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Heat Transfer Measurement in a Three-Phase Spray Column Direct Contact Heat Exchanger for Utilisation in Energy Recovery from Low-Grade Sources Ali Sh. Baqir 1 , Hameed B. Mahood 2 , Mudher S. Hameed 2 and Alasdair N. Campbell 3 1 Al-Furat Al-Awsat Technical University, Al- Najaf Engineering Technical College, Department of Aeronautical Engineering, Al-Najaf, Iraq 2 University of Misan, Misan, Iraq 3 Department of Chemical and Process Engineering, University of Surrey, UK Abstract Energy recovery from low-grade energy resources requires an efficient thermal conversion system to be economically viable. The use of a liquid-liquid-vapour direct contact heat exchanger in such processes could be suitable due to their high thermal efficiency and low cost in comparison to a surface type heat exchanger. In this paper, the local volumetric heat transfer coefficient ( U v ) and the active height ( H v ) of a spray column three-phase direct contact heat exchanger (evaporator) have been 1 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22

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Page 1: [30 - epubs.surrey.ac.ukepubs.surrey.ac.uk/811635/1/CLEAN _NEW_ MANUSCRI…  · Web viewThe heat exchanger comprised a ... Population growth and the continuing deployment and development

Heat Transfer Measurement in a Three-Phase Spray Column Direct Contact Heat

Exchanger for Utilisation in Energy Recovery from Low-Grade Sources

Ali Sh. Baqir1, Hameed B. Mahood2 , Mudher S. Hameed2 and Alasdair N. Campbell3

1Al-Furat Al-Awsat Technical University, Al- Najaf Engineering Technical College, Department of

Aeronautical Engineering, Al-Najaf, Iraq

2 University of Misan, Misan, Iraq

3 Department of Chemical and Process Engineering, University of Surrey, UK

Abstract

Energy recovery from low-grade energy resources requires an efficient thermal conversion

system to be economically viable. The use of a liquid-liquid-vapour direct contact heat

exchanger in such processes could be suitable due to their high thermal efficiency and low

cost in comparison to a surface type heat exchanger.

In this paper, the local volumetric heat transfer coefficient (U v ) and the active height ( H v) of a

spray column three-phase direct contact heat exchanger (evaporator) have been investigated

experimentally. The heat exchanger comprised a cylindrical Perspex tube of 100 cm height

and 10 cm diameter. Liquid pentane at its saturation temperature and warm water at 45 ℃

were used as the dispersed phase and the continuous phase respectively. Three different

dispersed phase flow rates (10, 15 and 20 l/h) and four different continuous phase flow rates

(10, 20, 30 and 40 l/h) were used throughout the experiments. In addition, three different

sparger configurations (7, 19 and 36 nozzles) with two different nozzle diameters (1 and 1.25

mm) were tested. The results showed that the local volumetric heat transfer coefficient (U v )

along the column decreases with height. An increase in both the continuous and dispersed

phase flow rates had a positive effect on U v, while an increase in the number of nozzles in the

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sparger caused Uv to decrease. The active height was significantly affected by the dispersed

and continuous phase flow rates, the sparger configuration and the temperature driving force

in terms of the Jacob number.

Keywords: spray column three-phase direct contact heat exchanger, local volumetric heat

transfer coefficient, active height, sparger configuration.

1. Introduction

Population growth and the continuing deployment and development of technology around the

word require augmentation of energy supplies. Currently, fossil fuels provide about 80% of

the gross energy needed. Only 11% of the total energy required is generated from renewable

energy resources [1]. Therefore, many environmental problems, such as air pollution and

global warming may continue to accelerate. Such problems necessitate novel solutions.

Accordingly, heat recovery processes, especially those that exploit industrial and interfacial

low-grade energy resources, have received an increasing amount of attention. There are,

however, many obstacles still hindering the development of these processes. In particular, the

low thermal efficiency of the equipment used, and specifically the heat exchanger, must be

overcome. The high capital cost of the heat exchanger can also significantly affect the

feasibility of the heat recovery plant. The low heat exchanger efficiency is principally due to

the presence of metallic barriers that separate the hot and cold fluid streams. These surfaces

impose an additional, potentially large, heat transfer resistance and are prone to corrosion and

fouling. Consequently, the heat transfer efficiency of the heat exchanger will reduce with

time.

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These problems could be mitigated by using direct contact heat exchangers. The absence of

the internal separating wall between the fluid streams in the direct contact heat exchanger

results in many advantages over the traditional surface type heat exchanger. For example, the

direct contact device can be operated with a very low temperature difference between the

working fluids, even as low as∆ T=1℃. The fouling and corrosion problems are all but

eliminated, as there is no heat transfer surface, and there is an increase in the heat transfer

rate between the fluids. Finally, the direct contact exchanger has a low capital and operational

cost as it can be constructed from very cheap materials [2]. In this context, Wright [3] found

that the replacement of a surface type heat exchanger that was used in a 5 MW power plant

by a direct contact heat exchanger could reduce the capital cost of the plant by 25%. For these

reasons, the direct contact heat exchanger, especially the three-phase direct contact heat

exchanger, has received considerable attention in many recent experimental and theoretical

investigations. These investigations were presented within the context many different

industrial processes, such as water desalination, power generation from geothermal energy

and heat recovery from low-grade energy resources [4, 5].

