Energy and Power En gi neering, 2010, 2, 291-297
doi:10.4236/epe.2010.24041 Published Online November 2010 (http://www.SciRP.org/journal/epe)
Copyright © 2010 SciRes. EPE
The Experimental Investigation of Recirculation of
Air-Cooled System for a Large Power Plant
Wanli Zhao1, Qiyue Wang2, Peiqing Liu1
1Moe’s Key Lab. for Fluid Mechanics, Beijing University of Aeronautics
&
Astronauts,
Beijing, China
2Department of Myanmar Corperation, CPI Yunnan International Power Investment
Co. Ltd., Kunming, China
E-mail: bhvip@sohu.com, lpq@buaa.edu.cn, wangqiyue@cpiyn.com.cn
Received June 19, 2010; revised July 6, 2010; accepted August 16, 2010
Abstract
The paper introduces thermal buoyancy effects to experimental investigation of wind tunnel simulation on
direct air-cooled condenser for a large power plant. In order to get thermal flow field of air-cooled tower,
PIV experiments are carried out and recirculation ratio of each condition is calculated. Results show that the
thermal flow field of the cooling tower has great influence on the recirculation under the cooling tower.
Ameliorating the thermal flow field of the cooling tower can reduce the recirculation under the cooling tower
and improve the efficiency of air-cooled condenser also.
Keywords: Direct Air-Cooled Condenser, Thermal Flow Field, Recirculation, PIV Experiment, Power Plant
1. Introduction
Recently years many large direct air-cooled condenser
(ACC) has been constructed in power plants where cool-
ing water is unavailable or costly in nearby areas. Recir-
culation was usually formed under the cooling tower in
the effect of ambient wind. When recirculation occurred;
the efficiency of air-cooled condenser dropped dramati-
cally, which sometimes even made the system break off
[1-3].
Zhifu Gu [4,5] carried out the wind-tunnel simulation
on the direct-air-cooled system for one power plant in
China, using the traced gas, which is different from the
surrounding air in density, to simulate hot air flow ex-
hausted from ACC. Recirculation was weighed by meas-
uring the concentration of traced gas. Although use of the
traced gas could act as hot exhausted air from finned
tubes with the thermal buoyancy effect, the heat ex-
change between the hot finned tube and the cold air can-
not be simulated realistically; yet backpressure of the
steam turbine is extremely sensitive to ambient tempera-
ture. Therefore this model of the traced gas investigation
on the ACC may not be sufficiently accurate. C.A. Salta
and D.G Kroger [6] car ried out an experimen tal study on
a scale model of a forced draft air-cooled heat exchange
(ACHE). The results showed significant change in air
flow rate caused by varying the platform height. It was
found that lowering the platform height resulted in a de-
crease of air flow rate across the fans, and badly de-
creases in boundary fans of the platform Furthermore,
the influence of the width of a walkway along the boun-
dary of the platform on the air flow rate through an
ACHE was also considered. Tests shown that flow rate of
the ACHE can be improved by increasing the width of
walkway or extending the height of the platform. P. Van
Staden [7], Martin P. Van Staden and Pretorius [8] nu-
merically simulated the effect of ambient conditions
nearby the Matimba power station. The effect of the re-
circulation on the fan perfo rmance and the steam-turbine
backpressure based were predicted, and the effects of the
wind speed and the wind direction on the cooling effi-
ciency of the ACC were discussed. They found that the
cooling efficiency and the turbine backpressure were
very sensitive to the wind speed and wind direction. But
the mechanisms that caused hot recirculation and the
measures that minimized recirculation were not men-
tioned. C. Ziller, D. Schwarzkopf, and R. Balzereit [9],
studied the influence of wind speed and direction on the
efficiency of mechanically driven cooling devices, which
include multi-cell the cooling towers and air-cooled
condensers, by means of wind tunnel simulation. Their
results show that the negative influence affects the cool-
W. L. ZHAO ET AL.
Copyright © 2010 SciRes. EPE
292
ing devices. Besides, plant structures like gas turbines
which can suck hot exhaust air as fresh air can lead to a
dramatical decrease of its efficiency. Peiqing Liu, Hu-
ishen Duan, et al. [10] carried out the numerical simula-
tion of direct air-cooled system of Datong NO. 2 power
plant in China, and got the recirculation under the cool-
ing tower.
As we all know the thermal flow field around ACC
directly influences the hot air dispersing from ACC to the
cold air. It is very important to obtain thermal flow field
around ACC, especially in certain direction angles.
However, most current investigations have not concerned
on thermal flow field. Some researches on recirculation
were in cold condition, and engineering measures to re-
duce recirculation are very few. The present paper intro-
duces the buoyancy effects to experimental investigation
on direct air-cooled system for a power plant. PIV ex-
periment is conducted in wind tunnel to get thermal flow
field around ACC. At last, some measures are taken to
reduce the recirculation ratio.
