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LIQUID-LIQUID HEAT TRANSFER IN A SPRAY COLUMN THESIS Submitted
by SUDHANYA KARMAKAR Class Roll No- 001310302001 Exam Roll
No-M4CHE15-01 Registration No-124698 of 2013- 2014 Under the
Guidance of Prof. (Dr.) Avijit Bhowal in partial fulfillment for
the award of the degree of MASTER OF ENGINEERING IN CHEMICAL
ENGINEERING DEPARTMENT OF CHEMICAL ENGINEERING JADAVPUR UNIVERSITY
Jadavpur, Kolkata-700032 MAY 2015
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Declaration of Originality and Compliance of Academic Ethics
I hereby declare that this thesis contains literature survey and
original research work by
the undersigned candidate, as part of his Master of Engineering
in Chemical
Engineering studies.
All information in this document have been obtained and
presented in accordance with
academic rules and ethical conduct.
I also declare that, as required by these rules and conduct, I
have fully cited and
referenced all material and results that are not original to
this work.
Name: Sudhanya Karmakar
Class Roll No-001310302001
Exam Roll No- M4CHE15-01
Registration No- 124698 of 2013- 2014
Thesis Title : LIQUID LIQUID HEAT TRANSFER IN A SPRAY COLUMN
Date: Sudhanya Karmakar
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FACULTY OF ENGINEERING AND TECHNOLOGY
DEPARTMENT OF CHEMICAL ENGINEERING
JADAVPUR UNIVERSITY
CERTIFICATE OF RECOMMENDATION
This is to certify that Ms. Sudhanya Karmakar, final year
student of Master of
Engineering in Chemical Engineering, Jadavpur University, has
completed the Project
work titled Liquid Liquid Heat Transfer in a Spray Column under
the guidance of
Prof. Dr. Avijit Bhowal during his Masters Curriculum. This work
has not been reported
earlier anywhere and can be approved for submission in partial
fulfillment of the course
work.
--------------------------------------------
Dr . Avijit Bhowal
Project Supervisor
Professor
Department of Chemical Engineering
Jadavpur University , Kolkata 32
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Approval
The following thesis is hereby approved as a credible study of a
Engineering subject and
presented in a manner satisfactory to warrant its acceptance as
a perquisite to the degree
for which it has been submitted. It is to be understood that by
this approval, the
undersigned do not necessarily endorse or approve any statement
made, opinion
expressed or conclusion drawn there in, but approve the thesis
only for thr purpose for
which it has been submitted.
Department of Chemical Engineering
Jadavpur University
--------------------------------------------------
HOD (Department of Chemical Engineering)
---------------------------------------------------
Dean (FET)
Committee of final examination for evaluation of thesis
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ACKNOWLEDGEMENT
Though the following project is an individual work, I could
never have reached the
heights or explored the depths without the help, support,
guidance and efforts of a lot of
people. Firstly, I would like to thank my Project Guide, Prof.
Dr. Avijit Bhowal
(Chemical Engineering) for instilling in me the qualities of
being a good researcher. His
infectious enthusiasm and unlimited zeal have been major driving
forces through my post
graduate career at the Jadavpur University, Kolkata. I would
also like to thank my
laboratory co-researcher Aritra Das for her support during the
project work. I would like
to take this opportunity to thank Mr. Jayant Modak , for his
constant encouragement and
helpful advice. I also extend my gratitude to Ms. Chandana Das
for her support. My very
special thanks to my parents whom I owe everything I am today,
my father Mr. Subodh
Karmakar and my mother Mrs. Tapashi Karmakar. Their unwavering
faith and
confidence in my abilities and in me is what has shaped me to be
the person I am today.
Thank you for everything. Finally, I would like to take the
opportunity to thank all my
teachers and support staff of the Chemical Engineering
Department, Jadavpur University,
Kolkata.
Sudhanya Karmakar
22st May, 2013
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Contents Chapter No Topics/Subtopics Page No 1. Introduction
1-26 1.1 Cooling Tower 3 1.2 Evaporator 4 1.3 Heat Exchanger 4-23
1.3.1 Classification according to 9-17 contact type 1.3.2
Classification according to 18-19 flow type 1.3.3 Classification
according to 19-23 construction type 1.3.4 Classification according
to 23 number of fluids 1.3.5 Classification according to 23 surface
compactness 1.4 Spray Column 24-26 2. Literature Review 27-36 3.
Aim & Objective 37-39 4. Experimental Section 40-44 4.1
Experimental Setup 41-42
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4.2 Experimental Procedure 42-43 5. Results & Discussion
45-65 5.1 Study of heat loss in counter-flow 46-48 Spray-Column 5.2
Calculation of thermal efficiency 49 5.3 Calculation of heat
transfer coeff 49 -icient 5.4 Effect of water flow rate on h &
50-55 5.5 Effect of variation in water inlet 56-58 temperature on h
& 5.5 Effect of variation in column height 59-61 on h & 5.5
Effect of variation in phase ratio on 62-65 6. Conclusion 66-67
NOMENCLATURE 68 REFFERENCES 69-70
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List of Figures Fig No. Figure Name Page No. Fig 1.1
Classification of heat exchangers 8 Fig 1.2 Shell and tube heat
exchanger 9
Fig 1.3 Plate and Frame heat exchanger 10
Fig 1.4 Turbulent pipe contact 13
Fig 1.5 Typical mechanically agitated towers 14
Fig 1.6 Baffle tray column 15
Fig 1.7 A possible configuration of a packed bed condenser
15
Fig 1.8 Schematics of a Spray Column 16
Fig 1.9 Schematic of a sieve tray column 17
Fig 1.10 Schematic of a Parallel flow & a Counter Flow Heat
Exchanger 18
Fig 1.11 Schematic of a Cross Flow Heat Exchanger 19
Fig1.12 Tubular Heat Exchanger 19
Fig1.13 Plate-Type Heat Exchanger 20
Fig1.14 Extended Surface Heat Exchanger 21
Fig1.15 Regenerator 22
Fig1.16 Typical countercurrent-flow spray tower 26
Fig 1.17 Crosscurrent-flow spray tower 26
Fig 4.1 Overall Experimental Set Up 43
Fig 4.2 Schematic of experimental set up 44
Fig 5.1 Effect of water flow rate on thermal efficiency at water
51
bath temperature550C & Column Height 105cm
Fig 5.2 Effect of water flow rate on thermal efficiency 51
at water bath temperature 640C & Column Height 105cm
Fig 5.3 Effect of water flow rate on thermal efficiency 52
at water bath temperature550C & Column Height 80cm
Fig 5.4 Effect of water flow rate on thermal efficiency 52
at water bath temperature640C & Column Height 80cm
Fig 5.5 Effect of water flow rate on heat transfer coefficient
54
at water bath temperature 550C & column height 105cm
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Fig No. Figure Name Page No.
Fig 5.6 Effect of water flow rate on heat transfer coefficient
54
at water bath temperature 640C & column height 105cm
Fig 5.7 Effect of water flow rate on heat transfer coefficient
55
at water bath temperature 550C & column height 80cm
Fig 5.8 Effect of water flow rate on heat transfer coefficient
55
at water bath temperature 640C & column height 80cm
Fig 5.9 Effect on thermal efficiency with change in water 57
bath temperature at a height 105cm
Fig 5.10 Effect on thermal efficiency with change in water
57
bath temperature at a height 80cm
Fig 5.11 Effect on heat transfer coefficient with change in
water 58
bath temperature at a height 105cm
Fig 5.12 Effect on heat transfer coefficient with change in
water 58
bath temperature at a height 80cm
Fig 5.13 Effect on thermal efficiency with change in column
height 60
at a water bath temperature 550C
Fig 5.14 Effect on thermal efficiency with change in column
height 60
at a water bath temperature 640C
Fig 5.15 Effect on overall heat transfer coefficient with change
in 61
height at a water bath temperature 550C
Fig 5.16 Effect on overall heat transfer coefficient with change
in 61
height at a water bath temperature 640C
Fig 5.17 Effect on Thermal Efficiency with change in phase ratio
at 63
a Column Height 105cm
Fig 5.18 Effect on Thermal Efficiency with change in phase ratio
at 63
a Column Height 80cm
Fig 5.19 Effect on overall heat transfer coefficient with change
in 64
phase ratio at a Column Height 105cm
Fig 5.20 Effect on overall heat transfer coefficient with change
in 64
phase ratio at a Column Height 105cm
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Fig 5.21 Effect on Kerosene Outlet temperature with change in
65
phase ratio at a Column Height 105cm
Fig 5.22 Effect on Kerosene Outlet temperature with change in
65
phase ratio at a Column Height 80cm
List of Tables Table No. Table Name Page No
Table1 Heat loss at Water Bath Temperature-55 0C & 46
Column Height- 105 cm
Table2 Heat Loss at Water Bath Temperature- 64 0C & 47
Column Height- 105 cm
Table3 Heat Loss at Water Bath Temperature- 55 0C & 47
Column Height- 80 cm
Table4 Heat loss at Water Bath Temperature- 64 0C & 48
Column Height- 80 cm
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1
Chapter 1 IntroductIon
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Most of the industries use water for their production and this
water often requires
particular properties such as solubility, transportability and
heat exchanging potential.
