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SUPERCOOLING WATER IN CYLINDRICAL CAPSULES1




J. J. Milón2 G. and S. L. Braga2,3




1
    Paper presented at the Fifteenth Symposium on Thermophysical Properties, June 22-

27, 2003, Boulder, Colorado, U.S.A.
2
    Department of Mechanical Engineering. Pontifical Catholic University of Rio de

Janeiro. CEP 22453-900 – Rio de Janeiro, RJ, Brazil
3
    Correspondence should be addressed to - E-mail: slbraga@mec.puc-rio.br
ABSTRACT



An experimental apparatus was developed to investigate the supercooling phenomenon

of water inside cylindrical capsules used for cold storage process. The transfer fluid

(TF), is a water-alcohol mixture, controlled by a constant temperature bath (CTB).

Temperatures varying with time are measured inside and outside the capsule. Cylinders

with internal diameter and thickness of 45 mm and 1.5 mm, respectively, were made

from four different materials: Acrylic, PVC, Brass and Aluminum. The supercooling

period of the water and the nucleation temperature were investigated for different

transfer fluid temperatures. The supercooling and nucleation probabilities are shown as

a function of the transfer fluid temperature for the four different materials.



KEY WORDS: air conditioning, nucleation, phase change, supercooling, refrigeration,

thermal storage.
Nomenclature

T     temperature, [ºC]

TTF   transfer fluid temperature, [ºC]

Tdi   maximum density temperature, [ºC]

To    initial temperature, [ºC]

Tm    phase change temperature, [ºC]

Tn    nucleation temperature, [ºC]

SD    supercooling degree, [ºC]

NS    supercooling probability, []

NF    nucleation probability, []

CR    cooling rate, [ºC min-1]



Convention

PCM phase change material

∆t    duration of the supercooled state

TF    transfer fluid

CTB   constant temperature bath

PVC   polyvinyl chloride

PID   proportional, integral and derivative control
1. INTRODUCTION



The thermal storage for refrigeration systems is an important concept of many energy

conservation programs. Water is widely used as the phase-change material (PCM) due

to its advantages: high value in latent heat, stable chemical properties, low cost and easy

acquisition, no environmental pollution concern, and compatibility with the materials

used in air-conditioning equipment. However, there are a few disadvantages in using

water as PCM. Two of the most serious problems encountered are the supercooling

phenomenon and the density inversion occurring in the water solidification during the

thermal storage cooling process.

When the water is cooled in an enclosed container, freezing does not occur at its

freezing point (0°C) at atmospheric pressure. Instead, it is normally cooled below 0°C

before ice nucleation happens. Supercooled water refers to a state of metastable liquid

even though the water temperature is below its freezing temperature. The metastable

state ends when ice nucleation occurs and the thin plate-like crystal of dendritic ice

grows into the supercooled region of water. During the dendritic ice growth process,

latent heat is released from the dendritic ice and consumed by supercooled water. At the

end of the growth process, the temperature of the water will return to its freezing point

(0°C). If the metastable state exists and remains during the thermal storage process,

thermal energy can only be stored in the form of sensible energy. In this case, the

storage capacity is strongly reduced. Because of this, it is very important to prevent the

occurrence of the supercooling and to acquire precise knowledge from the water

supercooling phenomenon during a thermal storage process.
There are several studies about the solidification of water: Chen et al. (1) studied the

numerical and experimental method to analyze the influence of nucleation agents in the

water solidification process inside cylindrical copper capsules of different sizes. Yoon et

al. (2) studied experimentally the freezing phenomenon of saturated water within the

supercooled region in a horizontal circular cylinder using the holographic real time

interferometry technique. Milón and Braga (3) studied the phenomenon of supercooling

in spherical capsules of different diameters and determined the parameters that

influence this phenomenon appearance.

The present work studies experimentally the supercooling phenomenon inside capsules

with perfectly cylindrical geometry made from different materials.



1.1 SUPERCOOLING IN CAPSULES

For a typical stable thermodynamic water cooling process, the temperature variation

versus time is presented in Fig. 1. The solidification starts in d’ and finishes in f,

without supercooling. The isothermal phase change process is evident. Fig. 2 presents

four different cooling processes: (I) Supercooling, nucleation and evident phase change;

(II) Supercooling, nucleation and no evident phase change; (III) Hypercooling and (IV)

Supercooling without nucleation. For supercooled water with nucleation, the completion

of freezing can be divided into four stages, as shown in Fig. 2 (except in case IV).