It has been shown previously [6,7] that the heat transfer characteristics of the spray column

heat exchanger can be represented clearly by the volumetric heat transfer coefficient. Despite

this, only a limited number of studies have actually reported the volumetric heat transfer

coefficient. Bauerle and Ahlert [8] observed an increase in the volumetric heat transfer

coefficient of the spray column heat exchanger with dispersed phase hold-up until the

flooding limit of the exchanger was reached. There was a subsequent decline in heat transfer

coefficient. The same trend in the volumetric heat transfer coefficient in a spray column heat

exchanger was noted by Plass et al. [9]. Their results were correlated and accurately fitted

with the data over a range of hold-ups. The effect of the initial diameter of the dispersed

phase droplets can significantly affect the volumetric heat transfer coefficient in the spray

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column direct contact heat exchanger, by affecting the interfacial heat transfer area. Sideman

et al. [10] ascertained that there is a decrease in the volumetric heat transfer coefficient of the

spray column heat exchanger with an increase in the initial drop diameter. This observation

was confirmed numerically by Cabon and Boehm [11] and Jacobs and Golafshani [12].

There are few analytical models for the volumetric heat transfer coefficient available in the

literature. Only that of Mori [7] is prominent. The difficulty in deriving and solving analytical

models is because of the complexity that arises due to the large number of interacting

parameters that control the heat transfer in the spray column. However, Mori [7] was able to

exploit the expression for the heat transfer coefficient for single drop evaporating in an

immiscible liquid [13] as a starting point for his analytical solution. He succeeded in finding

both the local and the average volumetric heat transfer coefficient of the spray column direct

contact heat exchanger.

In contrast to the few studies that have investigated the volumetric heat transfer coefficient,

much research has been directed toward the temperature distribution along the spray column

direct contact heat exchanger, both experimentally and theoretically [14-20]. All of these

studies have confirmed that the exit temperature of the dispersed phase increased with

exchanger height, while it decreases in the case of the continuous phase. Interestingly, and

surprisingly, Siqueiros and Bonilla [21] observed that when the initial temperature (inlet

temperature) of the continuous phase (water) ranged between 75-88 ℃ and the inlet

temperature of the dispersed phase (pentane) between 23-38 ℃, the continuous phase outlet

temperature was between 70-84 ℃ and the dispersed phase outlet temperature between 72-85

℃. Although, no other study has confirmed these results, they are in accord with the

expectation that latent heat controls the direct contact heat exchange process. Recently,

Mahood et al. [22] studied analytically the distribution of the temperature of both the

dispersed and continuous phases along a spray column direct contact condenser. The

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temperature of the dispersed phase was shown to increase with exchanger height and with

decreasing drop size. Wang et al. [23] found that the volumetric heat transfer calculated in

respect to the dispersed-continuous phase temperature interface was significantly greater than

that calculated based on the average dispersed phase-continuous phase bulk temperature

difference. Recently, Jiang et al. [24] noted that the size of a spray column direct contact heat

exchanger could be considerably reduced when using packed materials, as the volumetric

heat transfer coefficient was significantly increased. Mahood et al. [1, 4, 25-31] investigated

the heat transfer characteristics of a bubble type three-phase direct contact condenser.

Different effective parameters, such as the mass flow rates of the dispersed and continuous

phases, and the initial temperature of the dispersed phase on the transient [4] and steady state

temperature distributions along the condenser [25], the transient [26] and steady volumetric

heat transfer coefficient [27], the condenser efficiency and ultimately cost were studied [1].

In addition, the conditions under which the direct contact condenser flooded and its heat

transfer performance under these conditions were determined [28]. Furthermore, the

feasibility of implementing the three-phase direct contact heat exchanger in the applications

of water desalination and power generation was investigated [29, 30]. Finally, a new model

for the drag coefficient exerted on the bubbles as they move through a real three-phase

exchanger was developed [31]. More recently Baqir et al. [32] measured the average

volumetric transfer coefficient and the dispersed phase holdup in a liquid-liquid-vapour heat

exchanger. The effect of the initial drop size, the heat exchanger active height, and the

sparager configuration on the average volumetric heat transfer coefficient was tested. They

observed that average volumetric heat transfer coefficient was significantly affected by the

change in the drop size, the holdup ratio and the heat exchanger active height. On the other

hand, the sparger configuration had a very slight impact.

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In the present study, measurements of the local volumetric heat transfer coefficient along and

the active height of the three-phase direct contact evaporator were carried out. The effect of

the continuous phase flow rate, the dispersed phase flow rate, the sparger configuration and

the diameter of the injection nozzles on the volumetric heat transfer coefficient and the active

height were examined.

2. Experimental work

2.1 Experimental setup

In Figure (1) is shown a schematic diagram of the experimental rig that was used in the

present work. The apparatus is comprised of the direct contact column (test section),

dispersed phase supply system, continuous phase supply system, measuring devices and

auxiliary equipment, such as the data logger and thermocouples. The direct contact column

(test section) consists of a 100 cm long cylindrical Perspex tube with a 10 cm diameter. Six

equidistant holes along the test section were made to fix six calibrated K-type thermocouples

(average error ± 1℃). A circular shaped sparger with an outer diameter of 49 cm is fixed at

the bottom of the column. Three different sparger configurations (7 nozzles, 19 nozzles and

36 nozzles), with two different nozzle diameters were used during the experiments. In Figure

(2) is presented a schematic diagram of the sparger configurations. The test section is

connected to the dispersed and continuous phase supplies via inlet tubes from its bottom and

top respectively. The dispersed phase supply unit comprises a 20 l plastic storage tank,

peristaltic pump, pipes, fittings and valves. Liquid pentane (99% purity) was used as the

dispersed phase. Table (1) shows the properties of pentane at 1 bar and saturation

temperature.

