Question 4.6: Analyzing a Pump System A pump steadily draws water from a p...

Analyzing a Pump System

A pump steadily draws water from a pond at a volumetric flow rate of 220 gal/min through a pipe having a 5 in. diameter inlet. The water is delivered through a hose terminated by a converging nozzle. The nozzle exit has a diameter of 1 in. and is located 35 ft above the pipe inlet. Water enters at 70°F, 14.7 lbf / in. ^{2} and exits with no significant change in temperature or pressure. The magnitude of the rate of heat transfer from the pump to the surroundings is 5% of the power input. The acceleration of gravity is 32.2 ft / s ^{2}.

Determine (a) the velocity of the water at the inlet and exit, each in ft/s, and (b) the power required by the pump, in hp.

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Known A pump system operates at steady state with known inlet and exit conditions. The rate of heat transfer from the pump is specified as a percentage of the power input.

Find Determine the velocities of the water at the inlet and exit of the pump system and the power required.

Schematic and Given Data:

Engineering Model

1. A control volume encloses the pump, inlet pipe, and delivery hose.

2. The control volume is at steady state.

3. The magnitude of the heat transfer from the control volume is 5% of the power input.

4. There is no significant change in temperature or pressure.

5. For liquid water, v \approx v_{f}(T) (Eq. 3.11) and Eq. 3.13 is used to evaluate specific enthalpy.

 

v(T, p) \approx v_{ f }(T) (3.11)

 

h(T, p) \approx h_{ f }(T)+\underline{v_{ f }(T)\left[p-p_{ sat }(T)\right]} (3.13)

 

6. g=32.2 ft / s ^{2}.

 

Analysis

a. A mass rate balance reduces at steady state to read \dot{m}_{2}=\dot{m}_{1}. The common mass flow rate at the inlet and exit, \dot{m}, can be evaluated using Eq. 4.4b together with v \approx v_{f}\left(70^{\circ} F \right)=0.01605 ft ^{3} / lb from Table A-2E. That is,

 

\dot{m}=\frac{ AV }{v} (one-dimensional flow) (4.4b)

 

\dot{m}=\frac{ AV }{v}=\left(\frac{220 gal / min }{0.01605 ft ^{3} / lb }\right)\left|\frac{1 min }{60 s } \right| \left|\frac{0.13368 ft ^{3}}{1 gal }\right|

 

= 30.54 lb/s

 

Thus, the inlet and exit velocities are, respectively,

 

1 V _{1}=\frac{\dot{m} v}{ A _{1}}=\frac{(30.54 lb / s )\left(0.01605 ft ^{3} / lb \right)}{\pi(5 in .)^{2} / 4}\left|\frac{144 in \cdot{ }^{2}}{1 ft ^{2}}\right|=3.59 ft / s

 

V _{2}=\frac{\dot{m} v}{ A _{2}}=\frac{(30.54 lb / s )\left(0.01605 ft ^{3} / lb \right)}{\pi(1 in .)^{2} / 4}\left|\frac{144 in .^{2}}{1 ft ^{2}}\right|=89.87 ft / s

 

b. To calculate the power input, begin with the one-inlet, oneexit form of the energy rate balance for a control volume at steady state, Eq. 4.20a. That is,

 

0=\dot{Q}_{ cv }-\dot{W}_{ cv }+\dot{m}\left[\left(h_{1}-h_{2}\right)+\frac{\left( V _{1}^{2}- V _{2}^{2}\right)}{2}+g\left(z_{1}-z_{2}\right)\right] (4.20a)

 

0=\dot{Q}_{ cv }-\dot{W}_{ cv }+\dot{m}\left[\left(h_{1}-h_{2}\right)+\frac{\left( V _{1}^{2}- V _{2}^{2}\right)}{2}+g\left(z_{1}-z_{2}\right)\right]

 

2 Introducing \dot{Q}_{ cv }=(0.05) \dot{W}_{ cv }, and solving for \dot{W}_{ cv }

 

\dot{W}_{ cv }=\frac{\dot{m}}{0.95}\left[\left(h_{1}-h_{2}\right)+\left(\frac{ V _{1}^{2}- V _{2}^{2}}{2}\right)+g\left(z_{1}-z_{2}\right)\right] (a)

 

Using Eq. 3.13, the enthalpy term is expressed as

 

h_{1}-h_{2}=\left[h_{ f }\left(T_{1}\right)+v_{ f }\left(T_{1}\right)\left[p_{1}-p_{ sat }\left(T_{1}\right)\right]\right]

 

-\left[h_{ f }\left(T_{2}\right)+v_{ f }\left(T_{2}\right)\left[p_{2}-p_{ sat }\left(T_{2}\right)\right]\right] (b)

 

Since there is no significant change in temperature, Eq. (b) reduces to

 

h_{1}-h_{2}=v_{ f }(T)\left(p_{1}-p_{2}\right)

 

As there is also no significant change in pressure, the enthalpy term drops out of the present analysis. Next, evaluating the kinetic energy term

 

\frac{ V _{1}^{2}- V _{2}^{2}}{2}=\frac{\left[(3.59)^{2}-(89.87)^{2}\right]\left(\frac{ ft }{ s }\right)^{2}}{2}\left|\frac{1 Btu }{778 ft \cdot lbf }\right|

 

\times\left|\frac{1 lbf }{32.174 lb \cdot ft / s ^{2}}\right|=-0.1614 Btu / lb

 

Finally, the potential energy term is

 

g\left(z_{1}-z_{2}\right)=\left(32.2 ft / s ^{2}\right)(0-35) ft \left|\frac{1 Btu }{778 ft \cdot lbf }\right|

 

\times\left|\frac{1 lbf }{32.174 lb \cdot ft / s ^{2}}\right|=-0.0450 Btu / lb

 

Inserting values into Eq. (a)

 

\dot{W}_{ cv }=\left(\frac{30.54 lb / s }{0.95}\right)[0-0.1614-0.0450]\left(\frac{ B tu }{ lb }\right)

 

= -6.64 Btu/s

 

Converting to horsepower

 

\dot{W}_{ cv }=\left(-6.64 \frac{ B tu }{ s }\right)\left|\frac{1 hp }{2545 \frac{ Btu }{ h }}\right|\left|\frac{3600 s }{1 h }\right|=-9.4 hp

 

where the minus sign indicates that power is provided to the pump.

 

1 Alternatively, V _{1} can be evaluated from the volumetric flow rate at 1. This is left as an exercise.

2 Since power is required to operate the pump, \dot{W}_{ cv } is negative in accord with our sign convention. The energy transfer by heat is from the control volume to the surroundings, and thus \dot{Q}_{ cv } is negative as well. Using the value of \dot{W}_{ cv } found in part (b), \dot{Q}_{ cv }=(0.05) \dot{W}_{ cv }=-0.332 Btu / s (-0.47 hp ).

Skills Developed

Ability to…

• apply the steady-state energy rate balance to a control volume.

• apply the mass flow rate expression, Eq. 4.4b.

• develop an engineering model.

• retrieve properties of liquid water.

Quick Quiz

If the nozzle were removed and water exited directly from the hose, whose diameter is 2 in., determine the velocity at the exit, in ft/s, and the power required, in hp, keeping all other data unchanged. Ans. 22.47 ft/s, −2.5 hp.

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