The first stage involves the process from the beginning of cooling, from the initial

temperature Ti to the metastable state, before the occurrence of nucleation, passing

through the maximum density effect, where the temperature inside the capsule is near

Tdi. This stage is called the sensible heat thermal storage process. In Fig.2: (a) water in


a stable liquid state and (b) water in a metastable liquid state. Tm and Tn represent the
freezing temperature and the nucleation temperature of water, respectively, then the

supercooling degree SD is defined as (Tm-Tn). The second stage is the process from the

occurrence of nucleation to the completion of dendritic ice formation, called the

dendritic ice formation process. This process begins at the occurrence of nucleation,

when the water temperature is Tn. Once nucleation occurs, a thin slice of dendritic ice,

as shown in Fig. 2(c), spreads rapidly from the nucleation site down toward the center

region of the cylinder; in the meanwhile, it also grows down along the cold boundary

layer region adjacent to the inner cylinder surface. Latent heat released by dendritic ice

enables the supercooled water temperature to rise to the temperature Tm, (d), where ice

and water can coexist inside the capsule. Once this equilibrium temperature is reached,

the formation of dendritic ice ends. The duration of this process is very short, lasting

only 1 to 5 seconds, depending on the degree of supercooling. In curve IV, the phase

change doesn’t happen and the water remains in a metastable state for an undetermined

time without the formation of dendritic ice. The third stage involves the phase-change

process, from the completion of ice crystals formation to the complete freezing of the

water inside the capsule. This is called the latent heat thermal storage process. This

process begins after the dendritic ice formation is finished. As indicated in Fig. 2(e), a

thick ice layer starts to form from the inner surface of the capsule toward the cell center

till the water is completely frozen (f). The last stage involves the process of the cooling

of ice until it reaches the same temperature as that of the coolant temperature. This

process is similar to the water sensible heat thermal storage process (g).
For the case presented in Fig. 1, as supercooling doesn’t happen, the solidification

process happens without the formation of dendritic ice in any stage. For the curves II

and III, Fig. 2, stage 3 is nearly null (rapid phase change).



2. EXPERIMENTAL APPARATUS



 The experimental apparatus, shown schematically in Figure 3, consists of a test section

(1), an observing system (2), a cooling system (3) and (4), and a measurement and data

logging system (5).



2.1. Test section.

This section contains the capsule to be analyzed. The walls are made of a 10 mm thick

acrylic plate externally covered with a 25 mm thick insulation. A test section transversal

cut is shown in the Figure 4. The diffuser is intended to homogenize the TF temperature

in the test section. The temperature control is carried out by a constant temperature bath

which receives the signals from a temperature sensor - RTD type PT-100. K type

thermocouples were used for the circulating fluid temperature registration. Two flanges

are installed in the vertical walls to facilitate the cylinder change. An overflow tank,

working at atmospheric pressure, was installed to compensate the volume variation

during the phase change. In the same figure, the cylindrical capsule, filled with the

PCM, can be observed. K type thermocouples of 0,076 mm diameter, covered with

Teflon, are also indicated. Their positions are in Fig. 5 and expressed in Table I. These

thermocouples are used to register the temperature during the experiences. To define the
volume of the PCM, a sliding disk (movable in the axial direction) is used. The acrylic

capsule is shown in Fig. 6.



2.2. Observing system

A digital camera (30 images per second), located inside a box, is used to register the

exact instant of the nucleation and the growth of the ice. To avoid condensation, the

space between the capsule and the camera’s lens is filled with nitrogen, an inert gas that

removes the humid air. The box is also insulated.



2.3. Cooling system

The cooling system can be seen in Fig. 3. It is composed of two constant temperature

baths (CTB) (3), two reservoirs (4) and the transfer fluid (TF). The initial temperature

for the tests is set at one CTB while the other CTB is set at the test temperature. The

temperature control system is of the PID type (Proportional Integral Derivative) and it is

able to maintain the temperature into a range of ±0.05 °C with a refrigeration power of

800 W at 0 ºC and 1000 W of electric power heater. The transfer fluid is an alcohol-

water solution (50% in volume).



2.4. Measuring and data logging system

The measurements and storage of data are made by the data acquisition system and a

personal computer (PC). The acquisition equipment, which communicates with the PC

by the RS232 communication port, receives processes and transmits the temperature

signals to PC for storage and posterior analysis.
3. EXPERIMENTAL PROCEDURE

The initial water temperature inside the capsule (25.0 ºC) was imposed using a constant

temperature bath (CTB). The cooling procedure starts by pumping the transfer fluid

(TF) through the upper reservoir while its temperature is controlled by the second CTB.

At this time the test section is empty at the initial temperature. When the desired test

temperature is reached, the FT is addressed to the section test absorbing the initial

thermal loads and passing later to the underneath tank. When the upper tank is empty,

the flow of the CTB is addressed toward the test section. After each test, a pump impels

the FT toward the upper reservoir for a new test. This procedure is carried out to

maintain the test temperature constant along each test. A lapse of time shorter than 4

min is necessary for the FT temperature to reach stability. This lapse represents less

then 2.5% of the total test time. See ∆t in Fig. 7.

The duration of each test varies from 1 to 5 hours, depending of the test conditions and

material of the capsule. If the nucleation doesn't happen within 5 hours, the test is

interrupted. The data is acquired once a second. Uncertainties are presented in Table II.



3.1. Investigated parameters

The following parameters were investigated: supercooling and nucleation probability,

cooling rate and temperature field for cylindrical capsules made of acrylic, PVC, brass

and aluminum. All capsules have a 45 mm internal diameter and 1.5 mm wall thickness.