The continuous phase system supply is made up of a 500 l constant temperature water bath

with a temperature controller, water pump, pipes, fittings and valves. The water bath is heated

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by three electric heaters (3 kW each). The pressure in the water bath is controlled by a safety

relief valve (1.5 bar operating pressure). Distilled water was used as the continuous phase. It

was heated using a 10 mm outer diameter 2.5 m long copper coil which was completely

immersed in the constant temperature water bath. The flow rate of both the dispersed phase

and the continuous phase were measured before entering the test section using suitable

rotameters with an error of ± 1.25 % .

Nine calibrated K-type thermocouples were used to measure the temperature distribution of

the continuous phase along the test section and the inlet and outlet dispersed phase

temperature. These thermocouples were connected to a 64 channel Data Logger (Delta-T

Devices Ltd) and PC. A surface-type condenser was used to condense the dispersed phase

vapour produced at the top of the test section during the experiments.

2.2 Experimental procedure

Once the continuous phase reached the temperature desired for the experimental run, it was

circulated throughout the test section to maintain a constant temperature. The active height of

the continuous phase was selected, and the temperature and the flow rate were measured. The

dispersed phase (n-pentane liquid) at its saturation temperature was then injected in to the test

section via a sparger, at a specified flow rate. Pentane drops were formed at the sparger and

then subsequently detached and rose up along the test section of the column. There was

therefore counter-current contact between the dispersed phase moving up the column and the

continuous phase moving down. Accordingly, the cold dispersed phase drops absorbed heat

from the hot continuous phase and evaporated as they rose. Two-phase bubbles (liquid-

vapour) formed (see Fig. 3) when the dispersed phase drops first come into direct contact

with the continuous phase [33-37]. These bubbles consist of liquid n-pentane, which is

immiscible with the aqueous continuous phase and the n-pentane vapour produced by

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evaporation. The two-phase bubbles existed along the majority of the column’s height, and

only become 100% vapour when they reached the end of the active height. The active height

is the maximum section of the column over which the phase change of the dispersed phase

drops occurred. After the pentane was evaporated, there remained a driving force for heat

transfer to the bubbles, and so the vapour collected at the top of the column was in fact

slightly superheated. As a consequence of the direct contact heat exchange, the continuous

phase cools down while it moves down from the top of the column to the bottom. To perform

the process as efficiently as possible the continuous phase should be drained out with

minimum energy content. The continuous phase temperature profile was measured using the

thermocouples and directly displayed on a PC via the data logger. The dispersed temperature

was measured at only two points: the inlet and outlet. The vapour produced at the top of the

column was condensed using a surface-type condenser and sent back to the dispersed phase

storage tank to use again in another run. The conditions of the experiments are shown in

table (2).

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Table 1 The physical properties of n-pentane at its saturation temperature at 1 bar

Property Values

Saturation temperature (° C) 36.0

Molar mass (kg /kmol) 72.15

Thermal diffusivity (m2/s) 7.953×10−8

Specific heat of liquid (kJ /kg K ) 2.363

Specific heat of vapour (kJ /kg K ) 1.66

Thermal conductivity of liquid (W /m K ) 0.1136

Thermal conductivity of vapour(W /m K ) 0.015

Kinematic viscosity (m2/s ) 2.87×10−7

Viscosity ( Pa s ) 1.735×10−4

Latent heat of vaporisation (kJ /kg ) 359.1

Density of liquid (kg /m3 ) 621

Density of vapour (kg /m3 ) 2.89

Surface tension ( N /m ) 0.01432

Table 2 Conditions of experimental operations

Temperature of the continuous phase (water)

inlet

Temperature of the dispersed

phase (n-pentane) inlet

Pressure at the top of test

section

Volumetric flow rate of the continuous

(water) phase

Volumetric flow rate of the

dispersed (n-pentane) phase

45 ℃ ± 1% 36 ±0.5 % 1 atm. 10-40 l/hr± 1.5 % 10-20 l/hr ± 1.5 %

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10

Fig. 1. Schematic diagram of the experimental rig.

Water drain

Constant temperature

water bath

Valve Valve

Valve

Rotameter

Pentane liquid (condensate)

Two-phase bubbles

Water level

Water out

Water in

Condenser

Pump

Valve

Water tank

Pump

D

ir

ec

t

C

o

nt

ac

t

E

Pentane tank

PC

Data logger

Thermocouples

Rotameter

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Fig. 2. Sparger configurations used in the present work. Specifically, spargers with a) 7

nozzles, b) 19 nozzles and c) 36 nozzles, were used.

Fig. 3. Configuration of a two-phase bubble evaporating in an immiscible liquid (a represents

the two-phase bubble radius, U denotes the continuous phase velocity, V r and V θ are the

radial and tangential velocity components, θ is the angle in spherical coordinate).

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mm mm mm

mm

(c)(b)(a)

U

a

θ

β

Vapour

Non-evaporated Liquid pentane

V θ

V r

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3. Results and discussion

The local volumetric heat transfer coefficient along a three-phase spray column direct contact

evaporator was studied experimentally. The calculation of the volumetric heat transfer

coefficient was based on an energy balance, whilst assuming that latent heat dominated over

sensible throughout the process. It was further assumed that there were no heat losses to the

environment and that the flow rates of both the continuous and dispersed phases were

constant. This is because of using a thick Perspex tube as a spray column, which is a poor

conductor of heat, is likely to minimise the heat losses over the short duration of the

experiments.