Water in industry is used for boiler make up, processing,
product treatment and cleaning,
cooling etc. The quantity of water consumption differs between
types of industries. The steel,
chemical, oil, petrochemical, pulp and paper industries are
major users of large quantities
of water per unit price of products because they use fresh water
for cooling, cleaning and
product processing. Cooling water comprise the majority of
consumption of industrial
water. Due to huge water consumption in each plant, cooling
water is generally reused in
order to save the acquisition cost & the water resource.
So, a huge amount of water is necessary to re-circulate in many
industries such as:
thermal power plant, oil industries, petrochemical industries
etc. In thermal power plant,
large amount of superheated steam is produced by using soft
water. This steam is used to
rotate the impeller of the turbine so that it can generate
power. This used steam is
condensed by passing it through a condenser. For this purpose, a
water stream is passed
through the condenser coil to transfer the heat energy from
steam to water. Therefore, the
water temperature rises. The temperature of the water must be
reduced to make the water
fit for recycling.
In oil and petroleum industries, steam is used to raise the
temperature of oil and
petroleum product to maintain the flowability. For this reason a
huge steam is used in
steam jacket in storage tanks, process lines, columns, reboilers
etc. in all over the process.
That steam passed through the condenser where water
recirculation is necessary. Besides
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condenser there are many heat exchanger equipments in those
industries where water is
used as coolant. There also water recycling process is
essential. Again, it should also be
noted that for the environmental friendly discharging of the
waste water in some
industries the temperature of the water should be brought down
or else it may have
several effects on the aquatic or marine life by causing
abnormal increase in the
temperature of the water body. The sharp increase in water
temperature inhibits the
growth of microorganisms which are very essential for the
maintenance of aquatic
symbiosis. So cooling of process hot water stream is an
important operation in process
industries. There are various equipment used for cooling hot
water such as heat
exchanger, cooling towers, evaporators etc. The different
equipment used for cooling
water is:
1.1 Cooling Tower
When warm liquid is brought into contact with unsaturated gas,
part of the liquid
evaporates and the liquid temperature drops. The most important
application of this
principle is in the use of cooling towers to lower the
temperature of recirculated water
used for condensers and heat exchangers in chemical plants,
power plants. Cooling
towers are large-diameter columns with special type of packing
designed to give good
gas-liquid contact with low pressure drop. Warm water is
distributed over the packing by
spray nozzles or a grid of notched troughs or pipes. Air is
passed through the packing by
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forced-draft or induced-draft fan or in some designs it is drawn
through by natural
convection.
1.2 Evaporator
An evaporator is a device used to turn the liquid form of a
chemical into its
gaseous form. The liquid is evaporated, or vaporized, into a
gas. It is used in air
conditioning system to evaporate gas from liquid while absorbing
heat in the process. It
can also be used to remove water or other liquids from mixtures.
In the concentration
process, the main objective of evaporation is to vaporize most
of the water from a
solution which contains the desired product. The general types
of evaporator used in
todays world are open kettle or pan evaporator, agitated film
evaporator, pan solar
evaporator, natural circulation type and forced circulation
type. Natural circulation type
evaporators are classified into horizontal tube evaporator,
vertical short tube or calandria
evaporator, long tube vertical rising film type, long tube
vertical falling film type. Open
kettle or pan evaporators are the simplest evaporator consists
of an open kettle in which
the liquid is boiled. The heat supplied by condensation of steam
in a jacket in the liquid.
these are inexpensive and simple to operate but the steam
economy is very poor.
1.3 Heat Exchanger
A heat exchanger is a device that is used to transfer thermal
energy (enthalpy)
between two or more fluids, between a solid surface and a fluid,
or between solid
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particulates and a fluid, at different temperatures and in
thermal contact. In heat
exchangers, there are usually no external heat and work
interactions.
Heat exchangers are commonly used in practice in a wide range of
applications,
from heating and air-conditioning systems in a household, to
chemical processing and
power production in large plants. Heat exchangers differ from
mixing chambers in that
they do not allow the two fluids involved to mix. In a car
radiator, for example, heat is
transferred from the hot water flowing through the radiator
tubes to the air flowing
through the closely spaced thin plates outside attached to the
tubes.
Heat transfer in a heat exchanger usually involves convection in
each fluid and
conduction through the wall separating the two fluids. In the
analysis of heat exchangers,
it is convenient to work with an overall heat transfer
coefficient U that accounts for the
contribution of all these effects on heat transfer. The rate of
heat transfer between the two
fluids at a location in a heat exchanger depends on the
magnitude of the temperature
difference at that location, which varies along the heat
exchanger. In the analysis of heat
exchangers, it is usually convenient to work with the
logarithmic mean temperature
difference LMTD, which is an equivalent mean temperature
difference between the two
fluids for the entire heat exchanger.
In a few heat exchangers, the fluids exchanging heat are in
direct contact. In most
heat exchangers, heat transfer between fluids takes place
through a separating wall or into
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and out of a wall in a transient manner. In many heat
exchangers, the fluids are not
separated by a heat transfer surface, and ideally they do not
mix or leak. Such exchangers
are referred to as direct transfer type, or simply recuperators.
In contrast, exchangers in
which there is intermittent heat exchange between the hot and
cold fluidsvia thermal
energy storage and release through the exchanger surface or
matrix are referred to as
indirect transfer type, or simply regenerators. Such exchangers
usually have fluid leakage
from one fluid stream to the other, due to pressure differences
and matrix rotation/valve
switching. Common examples of heat exchangers are shell-and tube
exchangers,
automobile radiators, condensers, air preheaters. If no phase
change occurs in any of the
fluids in the exchanger, it is sometimes referred to as a
sensible heat exchanger. There
could be internal thermal energy sources in the exchangers, such
as in electric heaters and
nuclear fuel elements. Combustion and chemical reaction may take
place within the
exchanger, such as in boilers, fired heaters, and fluidized-bed
exchangers. Mechanical
devices may be used in some exchangers such as in scraped
surface exchangers, agitated
vessels, and stirred tank reactors. Heat transfer in the
separating wall of a recuperator
generally takes place by conduction. However, in a heat pipe
heat exchanger, the heat
pipe not only acts as a separating wall, but also facilitates
the transfer of heat by
condensation, evaporation, and conduction of the working fluid
inside the heat pipe. In
general, if the fluids are immiscible, the separating wall may
be eliminated, and the
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interface between the fluids replaces a heat transfer surface,
as in a direct-contact heat
exchanger. There are different types of heat exchangers as
follows.
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8
Fig 1.1: Classification of Heat Exchangers
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1.3.1 Classification according to contact type:
1.3.1(a) Indirect contact heat exchanger involves heat transfer
between hot and cold
streams of two phases in the presence of a separating solid
wall.
Shell and tube heat exchangers:
As shown in fig.1.2 shell and tube heat exchanger has two sides.
One is tube side
and another is shell side. Tube side has series of tubes called
tube bundle. Tube bundle
can be made of different types of tubes: plain, longitudinally
finned, etc .The fluid
contains tube side can be heated or cooled by transferring heat
with shell side fluid. The
shell and tube heat exchanger can be used at temperature
>2500 C and pressure at>30 bar.
Fig.1.2: Shell and tube heat exchanger.
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Plate and Frame heat exchanger:
For many applications at moderate temperature and pressure, an
alternative to the
shell and tube exchanger is the gasketed plate exchanger
(fig.1.3), which consists of
many corrugated stainless-steel sheets separated by polymer
gaskets and clamped in a
steel frame. Inlet portals and slots in the gaskets direct the
hot and cold fluid to alternate
spaces between the plates. The corrugation induces turbulence
for improved heat transfer
and each plate is supported by multiple contacts with adjoining
plates, which have a
different pattern or angle of corrugation. The space between
plates is equal to the depth of
the corrugations and is usually 2 to 5 mm.
Fig.1.3: Plate and Frame heat exchanger
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1.3.1(b) Direct Contact Heat Exchanger
In a direct-contact exchanger, two fluid streams come into
direct contact,
exchange heat, and are then separated. Common applications of a
direct-contact
exchanger involve mass transfer in addition to heat transfer,
such as in evaporative
cooling and rectification; applications involving only sensible
heat transfer are rare. The
enthalpy of phase change in such an exchanger generally
represents a significant portion
of the total energy transfer. The phase change generally
enhances the heat transfer rate.
Advantages and Disadvantages in Utilizing Direct Contactors
The exchange of heat between two fluid streams can, in general,
be accomplished
using either direct contact or surface-type heat exchangers.