Experiences were carried out with different temperatures of the transfer fluid (TF),

varying from -2 to -10 ºC, in steps of 2 ºC. For each temperature of the FT, the

procedure was repeated 20 times, with the same initial and boundary conditions.
4. RESULTS AND DISCUSSION

4.1 Effect of the cooling rate

The cooling rate is defined as the inner wall average temperature gradient evaluated

from the start of supercooling until the nucleation, or,

        n                  n
                                 (T     − TIWi−1   )
       ∑ CR ∑
                                  IWi

                                      ∆t ’
                  i
                                                                      SD
CR =   i =1
                      =   i =1
                                                       , or,   CR =      ........................................................................... (1)
              n                       n                               ∆t

CR is the cooling rate in the internal wall

TIWi is the internal wall temperature

∆t ’ is the time interval of acquisition data and n is the number of measurements.

∆t is the total supercooling time and the supercooling degree SD

SD is the supercooling degree



Figure 8 shows a test interrupted after 5 hours of supercooling without nucleation. The

effect of the TTF can be observed in Figs. 9 and 10. In both cases it is possible to


observe the phenomenon of supercooling, but for bigger TTF, the nucleation takes more

time to occur. It was always observed.

A solidification process without supercooling is observed in Fig. 11. The phase change

occurs exactly at Tm.

In Fig. 12, it is observed that the PCM starts supercooling (IW) and returns to Tm. It

was caused, probably, by the convection due to the density inversion effect. After some

time, the supercooling appears again and the nucleation takes place, starting the

solidification process. The IW temperature in Fig. 13 shows a phenomenon defined as
hypercooling (temperature in IW). When the nucleation occurs, the temperature rises to

a value smaller then Tm and continues falling in the sensible stage.

Fig. 14 shows the supercooling period as a function of cooling rate and material. It is

possible to see the great influence of the CR. Large values of this variable imply short

periods of supercooling.

4.2 Effect of coolant temperature on supercooling and nucleation probabilities

Figs. 15 and 16, show, respectively, the supercooling and nucleation probability

distribution curves, under different conditions of coolant temperatures, varying from -2

ºC to -10 ºC, for pure water, contained in the different capsules.



       number of observed supercoolings        number of nucleations
NS =                                    , NF =                       ....................(02)
             total number of test               total number of test



NS and NF are the supercooling and nucleation probabilities.


It is possible to see that the supercooling probability increases for bigger TTF. For TTF

-2 and -4ºC, this probability was 100%, independent of the material of the capsules. The

acrylic capsules present bigger probability of supercooling, probably due to its low

thermal conductivity. On the other hand, the aluminum capsule presents more cases of

supercooling then the PVC capsules. The reason for that could be its roughness and

should be well investigated. The probability of nucleation is presented in Fig. 16 and

shows that for high thermal conductivity materials, the nucleation occurs more

frequently. It can be explained by the stronger convection inside the capsules,

facilitating the starting of the freezing process.
4.3 Nucleation and solidification process

The nucleation process inside the acrylic capsule for TTF = -8 ºC can be observed in

Fig. 17. The left hand side of the figure presents the pictures captured along the test. On

the right hand side a schematic representation of the phenomenon is presented. The

entire process takes about 3 seconds. In the first image the PCM is supercooled at -8 ºC

and, for this particular case, the nucleation starts after 3500 seconds from the beginning

of the cooling process. The sequence shows the development of scattered thin dendrites

distributed inside the capsule. Figure 18 shows the continuation of the same case. After

the nucleation, solid ice grows from the wall. This process is slower then the nucleation

one and takes approximately 4.6 hours to be completed. For each image of the sequence

in Fig. 18 the correspondent instant of time is shown in minutes.           Two different

structures can be seen inside the capsule. A diffuse interface between the solid ice and

the solid dendritic structure regions is observed. Fig. 19 shows the images captured

from the solidification process of the water without supercooling, for the aluminum

capsule with TTF = -6ºC. In this case the dendritic structure is not present and the

interface is sharp and well defined. The total solidification process lasted 6.16 hours.



5. CONCLUSION

The supercooling phenomenon was experimentally investigated inside cylindrical

capsules filled with pure water, utilized as Phase Change Material (PCM) for cool

storage systems. Cylinders with 45 mm internal diameter and 1.5 mm wall thickness,

made from four different materials (Acrylic, PVC, Brass and Aluminum) were

investigated. The water supercooling period and the nucleation temperature were

investigated for different transfer fluid temperatures. Characteristic curves of water
cooling processes in cylindrical capsules with or without supercooling effects were

observed. Particular experiments were done, where continuous metastable states were

observed, or cases of double supercooling phenomenon. It was verified that the

supercooling probability increases for bigger TTF values. For TTF -2 and -4ºC, the

probability of supercooling was 100%, independent of the material of the capsule.

Nucleation is more frequent in experiences with high thermal conductivity materials.

When supercooling appears, dendritic ice accompanies the solidification process, as

well as the presence of a kind of mushy region. In the cases without supercooling, the

interface between the ice and the liquid water is well defined with no dendritic

formation.
REFERENCES



  1. S. L. Chen and T. Z. Lee. A study of the supercooling phenomenon and the

     freezing probability of water inside horizontal cylinders, International Journal of

     Heat and Mass Transfer, Volume 41, Issues 4-5, 3, Pages 769-783 (1998).