The local volumetric heat transfer coefficient can be found by:

U vi=qi

A ∆ Z i (∆ T lm )i (1)

where ( ∆T lm )i , q i, A and ∆ Z i denote the log-mean temperature difference for each sub-

volume, the total heat transfer rate for each sub-volume, the direct contact condenser cross-

sectional area and the height of a sub-volume, respectively.

The energy balance can be written as:

q i=mc C pc (T co−T ci ) i=mdih fg (2)

where , mc , is the mass flow rate of the continuous phase, C pc is the specific heat capacity of

the continuous phase, T co and T ci are the temperatures of the continuous phase as it leaves the

and enters the sub-volume, mdi is the rate at which the dispersed phase evaporates in the sub-

volume and hfg is the latent heat of vaporisation. The temperature difference between the

contacting phases inevitably varies nonlinearly along the length of the column due to the

effects of the nonlinear drop size distribution and back-mixing. This back-mixing is the main

problem that hinders the direct contact heat exchanger. The use of the log-mean temperature

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difference accounts for these effects. For counter-current flow with latent heat dominating,

the log-mean temperature difference is:

∆ T lm=(T ci−T co )

ln( T ci−T d

T co−T d ) (3)

Combining Eqs. (1-3) results in the local volumetric heat transfer coefficient:

U vi=mc C pc

A . ∆ Z iln [ (T co−T d )i+( mdi

mc ) hfg

C pc

(T co−T d )i ] (4)

where T d denotes the temperature of the dispersed phase at each individual sub-volume (i.e.

the saturation temperature).

It is well-known [6,7, 10, 19] that heat transfer in the direct contact device is dominated by

transfer across the liquid-liquid interface. As the dispersed phase moves up the column, more

vapour is produced within the two-phase bubble as a result of evaporation. Consequently, the

liquid-liquid interface becomes smaller and the amount of energy that can be absorbed by the

bubble as latent heat becomes lower. Therefore, the liquid fraction of the dispersed phase has

to be specified along the column. By using the energy balance, the local non evaporated

dispersed phase mass flow rate can be found using Eq. (2) above:

The evaporator height has been divided into six equally sized sub-volumes. From Eq. (4)

above, only the outlet temperature of the continuous phase of each sub-volume and the mass

flow rate of both phases are important to calculate the local volumetric heat transfer

coefficient. Accordingly, the local temperature along the column height has been measured

using thermocouples. The temperature of the dispersed phase was as assumed to be its

saturation temperature.

3.1 Local volumetric heat transfer coefficient

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The variation of the local volumetric heat transfer coefficient for three different sparger

configurations and four different continuous phase flow rates is shown in Figs. (4 & 5). It is

clear from the figures that the local volumetric heat transfer coefficient decreases

monotonically upon moving up the exchanger. This is because of the decrease in the

temperature driving force as the evaporating drops move upward, and the reduction of

dispersed phase liquid to act as a heat sink. The decrease in the liquid content within the drops

(i.e. the non-evaporated dispersed phase) as a result of evaporation also results in a reduction

in the liquid-liquid interface. Thus, the internal heat transfer resistance in the drops increases

because of the poor thermal conductivity of the vapour. Consequently, the local heat exchange

and the local volumetric heat transfer coefficient are reduced.

The impact of the continuous phase flow rate on the local volumetric heat transfer coefficient

is clearly demonstrated in Figs. (4 &5). As expected, a higher continuous phase mass flow

rate results in a higher volumetric heat transfer coefficient over the entire height of the

exchanger. The continuous phase is the only the energy source that is responsible for the

evaporation of the dispersed phase drops. A higher continuous phase flow rate means that

there is sufficient energy which can be transferred to the dispersed phase drops and therefore

the heat transfer coefficient of the process is increased, whilst the temperature difference

between the contacting phases is maintained. It is also interesting to note that the effect of

increasing the continuous phase flow rate on the volumetric heat transfer coefficient is

lessened somewhat at higher flow rates. This effect is most evident at the lowest dispersed

phase flow rate (10 l/h) in figures 4 and 5, but can be seen at the higher flow rates too. These

observations would indicate that there are diminishing returns on increases in the continuous

phase flow rate, with the optimum value depending on the dispersed phase flow rate. This is

an important point to note when considering the most economic mode of operation for the

exchanger.

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The dispersed phase flow rate exhibits a similar effect on the volumetric heat transfer

coefficient. This is more obvious at the bottom of the column as shown by Table (3) (Z =5 cm

at the bottom and Z=65 cm at the top). This could be explained by the fact that at the bottom

of the column, significant convective direct contact heat transfer between the two phases

occurs. The heat exchange is slower higher up the exchanger due to the high internal heat

transfer resistance that exists in the drop, which in turn reduces the impact of the dispersed

phase flow rate. This is consistent with observations by Sideman and Taitel [38] for a single

pentane drop evaporating in direct contact with hot water. They observed that a substantial

proportion of a drop evaporated over only a short distance from the injection point.

Fig. 4. Variation of the local volumetric heat transfer coefficient along the exchanger height

for four different continuous phase mass flow rates and three dispersed phase flow rates for a

sparger with 7 nozzles

15

nz=7Qd=20 L/h

nz=7Qd=15 L/h

nz=7Qd=10 L/h

0 0.1 0.2 0.3 0.4 0.5 0.6 0.710

20

30

40

50

60Qc(L/h)= 40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7102030405060708090

Qc(L/h)= 40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.710

20

30

40

50

60

70Qc(L/h)= 40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

Qd=20 l /h

Qd=15 l /h

nz=7

nz=7

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The effect of the flow rates of the two phases on the average volumetric heat transfer

coefficient can be clarified by considering the flow rate ratio as shown by Fig. (6) for two

different sparger configurations. It is obvious from the figure that the volumetric heat transfer

coefficient increases with increasing the flow rate ratio. This behaviour could be attributed to

the fact that the increase in the mass flow rate ratio means an increase in the heating medium

in the heat exchanger. Consequently, the heat transfer rate will rise due to the high energy

content available.