There are, however, several
limitations to the use of direct contactors. First, if two fluid
streams are placed in direct
contact, they will mix, unless the streams are immiscible. Thus,
stream contamination
will occur depending on the degree of miscibility. The two
streams must also be at the
same pressure in a direct contactor, which could lead to
additional costs. The advantages
in utilizing a direct contactor include the lack of surfaces to
corrode or foul, or otherwise
degrade the heat transfer performance. Other advantages include
the potentially superior
heat transfer for a given volume of heat exchanger due to the
larger heat transfer surface
area achievable and the ability to transfer heat at much lower
temperature differences
between the two streams. Still another advantage is the much
lower pressure drop
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associated with direct contactors as compared to their tubular
counterparts. A final
advantage is the much lower capital cost as direct contact heat
exchangers can be
constructed out of little more than a pressure vessel, inlet
nozzles for the fluid streams,
and exit ports. Of course, it is sometimes advantageous to
provide internals,
Varieties of Direct Contact Heat Exchangers
A typical direct contactor provides heat transfer between two
fluid streams. The
processes include the simple heating or cooling of one fluid by
the other; cooling with the
vaporization of the coolant; cooling of a gas-vapor mixture with
partial condensation;
cooling of a vapor or vapor mixture with total condensation; and
cooling of a liquid with
partial or complete solidification. Most of the direct-contact
applications can be
accomplished with the following devices: a) Spray columns, b)
Baffle tray columns, c)
Sieve tray or bubble tray columns, d) Packed columns, e)
Pipeline contactors, and f)
Mechanically agitated contactors. There are also some other
direct contactors like
evaporator, cooling tower , bubble column reactor.
Fig1.4 to 1.9 - illustrate the general configurations of a)
through f), respectively.
Except for the turbulent pipe contactor, all of the devices are
countercurrent devices and
depend upon the relative buoyancy of the dispersed phase through
a continuous phase.
While the figures illustrate a less-dense dispersed phase being
introduced at the bottom of
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the column, it is possible for the dispersed phase to be denser
and introduced at the top,
with the configuration internals appropriately revised.
The turbulent pipe contactor is a parallel-flow device and has
the limits of
efficiency of all such systems, whether they be direct contact
or surface-type heat
exchangers. That is, the maximum temperature
achieved by the cool stream is that of the
mixing cup temperature. The size of the
turbulent pipe contactor is dictated by the
relative mass flow rate and the nature of the
turbulence.Turbulence promoters can be Fig 1.4: Turbulent pipe
contactor
installed to enhance the turbulence and, thereby, reduce the
length of contactor necessary
to essentially obtain the mixing cup temperature. If separation
of the streams is desired,
the contactor must be followed by a separation device such as a
settler, a cyclone
separator, or other mechanisms. While the turbulent pipe
conductor is very inexpensive,
if separation is desired, the cost of the settler will in all
probability dictate the economics
of the process.The remaining apparatus all have the heat
transfer take place between a
continuous phase and a clearly defined disperse phase in the
form of drops, bubbles, jets,
sheets, or thin supported films in the case of packed beds.
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Heat exchangers with
mechanical agitators (Fig 1.5),
while often superior as heat or
mass transfer equipment, are more
difficult to design as the dispersed
phase may have a wide range or Fig 1.5: Typical mechanically
agitated towers
drop or bubble sizes. Thus, empirical data from the manufacturer
to establish
performance is necessary.Further, problems may result in seals
at the penetration point of
the drive shafts. Special designs may therefore be
necessary.
Baffle tray columns may have similar problems in defining the
nature of the
curtain of the dispersed phase. Depending on flow rates and
battle design, the dispersed
phase may be a sheet, a series of rivulets or defined streams,
which can break up into
drops. If the baffles are, in fact, trays with serrated or
notched rims, the dispersed phase
can be designed to be a series of well-defined streams and the
heat transfer is more easily
analyzed. The baffles/trays then result in mixing of the
dispersed phase and enhance the
internal-to-the-dispersed phase mixing.
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Fig 1.6: Baffle tray column
Fig1.7: A possible configuration of a packed bed condenser
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The spray column shown in Fig 1.8 is an open column whose only
internals are
the inlet nozzles for the dispersed and continuous
phase. Ideally, such columns are capable of pure
counter flow operation, with the dispersed phase made
up of nearly uniform diameter drops. While it is
possible to design the dispersed phase inlet nozzle to
achieve the desired characteristics, providing a Fig1.8:
Schematics of a Spray Column
uniform flow in the continuous phase is more difficult. Great
care must be taken or
maldistribution of the continuous phase may lead to diminished
heat transfer. Thus, the
design of continuous phase inlet nozzles is sometimes
proprietary, or patented.
The bubble column or sieve tray column (see Fig 1.9) enhances
the internal heat
transfer coefficient by repeatedly reforming the drops at each
tray. Proper tray or baffle
design can lead to shorter columns, and potentially small heat
exchanger volume for the
same service. Their major disadvantage is fouling, corrosion or
blockage of some of the
holes in the sieve tray.
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Fig 1.9: Schematic of a sieve tray column
A liquid to liquid heat exchanger designed for highly efficient
heat transfer
covering a wide variety of liquid types. The heavy duty design
makes it ideal for
demanding commercial, industrial and residential applications
where high performance
and low maintenance are important. Here transfer coefficients
are greater than
conventional shell and tube or plate exchangers because of the
enhanced heat exchange
surface and counter flow design.
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1.3.2 Classification according to flow type:
1.3.2(a) Parallel flow Heat Exchanger The hot and cold fluids
enter the same end,
flow in the same direction and leave at the same end.
Fig 1.10: Schematic of a Parallel flow & a Counter Flow Heat
Exchanger
1.3.2(b) Counter flow Heat Exchanger The hot and cold fluids
enter at opposite ends,
flow in opposite direction and leave at opposite ends.
1.3.2(c) Cross flow heat exchanger The flow of one fluid is
perpendicular to the other
fluid.
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Fig 1.11: Schematic of a Cross Flow Heat Exchanger
1.3.3 Classification according to Construction Type
1.3.3(a) Tubular Heat Exchangers-
These exchangers are generally built of
circular tubes, although elliptical,
rectangular, or round/flat twisted tubes
have also been used in some
Fig1.12: Tubular Heat Exchanger applications. There is
considerable flexibility in
the design because the core geometry can be varied easily by
changing the tube diameter,
length, and arrangement. Tubular exchangers can be designed for
high pressures relative
to the environment and high-pressure differences between the
fluids. Tubular exchangers
are used primarily for liquid-to-liquid and liquid-to-phase
change (condensing or
evaporating) heat transfer applications. They are used for
gas-to-liquid and gas-to-gas
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heat transfer applications primarily when the operating
temperature and/ or pressure is
very high or fouling is a severe problem on at least one fluid
side and no other types of
exchangers would work. These exchangers may be classified as
shell-and tube, double-
pipe, and spiral tube exchangers. They are all prime surface
exchangers except for
exchangers having fins outside/inside tubes.
1.3.3(b) Plate-Type Heat Exchangers-Plate-type
heat exchangers are usually built of thin plates (all
prime surface). The plates are either smooth or have
some form of corrugation, and they are either flat or
wound in an exchanger. Generally, these
exchangers cannot accommodate very high
pressures, temperatures, or pressure and Fig1.13 Plate-Type Heat
Exchanger
temperature differences. Plate heat exchangers (PHEs){ can be
classified as gasketed,
welded (one or both fluid passages), or brazed, depending on the
leak tightness required.
Other plate-type exchangers are spiral plate, lamella, and
platecoil exchangers.
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1.3.3(c) Extended Surface Heat
Exchangers- The tubular and
plate-type exchangers described
previously are all prime surface
heat exchangers, except for a shell-
and-tube exchanger with low
finned tubing. Their heat
exchanger effectiveness is usually Fig1.14: Extended Surface
Heat Exchanger
60% or below, and the heat transfer surface area density is
usually less than 700 m2 /m3
(213 ft2 /ft3). In some applications, much higher (up to about
98%) exchanger
effectiveness is essential, and the box volume and mass are
limited so that a much more
compact surface is mandated. Also, in a heat exchanger with
gases or some liquids, the
heat transfer coefficient is quite low on one or both fluid
sides. This results in a large heat
transfer surface area requirement. One of the most common
methods to increase the
surface area and exchanger compactness is to add the extended
surface (fins) and use fins
with the fin density ( fin frequency, fins/m or fins/in.) as
high as possible on one or both
fluid sides, depending on the design requirement. Addition of
fins can increase the
surface area by 5 to 12 times the primary surface area in
general, depending on the
design. The resulting exchanger is referred to as an extended
surface exchanger. Flow
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22
area is increased by the use of thin gauge material and sizing
the core properly. The heat
transfer coefficient on extended surfaces may be higher or lower
than that on unfinned
surfaces. For example, interrupted (strip, louver, etc.) fins
provide both an increased area
and increased heat transfer coefficient, while internal fins in
a tube increase the tube-side
surface area but may result in a slight reduction in the heat
transfer coefficient, depending
on the fin spacing. Generally, increasing the fin density
reduces the heat transfer
coefficient associated with fins. Flow interruptions (as in
offset strip fins, louvered fins,
etc.) may increase the heat transfer coefficient two to four
times that for the
corresponding plain (uncut) fin surface. Plate-fin and tube-fin
geometries are the two
most common types of extended surface heat exchangers.
1.3.3(d) Regenerators- The
regenerator is a storage-type heat
exchanger, as described earlier.
The heat transfer surface or
elements are usually referred to
as a matrix in the regenerator. Fig1.15:Regenerator
To have continuous operation, either the matrix must be moved
periodically into and out
of the fixed streams of gases, as in a rotary regenerator , or
the gas flows must be
diverted through valves to and from the fixed matrices as in a
fixedmatrix regenerator.