  2. J. I. Yoon, C. G. Moon, E.Kim, Y. S. Son, J. D. Kim, T. Kato. Experimental

     study on the freezing of water with supercooled region in a horizontal cylinder.

     Applied Thermal Engineering 21, 657-668 (2001).

  3. J.J. Milón and S. L. Braga, Spherical encapsulated cold storage, ICR 2003 –21st

     International Congress of Refrigeration, US, (2003).
Table I. Temperature sensors in the capsule.


  Symbol          Description          Distance from the center line

TF            Transfer fluid                       1,2 R
EW            External wall                        -(R+z)
IW            Internal wall                        -R
RMR           Right middle radius                  +R/2
C             Center                               0
LMR           Left middle radius                   -R/2

R is the cylinder radius and z is the cylinder wall thickness
Table II. Uncertainties of measurements


      Parameter               Uncertainty

Temperature               0,1 ºC
Time                      0,1 s
Length                    0,1 mm
Figure Captions



Fig. 1. Stable solidification of water.



Fig. 2. Metastable solidification of water.



Fig. 3. Experimental apparatus schematic diagram: test section (1); observing section

(2); cooling section: constant temperature bath (3) and reservoir (4), (5).



Fig. 4. Test section details.



Fig. 5. Test cylinder view.



Fig. 6. Capsule front view with thermocouples distribution.



Fig. 7. Temperature of the TF during a typical test.



Fig. 8. Temperature versus time, acrylic, TFT=-6 ºC




Fig. 9. Temperature versus time, brass, TFT=-6 ºC, CR= 0,082 C/min




Fig. 10. Temperature versus time, PVC, TFT=-8 ºC, CR= 0,214 C/min
Fig. 11. Temperature versus time, brass, TFT=-8 ºC




Fig. 12. Temperature versus time, PVC, TFT=-10 ºC, CR= 0,556 C/min




Fig. 13. Temperature versus time, aluminum, TFT=-10 ºC, CR= 0,609 C/min




Fig. 14. Supercooling period as a function of the cooling rate, different materials.



Fig. 15. Supercooling probability



Fig. 16. Nucleation probability



Fig. 17. Nucleation process: The left column shows the real image, the middle one the

time, in seconds, and the right one the processed image. Acrylic with TFT = -8 ºC.




Fig. 18. Solidification process: The left column shows the real image, the middle one

the time, in minutes, and the right one the processed image. Acrylic with TFT = -8 ºC




Fig. 19. Solidification process: The left column shows the real image, the middle one

the time, in minutes, and the right one the processed image. Brass with TFT = -6 ºC.
Ti
                                        liquid water
Temperature                             ice


                    a

              Tdi
                            e’
              Tm
                                                       g

              TTF


                                 Time




                        a         e’               g




                                                           Fig. 1
Ti
                                                           liquid water
                                                                                         I
                                                           dendritic ice                 II
                                                                                         III
Temperature
                                                           ice
                                                                                         IV
                    a
              Tdi              d
                                                                    f
                                                   e
              Tm
                         b         c                        g                 g
              Tn                               g
                                           b
              TTF


                                                   Time




                        a, b           c               d                  e       f,g




                                                                                        Fig. 2
5


    3




4
                             3
            2




        1




                4




                    Fig. 3
NITROGEN          RTD
                           PT-100      TF
           OUTLET
                                                             SECONDARY
                                                             DIFFUSER

                                                                  THERMOCOUPLES
          FIXED DISK                        CAPSULE

DIGITAL
CAMERA
                                                                             OVERFLOW
                                                                             TANK
                             PCM


                                                             SLIDING DISK
          NITROGEN
          CHAMBER




           NITROGEN
             INLET                     TF             PRIMARY
                       THERMOCOUPLES                  DIFFUSER




                                                                            Fig. 4
thermocouples                   cylinder
      support


                                       z




TF     EW IW    LMR   C   RMR




                           R




                                           Fig. 5
Fig. 6
30
               25
               20
temperature
               15
               To
               10
                5
                0
                -5
              TCTB
               -10
               -15
                         ∆t                        time
                     0.0 5.0 10.0 15.0 20.0 25.0 30.0 35.0 40.0 45.0 50.0 55.0 60.0




                                                                                      Fig.7
25
                                                              TF
                  20                                          EW
                                                              IW
                  15                                          LMR
temperature, ºC



                                                              C
                  10                                          RMR


                   5

                   0

                   -5

                  -10

                        0   3000   6000   9000      12000 15000 18000
                                          time, s




                                                                        Fig. 8
25
                                                      TF
                  20                                  EW
                                                      IW
                  15                                  LMR
temperature, ºC



                                                      C
                  10                                  RMR


                   5

                   0

                   -5

                  -10

                        0   2500   5000       7500   10000
                                    time, s




                                                             Fig. 9
25
                                                     TF
                  20                                 EW
                                                     IW
                  15                                 LMR
temperature, ºC