It is also evident that the rate of increase of heat transfer coefficient with the flow rate ratio

does decrease as the ratio increases. This is most likely because as the rate of the continuous

phase is increased relative to the dispersed phase, the change in temperature of the continuous

phase is smaller, hence there is less of a reduction in driving force for heat transfer. It is

unclear whether an optimum value is approached asymptotically, or a true maximum is

evident within the range of the flow rate ratios used.

The uncertainty in estimates of the volumetric heat transfer coefficient was calculated using

the method suggested by Coleman and Steele [39]. The results indicate that the uncertainty

strongly depends on the error in the continuous mass flow rate rather than the other

parameters, such as dispersed phase mass flow rate and log-mean temperature difference.

However, the maximum uncertainty was found about ± 3% .

16

322

323

324

325

326

327

328

329

330

331

332

333

334

335

336

337

338

339

340

341

342

343

344

345

346

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Fig. 5. Variation of the local volumetric heat transfer coefficient along the exchanger height

for four different continuous phase flow rates and three dispersed phase flow rates for a

sparger with 19 nozzles

(a) (b)

17

nz=19Qd=20 L/h

nz=19Qd=15 L/h

nz=19Qd=10 L/h

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7102030405060708090

Qc(L/h)=40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.710

20

30

40

50

60

70Qc(L/h)=40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7101520253035404550

Qc(L/h)=40 30 20 10

Z (m)

Uv

(kW

/m3.

oC)

nz=19Qd=20 l /h

nz=19Qd=15 l /h

nz=19Qd=10 l /h

nz=19nz=7

0 0.5 1 1.5 2 2.5 3 3.5 4 4.50

10

20

30

40

50

60

70Qd (L/h)=10 15 20

Flow Rate Ratio (-)

Uv

(kW

/m3.

oC)

0 0.5 1 1.5 2 2.5 3 3.5 4 4.50

10

20

30

40

50

60

70Qd (L/h)= 10 15 20

Flow Rate Ratio (-)

Uv

(kW

/m3.

oC)

347

348

349

350

351

352

353

354

355

356

357

358

359

360

361

362

363

364

365

366

367

368

369

370

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Fig. 6. Variation of the average volumetric heat transfer coefficient with flow ratio of the

continuous phase and dispersed phase for two different sparger configurations a) 7 nozzles

and b) 19 nozzles

Table 3 The effect of the dispersed phase flow rate on the local volumetric heat coefficient at

a point close to the injection point (Z = 5 cm) and near the top of the column (Z = 65 cm).

Values for three different sparger configurations are shown

Z

(cm)Qc (L /h )

nz 7 19 36

Qd ( L/h ) U v U v U v

5

65

40

40

10

15

20

10

15

20

51.47

69.42

84.82

26.96

35.83

42.82

50.2

63.2

2

82.3

26.8

34.5

2

42.4

45.73

60.69

78.43

26.59

34.27

42.13

The effect of the sparger configuration on the local volumetric transfer coefficient of the

exchanger for three different dispersed phase flow rates was studied and the pertinent results

are presented in Fig. (7). The local volumetric heat transfer coefficient does show a slight

decrease when the number of nozzles in the sparger is increased. This is especially apparent

near the bottom of the column. Towards the top of the column the differences between the

18

371

372

373

374

375

376

377

378

379

380

381

382

383

384

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heat transfer coefficient for different nozzle numbers effectively vanishes. This can be

explained by the fact that at the same dispersed phase flow rate and nozzle diameter, the

dispersed phase injection velocity is increased when there are fewer nozzles in the sparger.

Consequently, a smaller two-phase bubble is formed at the sparger because the drop/bubble

formation time is shortened, and the velocity relative to the continuous phase is increased.

Therefore, the convective heat exchange between the two phases is increased. Towards the

top of the column the motion of the bubbles is dominated by buoyancy forces and so the

effect of the injection velocity on the heat transfer is substantially lessened. What these results

clearly show is that the injection velocity and hence bubble formation significantly affects the

heat transfer in the three-phase direct contact heat exchanger. This is in accord with that has

been found by Mahood [40]. He recommended that the two-phase bubble velocity is the most

important factor that must be incorporated directly or indirectly in any quantitative description

of heat transfer in a three-phase direct contact exchanger.

Fig. (7) also clearly shows a significant increase in the local volumetric heat transfer

coefficient when the dispersed phase flow rate is increased. As mentioned above, the higher

dispersed phase flow rate can enhance the heat transfer process due to the increased interfacial

area and the higher relative velocities of the phases.

0 0.1 0.2 0.3 0.4 0.5 0.6 0.720

30

40

50

60

70

80

90

Qd(L/h)=10 & nz= 7, Reo=1760Qd(L/h)=10 & nz= 19, Reo=649Qd(L/h)=10 & nz= 36, Reo=342Qd(L/h)=15 & nz= 7, Reo=2640Qd(L/h)=15 & nz= 19, Reo=973Qd(L/h)=15 & nz= 36, Reo=514Qd(L/h)=20 & nz= 7, Reo=3520Qd(L/h)=20 & nz= 19, Reo=1300Qd(L/h)=20 & nz= 36, Reo=685

Z (m)

Uv (k

W/m

3.K)

19

Qc=40l /h

385

386

387

388

389

390

391

392

393

394

395

396

397

398

399

400

401

402

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Fig. 7. The effect of sparger configuration on the local volumetric heat transfer coefficient.

