3) Sample Fan Selection
Let? look at a typical case
of fan selection for a new cooling tower design. The
following is a sample calculation for the thermal condition
of 113.0 - 89.6 - 80.6?, 63,843 gpm of water flow, and
induced draft counter flow type.
First and foremost, it is
to decide the size of tower cell, air inlet height and
depth of fill considering the heat load. The basic parameters
for the optimum thermal design are as follows; the simplest
way to design a new tower is to start with largest cell
size and largest fan.
- ● 42' x 42' with a 28' fan,
175 hp (Square cell is best but rectangular tower
with a ratio of length of width = 0.8 to 1.2, but
all tower components are based on a 6' x 6' base increment.)
- ● Air inlet on 2 sides only
& air inlet height 1/3 of cell width (In general,
1/4 to 1/3 to
the cell width)
- ● Height of plenum chamber
which is a distance between the top of eliminator
and the bottom of fan deck is generally obtained from
0.25 x { (Tower Width2 + Tower Length2)1/2}
- Fan Diameter } as minimum. Using a larger fan reduces
fan power and reduces minimum plenum chamber height,
but be careful: recirculation is likely to increase
if fan discharge velocity is too low. If the less
plenum is used to, the air velocity in the center
part of the eliminators can become so high that the
drift losses will occur. Same thing in the upper portions
of the fill. All these result in the increased pressure
drop, reduced airflow, and reduced performance.
- ● For the fill, use 4' (In
general, 2' to 5' for film type of fill or 10' - 15'
for splash fill)
- ● Water Loading: 2 to 14
US GPM/ft2 for counter flow, 4 to 24 US
GPM/ft2 for cross flow
- ● Air Velocity at each location:
The below is a guide line for the best performance
with the minimum fan power. Especially the air velocity
at the fill must be ranged in the below table. If
the air velocity is low in the fill, the air can not
be smoothly moved upward due to the restriction of
downward water and if the air velocity is too high
in the fill, the heat of water can not be completely
removed as desired.
The problem when the air speed at the air inlet exceeds
below ranges is resulting in poor air distribution
in the fill. For more details refer to the subjects
of Air Distribution and Exit Velocity in Chapter
9, energy saving.
Location |
Counter
Flow Type |
Cross
Flow Type |
Air
Inlet w/out Louver |
Nor.
1,000, max. 1,100 fpm |
N/A |
Air
Inlet w/Louver |
800
to 1,000 fpm |
300
to 650 fpm, max. 800 fpm |
Fill,
Eliminator |
300
to 650 fpm, max. 700 fpm |
300
to 650 fpm, max. 700 fpm |
Fan
Inlet |
1,600
to 2,000 fpm |
1,600
to 2,000 fpm |
Fan
Stack Exit |
1.4
time max. ambient wind speed, or min. 1,200 fpm
at 880 fpm (10 mph = 16.09 kph) of wind spd.)
|
1.4
time max. ambient wind speed, or min. 1,200 fpm
at 880 fpm (10 mph = 16.09 kph) of wind spd.)
|
(1) Thermal Design Result:
Considering the water and heat loading, 6 cells of 42'
width x 42' length of tower size and 14' (33% or more
to the width of tower cell) air inlet height is reasonable.
For velocity recovery, 7o of incline &
6.0' (21.4% to fan diameter) of venturi height was applied
to this sample job. 1.0% fill support obstruction, without
air inlet louver (10.0% air inlet obstruction), concrete
structures.
(2) Airflow & Pressure
Drop: The airflows and pressure drops at each location
and each cell were produced as follows. Airflow is varying
every location since the air volume is proportionally
increasing as much as the heat of water is transferring
into the air stream.