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23
The latter is also sometimes referred to as a periodic-flow
regenerator, a swing
regenerator, or a reversible heat accumulator.
1.3.4 Classification According to Number of Fluids
Most processes of heating, cooling, heat recovery, and heat
rejection involve transfer of
heat between two fluids. Hence, two-fluid heat exchangers are
the most common. Three-
fluid heat exchangers are widely used in cryogenics and some
chemical processes (e.g.,
air separation systems, a heliumair separation unit,
purification and liquefaction of
hydrogen, ammonia gas synthesis). Heat exchangers with as many
as 12 fluid streams
have been used in some chemical process applications.
1.3.5 Classification According to Surface Compactness-
Compared to shell-and-tube exchangers, compact heat exchangers
are characterized by a
large heat transfer surface area per unit volume of the
exchanger, resulting in reduced
space, weight, support structure and footprint, energy
requirements and cost, as well as
improved process design and plant layout and processing
conditions, together with low
fluid inventory. A gas-to-fluid exchanger is referred to as a
compact heat exchanger if it
incorporates a heat transfer surface having a surface area
density greater than about 700
m2 /m3. In case of heat transfer surface having a surface area
density less than about 700
m2/m3 then it is called non-compact heat exchanger.
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24
1.4 Spray Column
1.4.1 Spray Column
In this study of liquid liquid heat transfer Spray Column is
used as a heat
exchange equipment. A Spray Column is a two phase contactor used
to achieve the mass
& heat transfer between a continuous phase & a dispersed
phase. It consists of empty
cylindrical vessel made of steel or plastic & nozzles that
spray liquid in the vessel. The
light phase usually enters the bottom of the tower and moves
upward while the heavy
phase moves downward.
A spray is a dynamic collection of drops dispersed in a gas. The
process of
forming a spray is known as atomization. A spray nozzle is the
device used to generate a
spray. The two main uses of sprays are to distribute material
over a cross-section and to
generate liquid surface area. There are thousands of
applications in which sprays allow
material to be used most efficiently. The spray characteristics
required must be
understood in order to select the most appropriate technology,
optimal device and size.
It is mainly considered as a gas liquid contactor. But it also
works on liquid-liquid
contact. The common design consists of an empty cylindrical
shell through which the gas
flows upwards against a downflowing spray of the absorbing
liquid .Here the gas is the
continuous phase & the liquid is the dispersed phase. The
liquid is dispersed in the form
of fine droplets near the top by forcing it through spray
nozzles. Spraying should be
uniform over the cross-section of the vessel for the sake of
better gas liquid contact. The
liquid droplets have a distribution of size. The contact time
between the droplets & the
gas has also a distribution. A fraction of the droplets
unavoidably strike the wall of the
tower and the liquid flows down as a film. Backmixing of the gas
remains small in a
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25
spray tower. The raining droplets are collected at the bottom
and liquid leaves through a
nozzle. A demister is invariably used to prevent entrainment of
droplets in the exit gases.
The Spray tower can handle a large volumetric gas flow rate at a
low pressure drop. The
HTU is substantially large. Pumping the liquid at a high
pressure to the spray nozzles
involves substantial power consumption. The absence of any
moving parts is also an
advantage of the spray Column. The device is particularly
suitable for a. corrosive liquids
& gases, b. liquids containing suspended solid, c. gas
streams may contain dust, d. low
gas pressure drop application, e. scrubbing various waste gas
stream, f. liquid-liquid
extraction.
1.4.2 Spray formation
Spray atomization can be formed by several methods. The most
common method
is through a spray nozzle which typically has a fluid passage
that is acted upon by
different mechanical forces that atomize the liquid. The first
atomization nozzle was
invented by Thomas A. DeVilbiss of Toledo, Ohio in the late
1800s His invention was
bulb atomizer that used pressure to impinge upon a liquid,
breaking the liquid into a fine
mist. Spray formation has taken on several forms, the most
common being, pressure
sprayers, centrifugal, electrostatic and ultrasonic nozzle.
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26
1.4.3 Flow Patterns in a Spray Column
Fig 1.16: Typical countercurrent-flow spray tower
Fig1.17: Crosscurrent-flow spray tower
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27
Chapter-2 Literature review
-
28
Letan & Kehat (1967) studied the mechanics of a Spray
Column. Local & average
hold up & drop size distribution as function of flow rates
which were measured for
kerosene drops and water in a counter current , 15cm I.D., 160cm
long Spray Column.
The range of flow rates was 5 to 40 liters/min of kerosene &
0 to 50 liters/min of water.
At the same pairs of flow rates of the dispersed and the
continuous phases in spray
columns, three modes of drop packing can be obtained. These are
termed, in order of
increasing average hold up and increasing regularity of flow
patterns, dispersed,
restrained, and dense packing. For dispersed packing, at low
flow rates of the two phases,
the hold up and the drop size are constant along the column. At
high flow rates the drop
size increases from bottom to top of the column & hold up
increases from top to bottom
of the column. The range of flow rates for the operation of a
spray column is extended by
use of a conical entry section (Elgin design) at the bottom of
the column, by the
formation of an equilibrium region in the conical section. The
average hold up increases
with flow rates of both phases for dispersed & restrained
packing, and restrained packing
and with decreased flow rates of both phases for dense packing.
The best definitions of
flooding in a spray column are either the point of maximum
average specific area of the
drops, which corresponds to the onset of coalescence in the
column, or the start of
rejection of drops from the column proper.
Siqueiros & Bonilla (1999) did an experimental study of a
three-phase, direct-
contact heat exchanger. An experimental pilot scale three-phase,
direct-contact heat
exchanger was constructed and tested. The DCHE (Direct Contact
Heat Exchanger) is a
spray column of 0.61 m (24 in) nominal diameter carbon steel,
3.3 m height with two
distributors. The water (continuous phase) distributor is on the
top of the column. The
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29
pentane (discontinuous phase) distributor is on the bottom of
the column. It has six
viewing windows along its length. The column has two flanges. On
the upper flange the
pentane vapour exit and the security valve were installed. On
the lower flange the cool
brine exit and the liquid pentane inlet were installed.
Steady-state conditions were
reached between 30 and 60 min after the pentane was fed into the
column. The main
parameters of control for each experimental test were the
pentane and water mass flow-
rates. The inlet water temperatures ranged from 75 C to 88C, and
the inlet pentane
temperatures varied from 23 C to 38C. The volumetric heat
transfer coefficient, hold-up
and heat flow-rate are functions of pentane mass flow-rate. For
high pentane/water
volumetric flow ratios flooding was reached. Before reaching
flooding conditions,
accumulation of liquid pentane at the top of the active volume
was found. The volumetric
heat transfer coefficient was achieved in between 4.5-8 KW m 1 K
1 .
Peng et.al, (2001) studied heat transfer in gasliquidliquid
three-phase direct-
contact exchanger. The heat transfer to dispersed droplets in an
immiscible continuous
phase is studied for the n-pentanewater system. The
gasliquidliquid three-phase
section of the exchanger is divided into two stages, where the
volumetric heat transfer
coefficients are developed, respectively. These models take into
account the evaporation
of continuous phase water into the dispersed phase and the
two-phase droplets break-up.
The calculated results showed good agreement with the
experimental values. This paper
studies the heat transfer in a parallel flow exchanger and
discusses the effects of some
operational parameters on the volumetric heat transfer
coefficient. Some expressions take
account of the possible coalescence and break-up of the
droplets. The expressions may
improve our insight into the dependencies of the total heat
transfer performance of
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30
exchangers on individual operational parameters and, indirectly,
on the exchanger design.
The exchanger is made of plexiglass with an inside diameter of
90mm and a length of
2000 mm. On both sides of the exchanger there are 20 holes with
a diameter of 8mm each
and which are used for measuring the temperature and pressure.
n-Pentane is used as the
dispersed fluid. It is injected into the exchanger from a
distributor located at the bottom
of the exchanger. Hot water is supplied to the exchanger from
the bottom when it is
heated to the given temperature in the heater. The water flow
rate is measured by using a
rotameter. A volumetric heat transfer coefficient was achieved
in between the range of
20-120 KW m 3 K 1 for variation in column elevations (0-2m) at
different flow rates of
dispersed & continuous phase.
Pierce et.al (1959) studied heat transfer and fluid dynamics in
mercury-water
spray columns. Heat transfer and fluid dynamics were studied in
columns in which hot
mercury was sprayed into a rising stream of water. Volumetric
and area heat transfer
coefficients are presented which were found to be lower than
those reported for heat
transfer from fixed spheres. It was observed that considerable
water bypassed the stream
of drops, while some surrounding the drops flowed downward. This
behavior resulted in
water temperatures at the base of the column which were
considerably higher than the
inlet water temperatures. Consequently the outlet mercury
temperature did not approach
the inlet water temperature as a limit. The very unconventional
flow pattern of the water
was unexpected and is believed to be an important factor in
spray-column heat transfer
and mass transfer kinetics. Six different columns were used, but
the same steel end
assemblies were used with each. The columns were fabricated from
1- and 2-in. I.D.