2. Experimental System
2.1. Definition of Recirculation Ratio
In practice, recirculation is often formed under the action
of environment wind. In order to explain the recircula-
tion in quantification, Wanli Zhao [1,2] gave evaluation
criteria of recirculation ratio:
in a
ou a
TT
RTT
(1)
The average recirculation rate is
1
/
N
i
i
RRN
(2)
Where a
T indicates temperature of ambient air; in
T
indicates average temperature of air at the inlet of fans;
ou
T refers to average temperature of finned tubes. We
can calculate the recirculation ratio of each measuring
point by (1) through measuring the temperature at the
inlet of fans and outlet of finned tubes. We can also get
average recirculation rate by (2) under different condi-
tions.
2.2. The Model Apparatus
The experiment is carried out in FL-8 wind tunnel of
Chinese Aviation Industry and Aerodynamic Research
Institute. The wind tunnel is a circulative tunnel. The
section of test segment is flat eight-square and the area of
section is 7.685 square meter. The length of experimental
section is 5.5 meters, and maximum velocity is 70 m/s.
Scaling model is similar to Datong No.2 direct air-cooled
system [2] the model scaling ratio is 1:120.The bound ary
layer of atmosphere of B type is simulated in wind tunnel,
and section plane exponent of time-average velocity are
expressed by 0.16
. The turbulence rate close to the
ground is greater than 5%. The device of measuring
temperature is multi-channel temperature patrol system
produced by Keithley Co rporation of USA. The sensor is
thermocouple of T type. There are 92 measuring points
altogether placed at inlet of fans and outlet of finned
tubes. In model test, the two supplies produced by
LongWei electronic Ltd. Hong Kong provide direct cur-
rent and steady voltage to 112 model fans, and voltage
can change continuously.
2.3. PIV Equipment
In this experiment, double compositive Nd : YAG laser is
used as a lamp-house, single fluctuating energ y is 200mJ,
the lamp-house produces green light, and wave length is
532nm. CCD camera is PIVCAM 13-8, resolving power
of gray degree is 4096, re solving pow er of image is 1280
x 1024, and image gathering velocity is 8 frames per
second. Frame grabber reads number image of CCD
camera to memory, and INSIGHT software is used to
deal with, and TECPLOT is used to display.
2.4. Particle Casting Equipment
The choice of tracer particle is very important in PIV
experiment. On one hand, the particle must have a cer-
tain size to enhance the light scattering, and rein force the
contrast of image; on the other hand, the particle must be
little enough to assure good following, which can reflect
the real flow of flui d.
In this study, smog generation of XQ-1200 type was
used to produce tracer particle, and the particle genera-
tion can cast tracer particle continuously; at the same
time, the casting position of tracer particle can also ad-
just automatically.
2.5. Layout of PIV Experiment
Because of area of measuring spatial is too large (the
width of measuring region is about 1500 mm), so four
little areas were divided to measure respectively, and
then connect four images to form an integrated image.
Figure 1 displays the sketch map of measuring area and
camera layout.
2.6. Parameter Choice of Experiment
The choice of experiment parameter according to idio-
W. L. ZHAO ET AL.
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293
Figure 1. Sketch map of measuring area and came r a layo ut.
graphic instance experiences a process of gradual opti-
mization. The parameters mainly include: wind velocity,
measuring area, size of question area, interval time of
fluctuating timet, arithmetic choice et al.
1) Velocity: V = 6 m/s
2) Size of question area: the pixel is 32 × 32
3) Interval time of fluctuating time t: displacement
of particle in t should less than 1/4 of question area,
so interval time of fluctuating time can be calculated by:
1max
4/tx U()
In which,
x
is size of question area, max
U is
maximum velocity in question area. If 8 mmx ,
max 8 mmU then 200 μst .
4) Arithmetic choice: INSIGHT software provides two
arithmetic, there are, FFT arithmetic and Hart arithmetic,
in this study; FFT arithmetic is used.
3. Results and Discussion
In order to change the thermal flow field of the cooling
tower, three methods are used in the experiment: adding
the height of wind wall, adding the width of the platform,
and adding the length of the platform. Meanwhile the
recirculation under the cooling tower of three methods is
measured.