The variation of the heat transfer coefficient with height in the column is shown for three

different dispersed phase flow rates and for spargers with 7, 19 or 36 nozzles.

In addition to the number of nozzles in the sparger affecting the performance, it is likely that

the diameter of the nozzles will also have an effect. In Fig. (8) is presented a comparison of

the local volumetric heat transfer coefficient along the direct contact exchanger for two

different nozzle diameters and so two different nozzle Reynolds numbers. It is once again

evident that regardless of the dispersed and continuous phase flow rates, the local volumetric

heat transfer coefficient decreases slightly when the nozzle Reo (nozzle diameter) is decreased

from 1760 to 1410), which corresponding to the change in the nozzle diameter from 1 mm to

1.25 mm. In fact, the increase in the nozzle Reo results in an increase in the dispersed phase

drops injection velocity, which enhances the volumetric heat transfer coefficient [17]. This

could be due to the improved mixing caused by the faster moving drops as well as the

reduction in thickness of the boundary layer surrounding the drops. At the same time, the

increase in the diameter of the nozzles significantly influenced the drop size, which affected

the interfacial heat transfer area. The larger nozzle diameter, the larger the drop size, and

hence the lower the heat transfer area [32]. This results in a low heat transfer rate.

20

403

404

405

406

407

408

409

410

411

412

413

414

415

416

417

418

419

420

421

422

423

424

425

426

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0 0.1 0.2 0.3 0.4 0.5 0.6 0.70

10

20

30

40

50

60

Qc(L/h)=40, Dnz=1 mm, Reo=1760

Qc(L/h)=40, Dnz=1.25 mm, Reo=1410

Qc(L/h)=30, Dnz=1 mm, Reo=1760

Qc(L/h)=30, Dnz=1.25 mm, Reo=1410

Qc(L/h)=10, Dnz=1 mm, Reo=1760

Qc(L/h)=10, Dnz=1.25 mm, Reo=1410

Z (m)

Uv (k

W/m

3.K)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.70

10

20

30

40

50

60

Qc(L/h)=40, Dnz= 1 mm, Reo=649

Qc(L/h)=40, Dnz=1.25 mm, Reo=519

Qc(L/h)=30, Dnz=1mm, Reo=649

Qc(L/h)=30, Dnz=1.25 mm, Reo=519

Qc(L/h)=10, Dnz=1 mm, Reo=649

Qc(L/h)=10, Dnz=1.25 mm, Reo=519

Z (m)

Uv (k

W/m

3.K)

Fig. 8. The effect of the diameter of the nozzles in the sparger on the local volumetric heat

transfer coefficient along the exchanger height for three different continuous phase flow rates

Figure (9) shows the effect of the continuous phase temperature in terms of Jacob number

(Ja) on the average volumetric heat transfer coefficient of the heat exchanger, for three

different sparger configurations and dispersed phase flow rates. The continuous phase Ja was

calculated as:

21

Qd=10 L/h∧nz=7

Qd=10 L/h∧nz=19

427

428

429

430

431

432

433

434

435

436

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Ja=ρc C pc (T c−T d )

ρv h fg (6)

In general, the average volumetric heat transfer coefficient was found to increase with Ja.

The temperature difference, in fact, represents the main driving force that drives the direct

contact heat transfer process. Accordingly, increasing the driving force (∆ T ) increases the

heat exchange between the two phases and of course increases the volumetric heat transfer

coefficient, which enhances the performance of the heat exchanger. Similar to above

findings, the increase in the dispersed phase flow rate results in an increase in the average

volumetric heat transfer coefficient. Again, the increase of number of nozzles in the sparger

results in a reduction in the average volumetric heat transfer coefficient.

10 15 20 25 30 3515

20

25

30

35

40

45

50

55

60Qd(L/h)=10, nz= 7, Reo=1760Qd(L/h)=15, nz= 7, Reo=2640Qd(L/h)=20, nz= 7, Reo=3520Qd(L/h)=10, nz=19, Reo=649Qd(L/h)=15, nz= 19, Reo=973Qd(L/h)=20, nz= 19, Reo=1300Qd(L/h)=10, nz= 36, Reo=342Qd(L/h)=15, nz= 36, Reo=514Qd(L/h)=20, nz= 36, Reo=685

Jac (-)

Uvav

(kW

/m3.

K)

Fig. 9. effect of the continuous phase Jacobs number on the average heat transfer coefficient

for three different dispersed phase flow rate and three different nozzle configurations

3.2 Heat Exchanger Active height

22

437

438

439

440

441

442

443

444

445

446

447

448

449

450

451

452

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The active height can be simply defined as the minimum height of the continuous phase in

the column that can lead to a complete evaporation of the dispersed phase drops. Therefore, it

directly affects the cost of the heat exchanger by influencing its volume. Also, the hydrostatic

pressure variation would be increased with an increase of the active height, which would

result in a reduction in the mixing rate [41]. Figure (10) shows the variation of the heat

exchanger active height with the continuous flow rate at three different dispersed phase flow

rates. For a constant dispersed phase flow rate and sparger configuration, the active height

was found to decrease with the continuous flow rate. This could be explained by the fact that

at the higher continuous phase flow rate, the amount of energy available in the heat

exchanger is adequate to completely evaporate the dispersed drops over a very short distance

from the injection point. On the other hand, at a constant continuous phase flow rate the

active height was significantly affected by an increase in the dispersed phase flow. The

higher the dispersed phase flow rate, the higher the heat exchanger active height. This is

because the increase flow of the dispersed phase requires a larger volume of the continuous

phase for complete evaporation of the drops.