Pyrex pipe. The enlarged ends of the columns were 6 in. I.D. to
accommodate the end
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31
assemblies. Measurements of temperatures, mercury flow rate,
water flow rate, drop
sizes, drop velocities, water phase movements were measured
& varied during the
experiment. The volumetric heat transfer coefficient observed in
between the range of
19.3*103 B.T.U/hr-cubic ft-0F to 48.3*103 B.T.U/hr-cubic ft-0F
for a column of 1 inch
diameter, 13.25 inch length where water flow rate were
maintained at 54.8 to 109.8
gal/min-sq ft & mercury flow rate were maintained at 2000 to
5000 lb/min-sq ft.
Hanna et.al presented investigation deals with experimental and
theoretical
phenomenological study of three phase direct-contact heat
exchanger, for n-pentane
water system. The test section consisted of a cylindrical
perspex column 17.2cm I.D. and
1m long, in which, distilled water, was to be confined. Liquid
n-pentane drops were
injected into the hot water filled column, through a special
design of two distributors. A
study of speed and high resolution camera films taken during the
heat transfer process
rendered information regarding the bubble shape, bubble size,
and evaporation rates of n-
pentane drops evaporating in hot water. The study was devoted to
express the effect of
process variables on heat transfer coefficient, and volumetric
heat transfer coefficient and
effectiveness. From this parametric analysis of this
countercurrent column it was found
that The volumetric heat transfer coefficient values fall with
an increase in the inlet
temperature of water. Small-diameter nozzles associated with
faster nozzle velocities, and
smaller droplets, yield higher volumetric heat transfer
coefficient, and larger heat transfer
coefficients gave higher values of volumetric heat transfer
coefficient .It was found that
volumetric heat transfer coefficient varied in between 0.5 KW/m3
0C to 4 KW/m3 0C for
the water flow rate 5 cm3/s to 55 cm3/s and n-pentane flow rate
0.8 cm3/s to 2 cm3/s.
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32
Mahood & Sharif et. Al (2013) developed a model for
temperature distribution of
a spray column, three-phase direct contact heat exchanger. This
study is for the relative
velocity and the drag coefficient of the evaporation swarm of
drops in an immiscible
liquid, using a convective heat transfer coefficient of those
drops. They assume a constant
holdup ratio (range 0.14 to 0.165) along the direct contact
column. From this study it is
been evaluated that the variation of dispersed and continuous
phase temperatures and the
spray column height at different initial phases temperatures and
flow rates, with an initial
drop radius equal to 2mm and 1.6mm. At the phases entrance, at
the fist zone where the
temperature difference is at its maximum between the phases. In
this region a high
increase in dispersed temperature occurs, while nearly a
constant temperature in the
continuous phase. This zone covers a very short length of the
column (about 1m), and it
seems independent of the operational column parameters. In the
second zone, a slow heat
exchange occurs between the phases and this region cover a wide
range of the column
height. At the final zone the temperature difference decreases
to minimum. The results
have shown that the rate of heat transfer increases with
decreasing drops size. And the
heat exchange is influenced by the vaporization ratio.
Letan & Kehat(1968) studied the mechanism of heat transfer
in a Spray Column
Heat Exchanger. Temperature profiles of water in a Spray Column
Heat Exchanger 15cm
in diameter and 150cm long operating with a dense packing of
kerosene drops were
measured. The range of superficial velocities was 0 to 0.8 cm/s
for water and 0.5 to 1.7
cm/s of kerosene. The bottom of the dense packing was either
slightly above or 15 cm
below the bottom of the column proper. The mathematical
equations for dispersed
packing of drops were modified to take into the account of the
reduction of wake size at
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33
the interface of the two packings and the difference in the
mixing patterns at the top of
the column.This operation was controlled by the fluid mechanics
of the system and not
by the resistance to heat transfer inside or at the surface of
the drops. The thermal
performance of the small diameter column was reduced
significantly by the effect of
bypassing and was also reduced if the bottom of the dense
packing of drops was
maintained within the conical bottom entry section.
Sathiyan (2011) et.al studied heat transfer for water-diesel
two-phase system in a
Spiral Heat Exchanger. In this study, the main objective was to
evolve a correlation to
predict liquid-liquid two-phase heat transfer coefficients in a
spiral plate heat exchanger.
Experimental studies were conducted in a spiral plate heat
exchanger using the liquid-
liquid two-phase system of water-diesel in different volume
fractions and flow rates as
the cold fluid. Experiments were conducted by varying the
volumetric flow rate and
temperature, keeping the volumetric flow rate of hot fluid
constant. The two-phase heat
transfer coefficients were correlated with Reynolds number,
Prandtl number and volume
fraction in the form Nu = a (Re) b (Pr) c () d. The data
obtained from fresh experiments
were compared with the predictions of the obtained correlation.
The predicted
coefficients showed a spread of 12 % in the laminar range,
indicating the potential use
for practical applications. For 40% water + 60% diesel mixture
it was found that the
overall heat transfer coefficient varied in the range of 162.22
- 766.06 W/m2K.
Zabulok et.al studied experimental investigation of direct
contact heat transfer in
Isopentane-water system. The test section consisted of a
cylindrical perspex column, in
which distilled water was to be confined. Liquid isopentane
drops were injected into the
hot water filled column through special distributors located at
the bottom of the column.
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34
Various operating and design parameters were investigated and
their effects on the
overall performance of the heat transfer process were deduced.
The experimental runs
were planned using the central composite rotatable design
method. It has been found that
the volumetric heat transfer coefficient values fall with an
increase in the inlet
temperature of water, also small-diameter nozzles associated
with faster nozzle velocities,
and smaller droplets, yield higher volumetric heat transfer
coefficient. In addition, iso-
pentane was found to yield a slightly higher volumetric heat
transfer coefficient
compared with n pentane. The inlet water temperature was
maintained in between 300C
to 380C & the volumetric flow rate of water & Iso
pentane was maintained in between
9.8-49 cm3/s and 0.96 to 1.92 cm3/s, respectively. The
volumetric heat transfer coefficient
varies in the range between 3-7 KW/m3 0C.
Ming Yeh (2010) performed an analysis of heat transfer in the
heat exchangers of
cocurrent and countercurrent flows with external recycle. It has
been carried out by heat-
transfer theory. Considerable improvement is achievable by
recycle operation if the
increase in heat-transfer coefficient by applying the recycle
effect to enhance the fluid
velocity can compensate for the decrease in the driving force
(temperature difference) of
heat transfer due to the remixing of inlet fluid. As expected,
the heat-transfer rate
obtained in the countercurrent-flow heat exchangers with or
without recycle is superior to
those in the cocurrent-flow devices. However, the space for the
improvement in
performance by recycle in the countercurrent-flow device is
smaller than that in the
cocurrent-flow one.
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35
Terasaka and Tsuge (Terasaka & Tsuge, 1993) studied the
bubble volumes and
shapes formed from a constant-flow nozzle submerged in a liquid.
They photographed
the bubble shapes during bubble formation with a high-speed
video camera, using
different liquids in N2 gas such as tap water and 68 Wt %
glycerol.
Sideman et al. (1965) investigated the spray column with fixed
dispersed phase
flow rates and different diameters of orifices using the
n-pentane / sea water system. The
results show that the smaller the droplets, the smaller the
optimal volume, and the larger
the volumetric heat transfer coefficient.
Sideman and Gat. (1966) measured the volumetric heat transfer
coefficient and
column heights required to vaporize pentane in water. Volumetric
heat transfer
coefficients were in the range of 8,000 to 20,000 kJ/m hr. C,
and the results show that the
coefficients decrease with increasing driving force.
Brickman and Boehm (1994) studied the liquid-liquid
direct-contact heat
exchangers for the purpose of finding the design that brings the
temperature difference
between the two fluids to as a small value as possible, using
oil-water system. They
confirmed that a longer column and smaller droplet size yield an
increase in
effectiveness.
Shahidi & Ozbelge et. Al (1995) investigated direct contact
heat transfer between
water and a heat transfer oil under non-boiling conditions in
co-current turbulent flow
through a horizontal concentric annulus. The ratio of the inner
pipe diameter to the outer
pipe diameter (aspect ratio) K = 0.730-0.816; total liquid
velocity (mixture velocity) =
0.42 1.1 m/s; inlet oil temperature = 38 94C; oil volume
fraction in the flowing
mixture = 0.25 0.75 were varied and their effects on the overall
volumetric heat
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36
transfer coefficient were determined at constant interfacial
tension of 48 dynes/cm. It
was found that, in each concentric pipe set, the overall
volumetric heat transfer
coefficient increased with increasing dispersed phase volume
fraction at each constant
mixture velocity and reached a maximum at around = 0.5. The
maximum U v
values increased with increasing total liquid velocity and
decreasing aspect ratio of the
annulus. The volumetric heat transfer coefficient was also found
to increase with
increasing inlet oil temperature and increasing total liquid
velocity but to decrease with
length along the test section keeping all other parameters
constant. Empirical expressions
for the volumetric heat transfer coefficient were obtained
within the ranges of the
experimental parameters.
Mori (1991) studied the evaporation of drops of a volatile
liquid sprayed upward
in an immiscible liquid flowing down in a vertical column, and
derived an expression for
the volumetric heat transfer coefficient in a counter flow spray
column. The expression of
the volumetric heat transfer coefficient was used to predict its
values under some
particular column operating conditions, which were then compared
with relevant
experimental data found in the literature.