3.1. The Influence of Wind Velocity on
Recirculation Ratio
The magnitude of wind velocity has great influence on
recirculation ratio. Theoretically, in the absence of wind,
there is hardly recirculation existin g. When wind velocity
increases to a certain value, recirculation of different de-
gree may be occurred. Before blows, temperature of
measuring points are measured; it is found that tempera-
ture of measuring points clo sed to turbine house is high er
than other points. This is because steam ducts are made of
steel, and located between turbine house and cooling
tower. Heat discharged from steam ducts is absorbed by
fans closed to turbine house, which results in that tem-
perature of measuring points close to turbine house is
higher than others. When ambient wind blows from boiler
to cooling tower, the magnitude of wind velocity a
V in
wind tunnel is 6 m/s, 8 m/s, 10 m/s, 12 m/s, 14 m/s, av-
erage velocity between two steam ducts
j
V is 2.1 m/s,
so relationship between average recirculation ratio and
velocity ratio /
aj
K
VV
can be obtained.
It can be found that with K increasing, average re-
circulation ratio under cooling tower is increasing as well,
as shown in Figure 3. This is because flow separated at
the top of boiler house and boundary of wind wall far
from the turbine-house. At the back of boiler house and
backward position of wind wall, two eddy come into
being. At the boundary of vortex, strong turbulent en-
trainment mixes up, which causes more and more plumes
roll into the vortex. When K which leads to enhancing
of inertial force increases, that is, vortex strength is aug-
mented; more and more plumes are coiled to bottom
which causes recirculation increase.
Figure 2. Relationship between velocity ratio and average
recirculation ratio.
Figure 3. Relationship between wind direction angle and
average recirculation ratio.
W. L. ZHAO ET AL.
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294
3.2. Influence of Wind Direction Angle on
Recirculation Ratio
In order to reflect the influence of wind direction angles
on recirculation ratio, the model test selects 16 direction
angles (the interval is 22.5) and wind velocity is 6 m/s
and 8 m/s. Average recirculation ratio changed with wind
direction angles under different velocities is shown in
Figure 4. We can see that the worst wind direction angle
is about 0
, where the sub-high recirculation ratio is
near to 45
 . Under the velocity of 8 m/s, the trend
of average recirculation ratio changing with the direction
angle is similar to velocity of 6 m/s. But when wind di-
rection angle β = 67.5°~67.5°, β = 180° ~ 112.5°, β =
112.5° ~ 180°average recirculation ratio of 8 m/s is dis-
tinctly higher than 6 m/s.
3.3. Influence of Height of Wind Wall on
Recirculation Ratio
In order to decrease recirculation ratio under cooling
tower, wind velocity in wind tunnel is 6 m/s, wind direc-
tion angle 0
, the height of wind wall w
H
is
adopted by 13 m (design value), 14 m, 15 m, 16 m, 17 m,
and 18 m, the diameter of fan
N
D is 8.91 m. Tempera-
ture of each point is measured, and then, recirculation
ratio of each point is calculated and the influence of
height of wind wall on recirculation ratio is analyzed.
Figure 4 shows the relationship among height of wind
wall and average recirculation ratio under cooling tower
and density Froude num ber
D
r.
In where, 000
//
D
F
rV gLTT represents the ratio
of inertial force to buoyancy, T
the difference in tem-
perature, 0
V, 0
L, 0
T the reference velocity, length and
reference temperature [3].
From Figure 4 we can see that when the rotational
velocity of fans keeps constant, with height of wind wall
increasing
D
r based on height of wind wall decreases,
that is to say, the thermal buoyancy decreases. We can
also find that with the height of wind wall increasing, the
average recirculation ratio decreased at first, and then
increased. However, the values of average recirculation
ratio were all below that of design height of wind wall.
This is because the wind velocity in the tunnel is much
larger than the velocity of hot air discharged from steam
ducts, ambient wind suppresses the hot air, leading that
the hot air cannot dispel to backward position timely. At
the same time, buoyancy force and inertial force act on
hot air during its dispersal. When height of wind wall is
increasing, and wmw
H
H, buoyancy force can over-
come the inertial force from ambient wind, so recircula-
tion decreases gradually. When the height of wind wall
continues to increase, and wmw
H
H, buoyancy force
Figure 4. Relationship among height of wind wall and av-
erage recirculation ratio and FrD.
can not overcome the inertial force any longer, most of
the hot air was suppressed to inlet of fans through finned
tubes, which cause recirculation ratio increases. That is
to say, when /1.65
WN
HD
(corresponding height of
prototype is 14.64 m), average recirculation ratio is the
minimum, average recirculation ratio decreased 1.5%
compared with the design height of wind wall. Therefore,
increased height of wind wall is beneficial to decrease
average recirculation ratio under the cooling tower.
From the above results of the measuring recirculation,
adding the height of the wind wall can reduce the recir-
culation under the cooling tower. Figure 5 and Figure 6
gives the streamline picture of mid-section of unit under
different height of wind wall, when wind velocity is 6m/s,
and wind direction angle is 0
0
(west wind). So the
relationship between the thermal flow field of the cool-
ing tower and recirculation ratio under the cooling tower
is investigated.