- ● Pressure Drop at Air Inlet
& Louver = K x (1/2) x (density x 0.1922) x (V2/115,820)
= 2.0 x (1/2) x (0.0717 x 0.1922) x (943.012/115,820)
= 0.1058 in H2O
- ● Pressure Drop at Fill:
This is given from the pressure drop curve of a specific
model of fill. The fill area is a net area deducting
the fill obstruction area from the total cross sectional
area of 42' x 42' tower. That is, 10,478.16 ft2
= 0.99 x 42' x 42 x 6 cells'. Note that heat transfer
in this fill obstruction is not occurring since the
water fraction and air stream can not be by-passed
through the parts of fills to be just laid onto the
fill supports. So, this
area called "Dead Zone
in Heat Transfer" must deducted as much as the
fill obstruction percentage.
- ● Pressure Drop at Eliminator
= K x (1/2) x (density x 0.1922) x (V2/115,820)
= 2.0 x (1/2) x (0.0688 x 0.1922) x (608.772/115,820)
= 0.0423 in H2O
- ● Pressure Drop at Fan Inlet
= K x (1/2) x (density x 0.1922) x (V2/115,820)
= 0.25 x (1/2) x (0.0688x 0.1922) x (1,853.712/115,820)
= 0.0491 in H2O
[Note that the net fan inlet area was obtained from
pie/4 (Fan Diameter2 - Seal Disc2).
That is, 573.52 ft2 = pie / 4 x (282
-7.33332).]
- ● Velocity Pressure at Fan
= (1/2) x (density x 0.1922) x (V2/115,820)
= (1/2) x (0.0688 x 0.1922) x (1,853.712/115,820)
= 0.1963 in H2O
or Press. Drop = (V/4,008.7)2 x 1/density
ratio
= (1,853.71/4,008.7)2 x 1/(0.0750/0.0688)
= 0.1963 in H2O
- ● Velocity Pressure at Stack
Exit = (1/2) x (density x 0.1922) x (V2/115,820)
= (1/2) x (0.0688 x 0.1922) x (1,661.072/115,820)
= 0.1576 in H2O
or Press. Drop = (V/4,008.7)2 x 1/density
ratio
= (1,661.07/4,008.7)2 x 1/(0.0750/0.0688)
= 0.1576 in H2O
[Note that the net fan stack exit area was calculated
as per the formula of pie / 4 x {fan diameter + (2
x tan 7?x venturi height)}2 - pie / 4 x
(seal disc diameter)2. That is, 640.03
= pie / 4{28 + (2 x 0.122785 x 6.0)}2 -
pie / 4 x 7.33332. The tip clearance was
neglected for the venturi.]
- ● Velocity Recovery (Pressure
Gain) = Efficiency of Fan Stack x VP at Fan x (1 -
(Fan Dia. / Stack Exit Dia)4)
= 0.7571 x 0.1963 x (1 - (28 - 29.47)4)
= 0.0276 in H2O
Since Hudson is considering 7?of stack incline and
is neglecting the no air flow zone at the top stack
due to the seal disc. (Unless the height of fan stack
is as mush as the fan diameter, the area of seal disc
in the fan must be subtracted from the fan stack top
area. Refer to Flow Pattern, Chapter
4), the net fan stack area must be corrected to
pie/4 x {fan diameter + (2 x tan 7o x venturi
height)}2. The area obtained from this
correction is 682.26 ft2 and consequently
the air velocity must be corrected to 1,558.24 fpm.
Then, velocity recovery is obtained from 0.7 x (0.1963
- 0.1386 ) = 0.0404 in H20.
Consequently, the fan brake horsepower based on above
calculation can differ from Hudson? fan rating, since
there is a little deviation in the velocity recovery.
BHP per Hudson? fan rating program in case of inputting
the 6.0' of venturi height and the 0.5100" Aq.
of static pressure (not considering the 0.0276"
of velocity recovery obtained from the thermal design
result.) is 136.7HP. This is less than BHP when inputting
0.4825 Aq. of static pressure and not inputting the
6.0' of venturi height by 3.1 HP. So, this is a reason
why we recommend the customers to use their own calculation
on the velocity recovery due to the fan stack.
- ● Total Static Pressure:
This is a value deducted by pressure gain, that is,
velocity recovery from a summation of pressure drops
at air inlet & louver, fill, eliminator and fan
inlet.