Rasheed (1999) studied the direct-contact evaporation of a drop
moving in a
stagnant column of an immiscible liquids, using n-pentane-water,
2-methyl pentane-
water, and n-pentane/2-methyl pentane-water systems. A
theoretical analysis of
evaporating droplets in an immiscible liquid was developed by
solving the governing
equations of the motion and heat transfer numerically by
Runge-Kutta method, assuming
a spherical drop in a column of stagnant immiscible liquid at
uniform temperature.
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37
Chapter 3 Aim & objectives
-
38
It reveals from the literature survey that Direct Contact Heat
Exchangers (such as
Spray Column, Mechanically agitated Column, Packed Column etc.)
between two
immiscible fluids have shown many advantages because of higher
effective heat transfer
coefficients, a relatively simple design that provides cost
effective performance and
absence of surface scaling.
Ming Yeh (2010) in his study reported that heat-transfer rates
obtained in the
countercurrent-flow heat exchangers with or without recycle, are
superior to those in the
cocurrent-flow device, the space for the improvement by recycle
in the countercurrent-
flow device is also smaller than that in the cocurrent-flow one.
This fact will be more
obvious when the devices are operated under higher temperature
difference and/or low
flow rate and/or smaller reflux ratio
With respect to liquid/liquid countercurrent studies in these
devices, Letan and
Kehat (1967) gave a theoretical model in which heat transfer in
a spray column is
controlled by the fluid dynamics of the system, and not by the
resistance to heat transfer
inside or at the surface of the drops. Siqueiros &
Bonilla(1999) did an experimental study
of heat transfer in a countercurrent Spray Column. The
experimental study resulted in
enhancement of heat transfer coefficient, thermal efficiency
etc. The volumetric heat
transfer coefficient found to be in the range of 4.5-8 KW m 1 K
1 . Again from the heat
transfer study in between mercurywater in a counter-current
spray column done by
Pierce et.al (1959) desirable heat transfer effects were found.
Mercury flow rate, water
flow rate, drop sizes, drop velocities, water phase movements
were measured & varied
during the experiment. The volumetric heat transfer coefficient
observed in between the
range of 19.3x103 B.T.U/hr-cubic ft-0F to 48.3x103
B.T.U/hr-cubic ft-0F for a column of 1
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39
inch diameter, 13.25 inch length where water flow rate were
maintained at 54.8 to 109.8
gal/min-sq ft & mercury flow rate were maintained at 2000 to
5000 lb/min-sq ft.
Extremely rapid heat transfer was experienced between the
dispersed phases in the
mercury-water columns. The major heat transfer resistance was
within the bulk of the
water phase. Heat transfer results did not vary appreciably with
minor change in column
design nor between 1 and 2 inch diameter columns, but the column
efficiencies decreased
markedly with increased column length. This study has
illustrated that flow patterns can
greatly limit the efficiency of liquid-liquid spray columns.
Because of the disadvantages reported in cross flow heat
exchanger as stated above and the
positive aspects of counter flow Spray Column reported by Pierce
et al. ( 1959 ), project aims
liquid to liquid heat transfer in a counter flow Spray Column.
By the application of this
contactor, the performance is expected to enhance the heat
transfer coefficient with reduced
heat loss. Therefore a project aimed to study heat transfer
performance of spray column with
water-kerosene system.
The objectives of the proposed project include:
1. To determine the heat transfer coefficient in a counter flow
Spray Column.
2. To study the effect of water & kerosene flow rate on heat
transfer characteristics
& thermal efficiency.
3. To reduce the heat loss.
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40
Chapter 4 ExpErimEntal sEction
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41
4.1 Experimental set up
A schematic diagram of apparatus is given in Fig 4.2. It
consists of a stainless
steel oil tank, a spray column, oil & water pump, a
stainless steel water bath equipped
with a 400V electrical heater, an electrical stirrer & a
thermocouple connected to the
digital temperature controller to keep the inlet water
temperature constant at the desired
value.
The heat transfer section is a vertical column made up of
stainless steel and has a
provision to change its height. A stationary distributor of 76
mm diameter, located at the
bottom of column, consisting of number of 1 mm diameter holes on
its surface was used
to spray kerosene around the heat transfer zone. The casing on
which the unit along with
the distributor is installed was cylindrical in shape, with a
diameter of 80 mm and axial
length of 120 cm. For another column this height was 95 cm.
A magnetic pump is used to feed warm water from a storage tank
of capacity
around 100 liters, maintained at a constant temperature to the
heat transfer unit. Kerosene
is sprayed against the vertically down flowing hot water, in the
cylindrical column and
flow vertically upward. There is a by pass system in the storage
tank to maintain uniform
temperature of the water bath, also there are two stirrers in
the water tank to maintain
constant mixing. Kerosene used for cooling the warm water was
fed to the column, by a
pump, in the reverse direction of gravity or in the upward
direction. One control valve is
provided at the water outlet for maintaining the water level in
the column. The spray
column provides a counter-flow contact of kerosene and warm
water.
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42
The water and kerosene flow rates were measured by previously
calibrated
rotameter of capacity 0.1-1 LPM and 0.2-2 LPM respectively. The
temperature of the
water entering and leaving the column was measured by
thermocouple connected to a
digital display. Also, the entering and exit kerosene
temperature was measured by
thermocouple connected to the digital display. Flow rates of
liquids were controlled by
the valves on the bypass line of the pumps and adjusting the
indivisual rotameters.
To reduce the heat loss the total heat transfer unit was covered
with two layers of nylon
rope .
4.2 Experimental Procedure
Distilled water was heated in a constant temperature bath with
the temperature
fixed at 55 C. After the temperature reaches to 55 C, the
stirrers along with the
recirculation in the bath was switched on to maintain complete
mixing and uniform
temperature of the water bath. In the mean time the water pump
was switched on with the
water flow rate fixed at the desired value, made to pass through
the column for 5-7 min
so that a steady state is attained. The water flow rates used
are 0.2, 0.3, 0.4, 0.5 LPM. The
water level was fixed in the column by adjusting the control
valve at the water outlet.
The kerosene flow rate is switched on now and the desired flow
rate is maintained by the
rotameter. The kerosene flow rates used are 0.2, 0.3, 0.4, 0.5
LPM. The hot water flows
downward & kerosene was sprayed at the bottom & flows in
the upward direction.
Now keeping the water flow rate, kerosene flow rate fixed it is
allowed to reach a
steady state. Subsequently after reaching the steady state in 7
to 8 minutes, few sets of
reading for inlet water temperature, outlet water temperature,
inlet kerosene temperature,
outlet kerosene temperature, was noted down at a regular
interval of 4 minutes for 20 to
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43
24 minutes and the most steady state of the readings is reported
among those noted. Also
the actual water & kerosene outlet flow rate were noted.
Then the water bath temperature
was increased to 64 0C and the above procedure was repeated with
the same kerosene and
water flow rate.
The whole experimental procedure was performed by varying the
height of the
column from 80 cm to 105 cm. Each set of run last for about
approximately 40 min. After
each set of run the machine was given rest for around 1 hr. In
the entire set of run for the
two sets of height the kerosene inlet temperature was found to
vary from 26.5 C to 32.9
C.
Fig 4.1: Overall Experimental Set Up
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44
Fig 4.2: Schematic of Experimental Set Up
A-Water Bath, B-Valve, C-Magnetic Pump, D- Gear Pump,
E-Rotameter, F-
Kerosene Bath, G-Spray Column, H-Water Inlet, I-Water Outlet,
J-Kerosene
Inlet, K-Kerosene Outlet, L- Stirrer, M-Heating Coil
-
45
Chapter 5
Results & Discussion
-
46
As stated earlier, this heat transfer study was performed for
two column heights in
counter flow mode between two liquid phases i.e. water and
kerosene.