                                                     C
                  10                                 RMR


                   5

                   0

                   -5

                  -10

                        0   2500   5000       7500   10000
                                    time, s




                                                             Fig. 10
25
                                                    TF
                  20                                EW
                                                    IW
                  15                                LMR
temperature, ºC



                                                    C
                  10                                RMR


                   5

                   0

                   -5

                  -10

                        0   2000             4000        6000
                                   time, s




                                                                Fig. 11
25
                                                                TF
                  20                                            EW
                                                                IW
                  15                                            LMR
temperature, ºC



                                                                C
                  10                                            RMR


                   5

                   0

                   -5

                  -10

                        0   250   500    750      1000   1250        1500
                                        time, s




                                                                            Fig. 12
25
                                                            TF
                  20                                        EW
                                                            IW
                  15                                        LMR
temperature, ºC


                                                            C
                  10                                        RMR


                   5

                   0

                   -5

                  -10

                        0   200   400   600   800   1000 1200 1400
                                         time, s




                                                                     Fig. 13
14000

12000

10000                              aluminum
                                   acrylic
 8000                              brass
                                   pvc
 6000

 4000

 2000

    0
        0   0.5                1              1.5
                  CR, ºC/min




                                                    Fig. 14
100%



     80%
                                             PVC
                                             ACRYLIC
                                             BRASS
     60%
                                             ALUMINUM
NS




     40%



     20%



      0%
            -10   -8   -6              -4   -2          0

                            TTF , ºC




                                                            Fig. 15
100%



       80%                                     PVC
                                               ACRYLIC
                                               BRASS
                                               ALUMINUM
       60%
  NF