23

453

454

455

456

457

458

459

460

461

462

463

464

465

466

467

468

469

470

471

472

473

474

475

476

477

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Fig. 10. The variation of active height with the continuous flow rate for different dispersed

flow rates and sparger configurations

The sparger configuration was found to have a significant effect on the active height of the

heat exchanger. As shown by Fig. (11) the active height was significantly increased by

increasing the number of nozzles in the sparger. As mentioned above, this could be as a result

of the slower heat transfer between the drops and the hot water.

24

0 5 10 15 20 25 30 35 40 450.14

0.145

0.15

0.155

0.16

0.165

0.17

0.175

Qd(L/h)= 20 15 10

Qc (L/h)

Hv

(m)

5 10 15 20 25 30 35 40 450.135

0.140.145

0.150.155

0.160.165

0.170.175

0.18

Qd(L/h)= 20 15 10

Qc (L/h)

Hv

(m)

5 10 15 20 25 30 35 40 450.155

0.160.165

0.170.175

0.180.185

0.190.195

0.2

Qc(L/h)= 20 15 10

Qc (L/h)

Hv

(m)

nz=7 nz=19

nz=36

478

479

480

481

482

483

484

485

486

487

488

489

490

491

492

493

494

495

496

497

498

499

500

501

502

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Fig. 11. The variation of the active height with the continuous flow rate for different

dispersed flow rates and sparger configurations

Finally, the effect of the temperature driving force, as characterised by the Jacob number

(Ja), on the active height was studied and is shown in Fig. (12), for three different dispersed

phase flow rates. The dependency of the active height on Ja was similar to that already found

for the case of the effect of the continuous phase flow rate on the active height, (Fig. (10)). It

is obvious that the energy content of the continuous phase increases with its flow rate.

Therefore, the temperature driving force is increased accordingly. The amount of energy

available in the continuous phase still high whatever how much the dispersed phase absorbed.

Also, it is clear from the figure, that the active height is significantly affected by the dispersed

phase flow rate. The higher the dispersed phase flow rate, the higher the active height. This is

as expected, where the higher dispersed phase flow rate needs more energy for complete

evaporation.

25

Qd=20 L/hQd=10 L/h

5 10 15 20 25 30 35 400.14

0.15

0.16

0.17

0.18

Qc(L/h)=10 30 40

nz (-)

Hv

(m)

5 10 15 20 25 30 35 400.15

0.16

0.17

0.18

0.19

0.2

Qc(L/h)=10 30 40

nz (-)

Hv

(m)

503

504

505

506

507

508

509

510

511

512

513

514

515

516

517

518

519

520

521

522

523

524

525

526

527

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Fig. 12. variation of active height with the continuous phase Jacob number for different

dispersed and three different sparger configurations

4. Conclusions

In the present study, the local volumetric heat transfer coefficient and the active height of a

spray column direct contact heat exchanger were measured. The experimental study was

performed under various operating conditions; specifically, the continuous phase flow rate,

dispersed phase flow rate, sparger configuration and temperature difference between the

26

15 17 19 21 23 25 27 290.14

0.1420.1440.1460.148

0.150.1520.1540.1560.158

Qd(L/h)= 20 15 10

Jac (-)

Hv

(m)

15 17 19 21 23 25 27 29 31 33 350.135

0.140.145

0.150.155

0.160.165

0.170.175

0.18

Qd(L/h)= 20 15 10

Jac (-)H

v (m

)

15 17 19 21 23 25 27 29 31 33 350.155

0.160.165

0.170.175

0.180.185

0.190.195

0.2

Qd(L/h)=20 15 10

Jac (-)

Hv

(m)

nz=7

nz=19

nz=36

528

529

530

531

532

533

534

535

536

537

538

539

540

541

542

543

544

545

546

547

548

549

550

551

552

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contacting fluids were all varied. With these data, the performance of the spray column direct

contact heat exchanger under the influence of various operational conditions was obtained.

The results show that the flow rate of the dispersed phase has more pronounced effect on U v

than that of the continuous phase and both phases flow rates have positively influenced U v.

The influence of both phases, however, becomes more obvious at high flow rates of the two

phases. The maximum average U v was 59.05 kW /m3 K at continuous and dispersed phase

flow rates of40 L/h and 20 L/h, respectively. The number of nozzles in the sparger has no

significant impact on the average U v. The U v was 59.05, 58.0 & 56.5 kW /m3 K for nz =7, 19

& 36 respectively, with the same above flow rates of the continuous and dispersed phases.

The local volumetric heat transfer coefficient was inversely affected by increasing the

diameter of the injecting nozzle and number of nozzles in the sparger. In both cases this

resulted in a reduction in Re for the injection of the dispersed phase. The lower relative

velocity of the injection leads to a lower rate of convective heat transfer, as one would expect

intuitively. The temperature driving force in term of Ja had a significant positive impact on

the volumetric heat transfer coefficient. This impact was significant at a high dispersed phase

flow rate, where U v varied almost linearly with Ja and the maximum average U v nearly

doubled It was changed from 27.78 to 59.06 kW /m3 K , 27.337 to 58.0 kW /m3 Kand 26.3 to

56.6 kW /m3 K , when Qd=20 L/h and for nz = 7, 19 & 36, respectively..