Value/Range of Operating Parameters in the study
qw=0.2LPM-0.5LPM ,
qk =0.2LPM-0.5LPM
Water bath Temperature- 550C -650 C
H=95cm-120cm, d= 8cm, t=2mm
w = 988.1 Kg/m3 at 550C, 983.2 Kg/m3 at 640C
k = 800 Kg/m3
C pw= 4.1806 KJ/ Kg-K at 550C, 4.1843 KJ/Kg-K at 640C
C kw= 2.01 KJ/ Kg-K
5.1 Study of Heat Loss in counter-flow Spray Column
Preliminary experimentation for calculation of heat loss in the
equipment was conducted
in the beginning so as to consider it during the calculations of
heat transfer coefficient for
accuracy purpose. The data for heat loss in Spray Column in Watt
is as given below
Table1: Heat loss at Water Bath Temperature-55 0C & Column
Height- 105 cm
Water Flow Rate (LPM) 0.2 0.3 0.4 0.5
Kerosene Flow Rate (LPM)
0.2 19.12 16.47 10.10 19.62
0.3 10.76 5.88 8.74 16.21
0.4 6.33 14.29 17.75 5.58
0.5 15 18.4 11.58 4.98
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47
Table2: Heat Loss at Water Bath Temperature- 64 0C & Column
Height- 105 cm
Water Flow
Rate (LPM) 0.2 0.3 0.4 0.5
Kerosene Flow
Rate(LPM)
0.2 20.87 21.71 26.05 26.33
0.3 2.30 18.53 24.94 16.6
0.4 1.4 14.1 22.8 16.96
0.5 2.61 17.93 8.76 8.67
Table3: Heat Loss at Water Bath Temperature- 55 0C & Column
Height- 80 cm
Water Flow
Rate (LPM) 0.2 0.3 0.4 0.5
Kerosene Flow
Rate (LPM)
0.2 14.14 2.34 25.72 0.62
0.3 0.74 6.96 2.49 0.63
0.4 22.20 25.10 10.81 7.99
0.5 29.22 23.86 14.70 5.71
-
48
Table4: Heat loss at Water Bath Temperature- 64 0C & Column
Height- 80 cm
Water Flow
Rate (LPM) 0.2 0.3 0.4 0.5
Kerosene Flow
Rate (LPM)
0.2 26.98 4.37 1.60 0.98
0.3 49.38 29.45 4.28 23.25
0.4 33.98 27.46 28.44 14.17
0.5 12.48 29.45 5.89 0.94
It can be seen a certain amount of heat loss in each of the
cases does exists. So,
the heat loss term, being considerable, was added in heat
transfer coefficient calculations
for the sake of accuracy in the governing equation.The amount of
kerosene coming out
from water outlet is negligible. 1 L of kerosene content in a 50
L of water bucket was
measured.
From the above experimental data thermal efficiency &
overall heat transfer coefficient
of the column were determined.
-
49
5.2 Calculation of Thermal Efficiency
Thermal efficiency for both height of the column & varying
water bath
temperature were determined. The simultaneous heat transfer of
the spray Column was
presented in terms of thermal efficiency defined as
= Actual heat transfer/ Maximum possible heat transfer
= TTTT
KIWI
WOWI
The effectiveness lies in between 0 to 1.
5.3 Calculation of Heat Transfer Coefficient
To calculate the overall heat transfer co-efficient (h) a model
equation is
developed and represented as
lQ
lATTh
dxdT
kowoaw
pwwcm.
)(
-
50
5.4 Effect of Water flow rate on h & Fig 5.1 and Fig 5.2
illustrates the variation of thermal efficiency with water flow
rate, at kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM for
water bath temperature 55 0C
& 640 C respectively and the column height of 105 cm. It can
be seen that the thermal
efficiency increased as the water flow rate decreased &
increased with increase in the
kerosene flow rates. For example, at a constant kerosene flow
rate of 0.2 LPM, the
thermal efficiency for the column decreased from 0.21 to 0.10
with an increase in water
flow rate from 0.2 LPM to 0.5 LPM for water bath temperature 55
0C, whereas in case of
constant water flow rate of 0.2 LPM thermal efficiency increases
from 0.21 to 0.43 with
an increase in kerosene flow rate from 0.2 LPM to 0.5 LPM for
water bath temperature
64 0C.
Fig 5.3 and Fig 5.4 plots the variation of thermal efficiency
with water flow rate
for kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM, water
bath temperature 550C & 640C
and the column height 80 cm. It was found that the thermal
efficiency decreased as the
water flow rate increased & increased with increase in the
kerosene flow rates which are
quite clear from the plots. For example, at a constant kerosene
flow rate of 0.2 LPM, the
thermal efficiency for the column decreased from 0.21 to 0.11
with an increase in water
flow rate from 0.2 LPM to 0.5 LPM for water bath temperature 55
0C. Where as in case
of constant water flow rate of 0.2 LPM thermal efficiency
increases from 0.22 to 0.39
with an increase in kerosene flow rate from 0.2 LPM to 0.5 LPM
for water bath
temperature of 64 0C.
-
51
Fig 5.1: Effect of water flow rate on thermal efficiency at
water bath
temperature 55 0C & Column Height 105 cm
Fig 5.2: Effect of water flow rate on thermal efficiency at
water bath
temperature 64 0C & Column Height 105 cm
00.050.1
0.150.2
0.250.3
0.350.4
0.450.5
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Ther
mal
Effi
cien
cy
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
0
0.050.1
0.15
0.20.25
0.3
0.350.4
0.45
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Ther
mal
Effi
cien
cy Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
-
52
Fig 5.3: Effect of water flow rate on thermal efficiency at
water bath
temperature 55 0C & Column Height 80 cm
Fig 5.4: Effect of water flow rate on thermal efficiency at
water bath
temperature 64 0C & Column Height 80 cm
00.05
0.10.15
0.20.25
0.30.35
0.40.45
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Ther
mal
Effi
cien
cy
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
0
0.050.1
0.15
0.20.25
0.3
0.350.4
0.45
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Ther
mal
Effi
cien
cy
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
-
53
Fig 5.5 and Fig 5.6 depicts the variation of heat transfer
coefficient with water
flow rate for kerosene flow rates of 0.2, 0.3, 0.4 & 0.5
LPM, water bath temperature 550C
& 640 C and the column height of 105 cm. It was found that
the heat transfer coefficient
increased as the water flow rate increased & decreased with
increase in the kerosene
flow. For example, at a constant kerosene flow rate of 0.2 LPM,
the heat transfer
coefficient for the column increased from 360 to 730 W/m2K with
an increase in water
flow rate from 0.2 LPM to 0.5 LPM for water bath temperature 55
0C. Where as in case
of constant water flow rate of 0.2 LPM heat transfer coefficient
decreases from 442 to
232 W/m2K with an increase in kerosene flow rate from 0.2 LPM to
0.5 LPM for water
bath temperature 64 0C.
Fig 5.7 and Fig 5.8 plots the variation of heat transfer
coefficient with water flow
rate, at kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM for
water bath temperature 550C &
640 C respectively and the column height is 80 cm. It can be
seen from figures that the
heat transfer coefficient increased as the water flow rate
increased & decreased with
increase in the kerosene flow rates. For example, at a constant
kerosene flow rate of 0.2
LPM, the heat transfer coefficient for the column increased from
465 to 775 W/m2K with
an increase in water flow rate from 0.2 LPM to 0.5 LPM for water
bath temperature
550C. Whereas in case of constant water flow rate of 0.2 LPM,
heat transfer coefficient
decreases from 478 to 295 W/m2K with an increase in kerosene
flow rate from 0.2 LPM
to 0.5 LPM for constant water bath temperature of 640C.
-
54
Fig 5.5: Effect of water flow rate on heat transfer coefficient
at water bath
temperature 550C & column height 105cm
Fig 5.6: Effect of water flow rate on heat transfer coefficient
at water bath
temperature 640C & column height 105cm
0
100
200
300
400
500
600
700
800
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
0
100
200300
400
500
600700
800
900
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Heat
Tra
nsfe
r Co
effic
ient
(W/m
2 K)
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
-
55
Fig 5.7: Effect of water flow rate on heat transfer coefficient
at water bath
temperature 550C & column height 80cm
Fig 5.8: Effect of water flow rate on heat transfer coefficient
at water bath
temperature 640C & column height 80cm
0
100200
300400
500600
700800
900
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
0100200300400500600700800900
1000
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Qw(LPM)
Hea
t Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Qk=0.2LPMQk=0.3LPMQk=0.4LPMQk=0.5LPM
-
56
5.5 Effect of variation in Water Inlet Temperature on h &
Fig 5.9 & 5.10 shows the variation of thermal efficiency with
change in the water
inlet temperature at constant water flow rate and kerosene flow
rates which are
maintained in between the range of 0.2 to 0.5 LPM for column
height of 105 cm & 80 cm
respectively . Water bath temperature was maintained at 550C
& 640C. It was found that
there is not much variation in thermal efficiency with change in
temperature. It remains
almost same. In some cases thermal efficiency decreased as the
water bath temperature
increased. For example, at a constant kerosene flow rate of 0.3
LPM and 0.2 LPM water
flow rate, the thermal efficiency for the column at 550C is 0.27
decreased to 0.25 at 640C
for the column height 105 cm.