       40%



       20%



          0%
               -10   -8   -6             -4   -2          0

                               TTF, ºC




Fig. 17

                                                              Fig. 16
0.0




0.5
       dendritic ice

       liquid water




1.0




1.5




2.0




2.5




      Fig. 17
0




67




       ice

       ice in dendritic
120
       structure

       dendrites +
       liquid water




184




243




277




      Fig. 18
0




43




209


      ice

      liquid water



306




355




370




      Fig. 19

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SUPERCOOLING WATER IN CYLINDRICAL CAPSULES

  • 1. SUPERCOOLING WATER IN CYLINDRICAL CAPSULES1 J. J. Milón2 G. and S. L. Braga2,3 1 Paper presented at the Fifteenth Symposium on Thermophysical Properties, June 22- 27, 2003, Boulder, Colorado, U.S.A. 2 Department of Mechanical Engineering. Pontifical Catholic University of Rio de Janeiro. CEP 22453-900 – Rio de Janeiro, RJ, Brazil 3 Correspondence should be addressed to - E-mail: slbraga@mec.puc-rio.br
  • 2. ABSTRACT An experimental apparatus was developed to investigate the supercooling phenomenon of water inside cylindrical capsules used for cold storage process. The transfer fluid (TF), is a water-alcohol mixture, controlled by a constant temperature bath (CTB). Temperatures varying with time are measured inside and outside the capsule. Cylinders with internal diameter and thickness of 45 mm and 1.5 mm, respectively, were made from four different materials: Acrylic, PVC, Brass and Aluminum. The supercooling period of the water and the nucleation temperature were investigated for different transfer fluid temperatures. The supercooling and nucleation probabilities are shown as a function of the transfer fluid temperature for the four different materials. KEY WORDS: air conditioning, nucleation, phase change, supercooling, refrigeration, thermal storage.
  • 3. Nomenclature T temperature, [ºC] TTF transfer fluid temperature, [ºC] Tdi maximum density temperature, [ºC] To initial temperature, [ºC] Tm phase change temperature, [ºC] Tn nucleation temperature, [ºC] SD supercooling degree, [ºC] NS supercooling probability, [] NF nucleation probability, [] CR cooling rate, [ºC min-1] Convention PCM phase change material ∆t duration of the supercooled state TF transfer fluid CTB constant temperature bath PVC polyvinyl chloride PID proportional, integral and derivative control
  • 4. 1. INTRODUCTION The thermal storage for refrigeration systems is an important concept of many energy conservation programs. Water is widely used as the phase-change material (PCM) due to its advantages: high value in latent heat, stable chemical properties, low cost and easy acquisition, no environmental pollution concern, and compatibility with the materials used in air-conditioning equipment. However, there are a few disadvantages in using water as PCM. Two of the most serious problems encountered are the supercooling phenomenon and the density inversion occurring in the water solidification during the thermal storage cooling process. When the water is cooled in an enclosed container, freezing does not occur at its freezing point (0°C) at atmospheric pressure. Instead, it is normally cooled below 0°C before ice nucleation happens. Supercooled water refers to a state of metastable liquid even though the water temperature is below its freezing temperature. The metastable state ends when ice nucleation occurs and the thin plate-like crystal of dendritic ice grows into the supercooled region of water. During the dendritic ice growth process, latent heat is released from the dendritic ice and consumed by supercooled water. At the end of the growth process, the temperature of the water will return to its freezing point (0°C). If the metastable state exists and remains during the thermal storage process, thermal energy can only be stored in the form of sensible energy. In this case, the storage capacity is strongly reduced. Because of this, it is very important to prevent the occurrence of the supercooling and to acquire precise knowledge from the water supercooling phenomenon during a thermal storage process.
  • 5. There are several studies about the solidification of water: Chen et al. (1) studied the numerical and experimental method to analyze the influence of nucleation agents in the water solidification process inside cylindrical copper capsules of different sizes. Yoon et al. (2) studied experimentally the freezing phenomenon of saturated water within the supercooled region in a horizontal circular cylinder using the holographic real time interferometry technique. Milón and Braga (3) studied the phenomenon of supercooling in spherical capsules of different diameters and determined the parameters that influence this phenomenon appearance. The present work studies experimentally the supercooling phenomenon inside capsules with perfectly cylindrical geometry made from different materials. 1.1 SUPERCOOLING IN CAPSULES For a typical stable thermodynamic water cooling process, the temperature variation versus time is presented in Fig. 1. The solidification starts in d’ and finishes in f, without supercooling. The isothermal phase change process is evident. Fig. 2 presents four different cooling processes: (I) Supercooling, nucleation and evident phase change; (II) Supercooling, nucleation and no evident phase change; (III) Hypercooling and (IV) Supercooling without nucleation. For supercooled water with nucleation, the completion of freezing can be divided into four stages, as shown in Fig. 2 (except in case IV). The first stage involves the process from the beginning of cooling, from the initial temperature Ti to the metastable state, before the occurrence of nucleation, passing through the maximum density effect, where the temperature inside the capsule is near Tdi. This stage is called the sensible heat thermal storage process. In Fig.2: (a) water in a stable liquid state and (b) water in a metastable liquid state. Tm and Tn represent the
  • 6. freezing temperature and the nucleation temperature of water, respectively, then the supercooling degree SD is defined as (Tm-Tn). The second stage is the process from the occurrence of nucleation to the completion of dendritic ice formation, called the dendritic ice formation process. This process begins at the occurrence of nucleation, when the water temperature is Tn. Once nucleation occurs, a thin slice of dendritic ice, as shown in Fig. 2(c), spreads rapidly from the nucleation site down toward the center region of the cylinder; in the meanwhile, it also grows down along the cold boundary layer region adjacent to the inner cylinder surface. Latent heat released by dendritic ice enables the supercooled water temperature to rise to the temperature Tm, (d), where ice and water can coexist inside the capsule. Once this equilibrium temperature is reached, the formation of dendritic ice ends. The duration of this process is very short, lasting only 1 to 5 seconds, depending on the degree of supercooling. In curve IV, the phase change doesn’t happen and the water remains in a metastable state for an undetermined time without the formation of dendritic ice. The third stage involves the phase-change process, from the completion of ice crystals formation to the complete freezing of the water inside the capsule. This is called the latent heat thermal storage process. This process begins after the dendritic ice formation is finished. As indicated in Fig. 2(e), a thick ice layer starts to form from the inner surface of the capsule toward the cell center till the water is completely frozen (f). The last stage involves the process of the cooling of ice until it reaches the same temperature as that of the coolant temperature. This process is similar to the water sensible heat thermal storage process (g).