Furthermore, the results indicated that the active height of heat exchanger was significantly

affected by the flow rate of both phases. The higher the continuous or dispersed phase, the

lower the active height of the exchanger. for a similar effect was observed for the temperature

driving force, while the number of injecting nozzle had the opposite effect.

In summary, with the absence of adequate data or theoretical results, the present experimental

results could be helpful in the design of spray column direct contact heat exchangers. These

data could help to improve the operational method in order to produce an efficient and low

27

553

554

555

556

557

558

559

560

561

562

563

564

565

566

567

568

569

570

571

572

573

574

575

576

577

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cost spray column direct contact heat exchanger for utilising in energy recovery from low-

grade resources.

Nomenclatures

A cross-sectional area of column, m2

C pc specific heat of continuous phase, kJ /kg . K

Jac Jacobs number

h fg latent heat of condensation, kJ /kg

H v active height of heat exchanger, m

md dispersed phase mass flow rate, kg /min

mc continuous phase mass flow rate, kg /min

nz number of nozzle in the sparagr

q heat transfer rate, kW

Qc volumetric flow rate of the continuous phase, L/h

Qd volumetric flow rate of the dispersed phase, L/h

ℜo nozzles’ Reyonlds number

T c temperature of the continuous pahse, ℃

T d temperature of the dispersed phase, ℃

∆ T lm log-mean temperature difference, ℃

U relative velocity, m /s

U v volumetric heat transfer coefficient, kW /m3 K

V r radial velocity component, rad

V θ tangential velocity component, rad

Z axial position, m

∆ Z sub-height along column, m

28

578

579

580

581

582

583

584

585

586

587

588

589

590

591

592

593

594

595

596

597

598

599

600

601

602

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Greek symbols

ρc density of continuous phase, kg /m3

ρ v density of dispersed phase vapour, kg /m3

θ angle, rad

Subscripts

c continuous phase

d dispersed phase

i initial, or location

o outlet

References:

[1] H.B. Mahood, A.N. Campbell, R.B. Thorpe, A.O. Sharif, Heat transfer efficiency and

capital cost evaluation of a three-phase direct contact heat exchanger for the utilisation of

low-grade energy sources, Energy Conv. Mang. 106(2015) 101-109.

[2] A. Sh. Baqir, Theoretical and experimental study of direct-contact evaporation of a

volatile drops(n-pentane) in an immiscible liquid (distilled water), PhD Thesis, Dep.

Mechanical Engineering, University of Basrah, Iraq, (2010).

[3] J.D. Wright, J. D., Selection of a working fluid for an organic Rankine cycle coupled to a

salt-gradient solar pond by direct-contact heat exchange. Journal of Solar Energy

Engineering, 104(4) (1982) 286-292.

[4] H.B. Mahood, R.B. Thorpe, A.N. Campbell , A.O. Sharif, Experimental measurements

and theoretical prediction for the transient characteristic of a three-phase direct contact

Condenser, Appl. Them. Eng. 87(2015) 161-174.

[5] G.F. Hewitt, G.L. Shires, R.T. Bott, Process heat transfer, CRC Press Inc, 1993.

29

603

604

605

606

607

608

609

610

611

612

613

614

615

616

617

618

619

620

621

622

623

624

625

626

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[6] S. Sideman, Y. Gat, Direct contact heat transfer with change of phase: Spray column

studies of a three-phase heat exchanger, AIChE J. 12(2)(1966) 296-303.

[7] Y.H. Mori, An analytic model of direct-contact heat transfer in spray-column evaporators.

AIChE Journal, 37(4) (1991) 539-546.

[8] G.L. Bauerle, R,C. Ahlert, Heat transfer and holdup phenomena in spray column, Indus.

Eng. Chem. Pro. Desg. Devl. 4(2)(1965) 225-230.

[9] S.B. Plass, H.R. Jacobs, R.F. Boehm, Operational characteristics of a spray column type

direct contact contactor preheater, AIChE Symposium Series-Heat Transfer, vol.

75(189)(1979) 227-234.

[10] S. Sideman, G. Hirsch, Y. Gat, Direct contact heat transfer with change phase: Effect of

the initial drop size in three-phase heat exchanger, AIChE J. 11(6)(1965) 1081-1087.

[11] T. Coban, R. Boehm, Performance of a three-phase, spray -column, direct-contact heat

exchanger, J. Heat Trans. 111(1) (1989) 166–172.

[12] H.R.Jacobs, M. Golafshani, Heuristic evaluation of the governing mode of heat transfer

in a liquid-liquid spray column, J. Heat Trans. 111(3) (1989) 773–779.

[13] Y. Shimizu, Y.H. Mori, Evaporation of single liquid drops in an immiscible liquid at

elevated pressure: experimental study with n-pentane and R113 drops in water, Int. J.

Heat Mass Trans. 31(9)(1988) 1843-1851.

[14] P. Battya, V.R. Raghavan, K.N. Seetharamu, Parametric analysis of direct contact

sensible heat transfer in spray column, Let. Heat Mass Trans. 9(4)(1982) 265-276.

[15] K.L. Core, J.C. Mulligan, Heat transfer and population characteristics of dispersed

evaporating droplets, AIChE J. 36(8)(1990) 1137-1144.

[16] S.M. Summers, C.T. Crowe, One-dimensional numerical model for a spray column heat

exchanger, AIChE J. 37(11)(1991) 1673-1679.

30

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628

629

630

631

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