Fig 5.11 & 5.12 plots the variation of heat transfer
coefficient with water flow
rate, at kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM for
water bath temperature 550C
& 640C for the column height is 105 cm & 80cm
respectively . It was found that the heat
transfer coefficient increased as the water bath temperature
increased which is revealed
by the plots. For example, at a constant kerosene flow rate of
0.2 LPM & 0.2LPM water
flow rate, the heat transfer coefficient for the column at 550C
is 360W/m2K increased to
408 W/m2K at 640C for 105 cm column height.
-
57
Fig 5.9: Effect on thermal efficiency with change in water bath
temperature at
a height 105cm
Fig 5.10: Effect on thermal efficiency with change in water bath
temperature at
a height 80cm
00.050.1
0.150.2
0.250.3
0.350.4
0.450.5
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Ther
mal
Effi
cien
cyQk=0.2LPM, Temp=55CQk=0.3LPM, Temp=55CQk=0.4LPM,
Temp=55CQk=0.5LPM, Temp=55CQk=0.2LPM,
Temp=64CQk=0.3LPM,Temp=64CQk=0.4LPM,Temp=64CQk=0.5LPM,Temp=64C
0
0.05
0.10.15
0.2
0.25
0.30.35
0.4
0.45
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Ther
mal
Effi
cien
cy
Qk=0.2LPM,Temp=55CQk=0.3LPM, Temp=55CQk=0.4LPM,
Temp=55CQk=0.5LPM, Temp=55CQk=0.2LPM, Temp=64CQk=0.3LPM,
Temp=64CQk=0.4LPM, Temp=64CQk=0.5LPM, Temp=64C
-
58
Fig 5.11: Effect on heat transfer coefficient with change in
water bath
temperature at a height 105cm
Fig 5.12: Effect on heat transfer coefficient with change in
water bath
temperature at a height 105cm
0
100200
300
400500
600
700800
900
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Qk=0.2LPM, Temp=55CQk=0.3LPM, Temp=55CQk=0.4LPM,
Temp=55CQk=0.5LPM, Temp=55CQk=0.2LPM,
Temp=64CQk=0.3LPM,Temp=64CQk=0.4LPM,Temp=64CQk=0.5LPM,Temp=64C
0100200300400500600700800900
1000
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Qk=0.2LPM,Temp=55CQk=0.3LPM, Temp=55CQk=0.4LPM,
Temp=55CQk=0.5LPM, Temp=55CQk=0.2LPM, Temp=64CQk=0.3LPM,
Temp=64CQk=0.4LPM, Temp=64CQk=0.5LPM, Temp=64C
-
59
5.5 Effect of Variation in Column Height
Fig 5.13 & 5.14 present the variation of thermal efficiency
with water flow rate, at
kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM for column
height 105 cm & 8 0cm for
water bath temperature 550C & 640C respectively. It was
found that the thermal
efficiency increased as the column height decreased. For
example, at a constant
kerosene flow rate of 0.2 LPM & 0.4 LPM water flow rate, the
thermal efficiency for the
column height 105 cm at 550C is 0.10 increased to 0.12 at 550C
for the 80 cm height. But
in most of the cases thermal efficiency does not vary too much
with column height.
Fig 5.15 & 5.16 plots the variation of heat transfer
coefficient with water flow
rate, at kerosene flow rates of 0.2, 0.3, 0.4 & 0.5 LPM for
column height 105 cm & 80
cm for water bath temperature 550C & 640C respectively. It
was found that the overall
heat transfer coefficient increased as the column height
decreased. For example, at a
constant kerosene flow rate of 0.3LPM & 0.3LPM water flow
rate, the heat transfer
coefficient for the column height 105 cm at 550C is 403 W/m2K
increased to 440 W/m2K
at 550C for the 80 cm height.
-
60
Fig 5.13: Effect on Thermal Efficiency with change in height at
a water bath
temperature 550C
Fig 5.14: Effect on Thermal efficiency with change in height at
a water bath
temperature 640C
00.050.1
0.150.2
0.250.3
0.350.4
0.450.5
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Ther
mal
Effi
cien
cyQk=0.2LPM,H=105cmQk=0.3LPM,H=105cmQk=0.4LPM,H=105cmQk=0.5LPM,H=105cmQk=0.2LPM,H=80cmQk=0.3LPM,H=80cmQk=0.4LPM,H=80cmQk=0.5LPM,H=80cm
0
0.1
0.2
0.3
0.4
0.5
0.6
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Ther
mal
Effi
cien
cy
Qk=0.2LPM,H=105cmQk=0.3LPM,H=105cmQk=0.4LPM,H=105cmQk=0.5LPM,H=105cmQk=0.2LPM,H=80cmQk=0.3LPM,H=80cmQk=0.4LPM,H=80cmQk=0.5LPM,H=80cm
-
61
Fig 5.15: Effect on overall heat transfer coefficient with
change in height at a
water bath temperature 550C
Fig 5.16: Effect on overall heat transfer coefficient with
change in height at a
water bath temperature 640C
0
100200
300
400500
600
700800
900
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2K
)Qk=0.2LPM,H=105cmQk=0.3LPM,H=105cmQk=0.4LPM,H=105cmQk=0.5LPM,H=105cmQk=0.2LPM,H=80cmQk=0.3LPM,H=80cmQk=0.4LPM,H=80cmQk=0.5LPM,H=80cm
0100200300400500600700800900
1000
0 0.2 0.4 0.6 0.8 1
Qw(LPM)
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2K
)
Qk=0.2LPM,H=105cmQk=0.3LPM,H=105cmQk=0.4LPM,H=105cmQk=0.5LPM,H=105cmQk=0.2LPM,H=80cmQk=0.3LPM,H=80cmQk=0.4LPM,H=80cmQk=0.5LPM,H=80cm
-
62
5.6 Effect of Phase Ratio
Fig 5.17 & 5.18 shows the variation of heat transfer
coefficient with variation in
kerosene-water phase ratio for column height 105 cm & 80 cm
and water bath
temperature 550C & 640C respectively at different water flow
rates. It was found that the
thermal efficiency increased as the phase ratio increased which
means that increase in the
kerosene mass flow rate is a result of increasing thermal
efficiency.
Fig 5.19 & 5.20 indicates the variation of heat transfer
coefficient with variation
in kerosene-water phase ratio for column height 105 cm & 80
cm varying water bath
temperature 550C & 640C respectively at different water flow
rate. It was found that the
overall heat transfer coefficient decreased as the phase ratio
increased.
Fig 5.21 & 5.22 shows change in kerosene outlet temperatures
with the change in
phase ratio for two different column heights varying the water
bath temperature. It was
found that with increasing phase ratio the kerosene outlet
temperature marginally varied.
But with increasing water inlet temperature it markedly
changed.
-
63
Fig 5.17: Effect on Thermal Efficiency with change in phase
ratio at a Column
Height 105cm
Fig 5.18: Effect on Thermal Efficiency with change in phase
ratio at a Column
Height 80cm
00.050.1
0.150.2
0.250.3
0.350.4
0.450.5
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase Ratio
Ther
mal
Effi
cien
cy
Temp=55CTemp=64C
0
0.05
0.10.15
0.2
0.25
0.30.35
0.4
0.45
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase Ratio
Ther
mal
Effi
cien
cy
Temp=55CTemp=64C
-
64
Fig 5.19: Effect on overall heat transfer coefficient with
change in phase ratio
at a Column Height 105cm
Fig 5.20: Effect on overall heat transfer coefficient with
change in phase ratio
at a Column Height 80cm
0
100200
300
400500
600
700800
900
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase ratio
Heat
Tra
nsfe
r Coe
ffici
ent(W
/m2 K
)
Temp=55CTemp=64C
0100200300400500600700800900
1000
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase Ratio
Heat
tran
sfer
coe
ffici
ent(W
/m2K
)
Temp=55CTemp=64C
-
65
Fig 5.21: Effect on Kerosene Outlet temperature with change in
phase ratio at
a Column Height 105cm
Fig 5.22: Effect on Kerosene Outlet temperature with change in
phase ratio at
a Column Height 80cm
0
10
20
30
40
50
60
70
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase Ratio
T ko(
0 C)
Temp=55 Ctemp=64C
0
10
20
30
40
50
60
70
0 0.2 0.4 0.6 0.8 1 1.2 1.4
Phase Ratio
T ko(0 C
) Temp=55CTemp=64C
-
66
Chapter 6 ConClusion
-
67
The performance of a Spray Column at two different column
heights of 105 cm & 80 cm
were studied for heat transfer in between Kerosene-Water. The
heat loss in the counter
flow Spray Column found, were not small enough to be negligible.
So, a term consisting
of heat loss was added to the governing equation for the
calculation of heat transfer
coefficient. The thermal efficiency of the 80 cm column height
varied in the range of 0.78
to 0.96 and found to be higher by maximum of 6 % than that of
105 cm column height.
So, it can be said that variation in column characteristics does
not affect thermal
efficiency. The value of overall heat transfer coefficient (h)
reported in the range of 200
W/m2K to 900 W/m2K. It increased as the water flow rate was
varied from 0.2 LPM to
0.5 LPM and decreased with increase in kerosene flow rate to 0.5
LPM. This could be
because as the water working here as a warm liquid so at higher
flow rate the amount of
heat flow in the column increases thus providing higher amount
of heat to be transferred.
It was also found that h increases markedly with increase in
water bath temperature &
decrease in column height.
The volumetric heat transfer coefficient reported in
mechanically agitated column at
similar operating conditions varied between 150 W/m2K to 600
W/m2K. Thus it can be
concluded that due to improved heat transfer coefficient along
with less heat loss, counter
flow Spray Column can be used as a replacement of mechanically
agitated column.
Further work can be performed by changing the column diameter,
increasing or
decreasing the nozzle diameter of the kerosene distributor or by
changing the no of holes
or nozzles in the kerosene distributor.
-
68
Nomenclature
mw= mass flow rate of water
mk= mass flow rate of kerosene
qw = volumetric flow rate of water
qk =volumetric flow rate of kerosene
Cpw= specific heat of water
w = Density of water
k= Density of Kerosene
C kw= Specific heat of Kerosene
dTw= Temperature change in water flow
ha= heat transfer coefficient
Two= Water outlet temperature
Tko= Kerosene outlet temperature
T