  • 7. For the case presented in Fig. 1, as supercooling doesn’t happen, the solidification process happens without the formation of dendritic ice in any stage. For the curves II and III, Fig. 2, stage 3 is nearly null (rapid phase change). 2. EXPERIMENTAL APPARATUS The experimental apparatus, shown schematically in Figure 3, consists of a test section (1), an observing system (2), a cooling system (3) and (4), and a measurement and data logging system (5). 2.1. Test section. This section contains the capsule to be analyzed. The walls are made of a 10 mm thick acrylic plate externally covered with a 25 mm thick insulation. A test section transversal cut is shown in the Figure 4. The diffuser is intended to homogenize the TF temperature in the test section. The temperature control is carried out by a constant temperature bath which receives the signals from a temperature sensor - RTD type PT-100. K type thermocouples were used for the circulating fluid temperature registration. Two flanges are installed in the vertical walls to facilitate the cylinder change. An overflow tank, working at atmospheric pressure, was installed to compensate the volume variation during the phase change. In the same figure, the cylindrical capsule, filled with the PCM, can be observed. K type thermocouples of 0,076 mm diameter, covered with Teflon, are also indicated. Their positions are in Fig. 5 and expressed in Table I. These thermocouples are used to register the temperature during the experiences. To define the
  • 8. volume of the PCM, a sliding disk (movable in the axial direction) is used. The acrylic capsule is shown in Fig. 6. 2.2. Observing system A digital camera (30 images per second), located inside a box, is used to register the exact instant of the nucleation and the growth of the ice. To avoid condensation, the space between the capsule and the camera’s lens is filled with nitrogen, an inert gas that removes the humid air. The box is also insulated. 2.3. Cooling system The cooling system can be seen in Fig. 3. It is composed of two constant temperature baths (CTB) (3), two reservoirs (4) and the transfer fluid (TF). The initial temperature for the tests is set at one CTB while the other CTB is set at the test temperature. The temperature control system is of the PID type (Proportional Integral Derivative) and it is able to maintain the temperature into a range of ±0.05 °C with a refrigeration power of 800 W at 0 ºC and 1000 W of electric power heater. The transfer fluid is an alcohol- water solution (50% in volume). 2.4. Measuring and data logging system The measurements and storage of data are made by the data acquisition system and a personal computer (PC). The acquisition equipment, which communicates with the PC by the RS232 communication port, receives processes and transmits the temperature signals to PC for storage and posterior analysis.
  • 9. 3. EXPERIMENTAL PROCEDURE The initial water temperature inside the capsule (25.0 ºC) was imposed using a constant temperature bath (CTB). The cooling procedure starts by pumping the transfer fluid (TF) through the upper reservoir while its temperature is controlled by the second CTB. At this time the test section is empty at the initial temperature. When the desired test temperature is reached, the FT is addressed to the section test absorbing the initial thermal loads and passing later to the underneath tank. When the upper tank is empty, the flow of the CTB is addressed toward the test section. After each test, a pump impels the FT toward the upper reservoir for a new test. This procedure is carried out to maintain the test temperature constant along each test. A lapse of time shorter than 4 min is necessary for the FT temperature to reach stability. This lapse represents less then 2.5% of the total test time. See ∆t in Fig. 7. The duration of each test varies from 1 to 5 hours, depending of the test conditions and material of the capsule. If the nucleation doesn't happen within 5 hours, the test is interrupted. The data is acquired once a second. Uncertainties are presented in Table II. 3.1. Investigated parameters The following parameters were investigated: supercooling and nucleation probability, cooling rate and temperature field for cylindrical capsules made of acrylic, PVC, brass and aluminum. All capsules have a 45 mm internal diameter and 1.5 mm wall thickness. Experiences were carried out with different temperatures of the transfer fluid (TF), varying from -2 to -10 ºC, in steps of 2 ºC. For each temperature of the FT, the procedure was repeated 20 times, with the same initial and boundary conditions.
  • 10. 4. RESULTS AND DISCUSSION 4.1 Effect of the cooling rate The cooling rate is defined as the inner wall average temperature gradient evaluated from the start of supercooling until the nucleation, or, n n (T − TIWi−1 ) ∑ CR ∑ IWi ∆t ’ i SD CR = i =1 = i =1 , or, CR = ........................................................................... (1) n n ∆t CR is the cooling rate in the internal wall TIWi is the internal wall temperature ∆t ’ is the time interval of acquisition data and n is the number of measurements. ∆t is the total supercooling time and the supercooling degree SD SD is the supercooling degree Figure 8 shows a test interrupted after 5 hours of supercooling without nucleation. The effect of the TTF can be observed in Figs. 9 and 10. In both cases it is possible to observe the phenomenon of supercooling, but for bigger TTF, the nucleation takes more time to occur. It was always observed. A solidification process without supercooling is observed in Fig. 11. The phase change occurs exactly at Tm. In Fig. 12, it is observed that the PCM starts supercooling (IW) and returns to Tm. It was caused, probably, by the convection due to the density inversion effect. After some time, the supercooling appears again and the nucleation takes place, starting the solidification process. The IW temperature in Fig. 13 shows a phenomenon defined as
