and the rotational speed \(104.7 \mathrm{rad} \cdot \mathrm{s}^{-1}\) (16.67 rev/s). The hydraulic and overall efficiencies may be assumed to be \(88 \%\) and \(85 \%\) respectively. Calculate the runner diameter at inlet and the power developed. (The thickness of the blades may be neglected.)

A quarter-scale turbine model is tested under a head of \(10.8 \mathrm{~m}\). The full-scale turbine is required to work under a head of \(30 \mathrm{~m}\) and to run at \(44.86 \mathrm{rad} \cdot \mathrm{s}^{-1}(7.14 \mathrm{rev} / \mathrm{s}) .\) At what speed must the model be run? If it develops \(100 \mathrm{~kW}\) and uses water at \(1.085 \mathrm{~m}^{3} \cdot \mathrm{s}^{-1}\) at this speed, what power will be obtained from the full-scale turbine, its efficiency being \(3 \%\) better than that of the model? What is the power specific speed of the full-scale, turbine?

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