Total Static Pressure = (0.1058 + 0.3128 + 0.0423
+ 0.0491) - 0.0276
= 0.4825 in H2O
- ● Total Pressure: This is
a summation of Total Static Pressure and Velocity
Pressure.
Total Pressure = 0.4825 + 0.1963 = 0.6788 in H2O
(3) Fan Diameter: As previously
mentioned, the minimum fan coverage to the cross sectional
area of each cell must not be less than 30% for the
induced draft type of cooling tower or must not be less
than 30% of the area of fill.
- ● Fan coverage to 30% of
cross sectional area of 42' x 42' tower: 529.2 ft2.
This is equal to 25.96 ft.
- ● Fan coverage to 30% of
net area of fill: 523.91 ft2. This is equal
to 25.83 ft.
Judging from above fan coverage, 26' or 28' fan can
be used. Considering fan shaft power, fan cost, fan
stack cost, and allowable space in the fan deck, 28'
fan is more applicable. As see the above airflow and
pressure table, the air velocity at fan is less than
2,000 fpm. Accordingly, 28' of fan diameter is a best
choice.
(4) Fan Speed: This must
be fixed before deciding the number of fan blades, since
the fan speed is directly corresponding to the fan brake
horsepower and resonant frequency margin due to the
change in the fan speed. If possible, it would be fine
to select the fan speed considering the standard gear
reduction ratio of manufacturers. If non-standard gear
reduction ratio is used, the additional cost and delivery
is requiring as usual. Model AGC-1712-14 in Amarillo?
products is satisfying the mechanical power rating and
gear ratio. Fan Speed = (Motor Full Load Speed / Exact
Gear Reduction Ratio) = 1,770 / 14.000 = 126.4 rpm.
(5) Number of Fan Blades:
This depends on the limitation of vibration at the gear
reducer (i.e. material constructions), BHP/blade, fan
speed, and minimum resonant frequency, etc. For maintaining
the 80 micron of vibration at the position of gear reducer,
the minimum 6 each of fan blade is required. However,
this is exceeding the allowable BHP/blade (24 = max.
BHP/blade - 4 hp = 24 - 4) for 28' fan. So, 6 blades
of fan can not be used. Also, the pressure margin with
7 blades are too close to the critical operating line.
Finally, the number of blade satisfying the allowable
BHP/blade and the minimum 10% of pressure margin is
8 each.
(6) Automatic Selection:
To optimum design the fan diameter & number of blades
in accordance with the given airflow conditions, Hudson's
fan rating program gives all the available fan diameter
and number of blades based on the cost /hour. You can
select a model having most less cost/hour, but it depends
on the tower application designs. The operating cost/hour
calculation is based on several variables:
- ● Fan Price Modifier: 1.0
- ● Asset Years: based on
10 years
- ● Work Hours/Year: based
on 8,000
- ● Electric Power Cost: $0.46($/kw-hr)
But, you can calculate to
modify the cost/hour using the following equation:
(List Price x Price Modifier)
(Fan HP x 0.746 kw/hr) x (Cost/kw-hr)
---------------------------------------------------
+ ----------------------------------------------------------
(Asset Years x Workhours / Year)
Total Efficiency
Fan program is outputting
all the available solutions for fan diameter and number
of blade of fan on your given airflow conditions. For
previous example, the result of solutions without information
on the fan diameter and number of blades and under the
conditions of;
- ● Fan use: included draft
cooling tower
- ● Type of Blade: H Type
- ● Static pressure: 0.4825"
Aq.
- ● Airflow: 1,063,126acfm
- ● Exit Air Density: 0.0688
lb/ft3
- ● Resonance Frequency Margin:
5%
Hudson's fan rating program
outputs all the fan solutions for given airflow conditions.
These solutions are all of the fan sizes and number
of blades that meet the same airflow specifications,
and their operating cost/hour values. If you absolutely
do not want one of those fans, try with a different
tip speed. |