From Figure 5 we can see when the ambient wind
blows from boiler to the cooling tower, because of air
separated from top of boiler and cooling platform, two
large captive eddies form on the lee side of the tower and
downstream position of platform. One vortex is formed
on the top of turbine house and the other vortex is
formed at backward position of wind wall away from
turbine house. On the boundary o f eddy, strong tur bulent
entrainment and mixing up which causes more and more
hot air discharged from ACC bring back into the bottom
of the cooling tower, under action of fans’ pumping, hot
air was sent to ACC again. From the Figure 5 we can see
a little bit “adverse flow” appears on the boundary of
wind wall closed to turbine house under the action of
eddy, because the height of wind wall is lower.
From the Figure 6 we can find in the case that height
of wind wall Hw = 150 mm, the large eddy at the lee back
of the boiler is uplifted, and has a trend of throwing away
W. L. ZHAO ET AL.
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295
Figure 5. The streamline of mid-section under the height of wind wall w
H= 108.3 mm, wind direction angle 0
0
.
Figure 6. The streamline of mid-section under the height of wind wall w
H= 150 mm, and wind direction angle 0
0
.
to the backward position. But only a little hot air dis-
charged from ACC closed to turbine house was brought
into eddy and then pumped by outer fans of platform.
The streamline on the top of platform was ascending, and
the eddy at backward position was raised. Eddy core
flowed away from wind wall, and threw away to the
backward position. From velocity profile of mid-section
of the unit in wind direction angle 0
, compared to
W. L. ZHAO ET AL.
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296
designed height of wind wall, when height of wind wall
increased, velocity profile above the platform became
slim, and magnitude of velocity closed to the platform
diminished. That is, the horizontal inertial force was re-
ducing, when buoyancy kept constant, which was helpful
for hot air to discharge. The results show good agree-
ment with recirculation results of experiment [3].
When wind velocity ratio increases, the average recir-
culation under the cooling tower increases as well. That
is because air separated at the top of boiler house and
boundary of wind wall far from the turbine house. At the
back of boiler house and backward position of wind wall,
two eddies came into being. At the boundary of vortex,
strong turbulent entrainment, and mixing up, which
caused more and more plumes roll into the vortex [11].
3.4. Add the Length or Width of the Platform
In the experiment, length and width of the platform are
all added, and the average recirculation ratio under the
cooling tower of the two situations is also measured.
Figure 7 gives the relationship between the average re-
circulation ratio and different schemes.
Where w
H
the height of wind wall,
N
D the diame-
ter of the fan, B is the adding width of the platform,
and L is the adding length of the platform. From Fig-
ure 7 we can find that adding the width of the platform
and adding the length of the platform can both reduce
average recirculation under the cooling tower [11].
Figure 8 gives the streamline picture of height of wind
wall is 108.3 mm, and width of front board is 50 mm. By
comparing Figure 5 and Figure 8, we can see that add-
ing the width of the platform, vortex configuration at the
back of boiler increased remarkable, and “adverse flow”
close to turbine house was weaken obviously. Because of
the supporting of the width board, the eddy configuration
downward position of the cooling tower is destroyed, so
when incoming flow conditions keep constant, turbulent
entrainment and mixing-up intensity of eddy downward
position weaken evidently. Then the hot air discharged
from ACC returned to the bottom of the cooling tower
becomes less. Besides, from the velocity figure we can
find that velocity figure above the platform becomes
Figure 7. The relationship between the average recircula-
tion and different schemes.
Figure 8. The streamline picture of height of wind wall is 108.3 mm, and width of front board is 50 mm.
W. L. ZHAO ET AL.
Copyright © 2010 SciRes. EPE
297
very slim and velocity closed to the bottom of platform
becomes less because of front-board supporting function,
which could help the hot air to discharge [3].
Therefore, adding the length or width of the platform
can both change the thermal flow flied configuration
around the cooling tower, and the recirculation under the
cooling tower is decreased.
4. Conclusions
The principal conclusions derived from investigations in
present paper can be summarized as follows:
The thermal flow field has great influence on the
average recirculation under the cooling tower,
recirculation under the cooling tower increases as
wind velocity ratio increases.
Increasing height of wind wall can ameliorate the
thermal flow field of the cooling tower, which
can help decrease the average recirculation ratio
under the cooling tower.
Adding the length or width of the platform can
also improve the therm al flow field of the cooling
tower; the average recirculation under the cooling
tower can be reduced by this way.
5. Acknowledgements
The authors are very grateful to the other members of our
groups for their experimental and numerical perform-
ances throughout this work. Special thanks should be
given to Jiali Jiang and Xiaoli Zhang of Chinese Aviation
Industry and Air Dynamic Research Institute for their
help in the PIV experiments.
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