  • 11. hypercooling (temperature in IW). When the nucleation occurs, the temperature rises to a value smaller then Tm and continues falling in the sensible stage. Fig. 14 shows the supercooling period as a function of cooling rate and material. It is possible to see the great influence of the CR. Large values of this variable imply short periods of supercooling. 4.2 Effect of coolant temperature on supercooling and nucleation probabilities Figs. 15 and 16, show, respectively, the supercooling and nucleation probability distribution curves, under different conditions of coolant temperatures, varying from -2 ºC to -10 ºC, for pure water, contained in the different capsules. number of observed supercoolings number of nucleations NS = , NF = ....................(02) total number of test total number of test NS and NF are the supercooling and nucleation probabilities. It is possible to see that the supercooling probability increases for bigger TTF. For TTF -2 and -4ºC, this probability was 100%, independent of the material of the capsules. The acrylic capsules present bigger probability of supercooling, probably due to its low thermal conductivity. On the other hand, the aluminum capsule presents more cases of supercooling then the PVC capsules. The reason for that could be its roughness and should be well investigated. The probability of nucleation is presented in Fig. 16 and shows that for high thermal conductivity materials, the nucleation occurs more frequently. It can be explained by the stronger convection inside the capsules, facilitating the starting of the freezing process.
  • 12. 4.3 Nucleation and solidification process The nucleation process inside the acrylic capsule for TTF = -8 ºC can be observed in Fig. 17. The left hand side of the figure presents the pictures captured along the test. On the right hand side a schematic representation of the phenomenon is presented. The entire process takes about 3 seconds. In the first image the PCM is supercooled at -8 ºC and, for this particular case, the nucleation starts after 3500 seconds from the beginning of the cooling process. The sequence shows the development of scattered thin dendrites distributed inside the capsule. Figure 18 shows the continuation of the same case. After the nucleation, solid ice grows from the wall. This process is slower then the nucleation one and takes approximately 4.6 hours to be completed. For each image of the sequence in Fig. 18 the correspondent instant of time is shown in minutes. Two different structures can be seen inside the capsule. A diffuse interface between the solid ice and the solid dendritic structure regions is observed. Fig. 19 shows the images captured from the solidification process of the water without supercooling, for the aluminum capsule with TTF = -6ºC. In this case the dendritic structure is not present and the interface is sharp and well defined. The total solidification process lasted 6.16 hours. 5. CONCLUSION The supercooling phenomenon was experimentally investigated inside cylindrical capsules filled with pure water, utilized as Phase Change Material (PCM) for cool storage systems. Cylinders with 45 mm internal diameter and 1.5 mm wall thickness, made from four different materials (Acrylic, PVC, Brass and Aluminum) were investigated. The water supercooling period and the nucleation temperature were investigated for different transfer fluid temperatures. Characteristic curves of water
  • 13. cooling processes in cylindrical capsules with or without supercooling effects were observed. Particular experiments were done, where continuous metastable states were observed, or cases of double supercooling phenomenon. It was verified that the supercooling probability increases for bigger TTF values. For TTF -2 and -4ºC, the probability of supercooling was 100%, independent of the material of the capsule. Nucleation is more frequent in experiences with high thermal conductivity materials. When supercooling appears, dendritic ice accompanies the solidification process, as well as the presence of a kind of mushy region. In the cases without supercooling, the interface between the ice and the liquid water is well defined with no dendritic formation.
  • 14. REFERENCES 1. S. L. Chen and T. Z. Lee. A study of the supercooling phenomenon and the freezing probability of water inside horizontal cylinders, International Journal of Heat and Mass Transfer, Volume 41, Issues 4-5, 3, Pages 769-783 (1998). 2. J. I. Yoon, C. G. Moon, E.Kim, Y. S. Son, J. D. Kim, T. Kato. Experimental study on the freezing of water with supercooled region in a horizontal cylinder. Applied Thermal Engineering 21, 657-668 (2001). 3. J.J. Milón and S. L. Braga, Spherical encapsulated cold storage, ICR 2003 –21st International Congress of Refrigeration, US, (2003).
  • 15. Table I. Temperature sensors in the capsule. Symbol Description Distance from the center line TF Transfer fluid 1,2 R EW External wall -(R+z) IW Internal wall -R RMR Right middle radius +R/2 C Center 0 LMR Left middle radius -R/2 R is the cylinder radius and z is the cylinder wall thickness
  • 16. Table II. Uncertainties of measurements Parameter Uncertainty Temperature 0,1 ºC Time 0,1 s Length 0,1 mm
  • 17. Figure Captions Fig. 1. Stable solidification of water. Fig. 2. Metastable solidification of water. Fig. 3. Experimental apparatus schematic diagram: test section (1); observing section (2); cooling section: constant temperature bath (3) and reservoir (4), (5). Fig. 4. Test section details. Fig. 5. Test cylinder view. Fig. 6. Capsule front view with thermocouples distribution. Fig. 7. Temperature of the TF during a typical test. Fig. 8. Temperature versus time, acrylic, TFT=-6 ºC Fig. 9. Temperature versus time, brass, TFT=-6 ºC, CR= 0,082 C/min Fig. 10. Temperature versus time, PVC, TFT=-8 ºC, CR= 0,214 C/min
  • 18. Fig. 11. Temperature versus time, brass, TFT=-8 ºC Fig. 12. Temperature versus time, PVC, TFT=-10 ºC, CR= 0,556 C/min Fig. 13. Temperature versus time, aluminum, TFT=-10 ºC, CR= 0,609 C/min Fig. 14. Supercooling period as a function of the cooling rate, different materials. Fig. 15. Supercooling probability Fig. 16. Nucleation probability Fig. 17. Nucleation process: The left column shows the real image, the middle one the time, in seconds, and the right one the processed image. Acrylic with TFT = -8 ºC. Fig. 18. Solidification process: The left column shows the real image, the middle one the time, in minutes, and the right one the processed image. Acrylic with TFT = -8 ºC Fig. 19. Solidification process: The left column shows the real image, the middle one the time, in minutes, and the right one the processed image. Brass with TFT = -6 ºC.
  • 19. Ti liquid water Temperature ice a Tdi e’ Tm g TTF Time a e’ g Fig. 1
  • 20. Ti liquid water I dendritic ice II III Temperature ice IV a Tdi d f e Tm b c g g Tn g b TTF Time a, b c d e f,g Fig. 2
  • 21. 5 3 4 3 2 1 4 Fig. 3
  • 22. NITROGEN RTD PT-100 TF OUTLET SECONDARY DIFFUSER THERMOCOUPLES FIXED DISK CAPSULE DIGITAL CAMERA OVERFLOW TANK PCM SLIDING DISK NITROGEN CHAMBER NITROGEN INLET TF PRIMARY THERMOCOUPLES DIFFUSER Fig. 4
  • 23. thermocouples cylinder support z TF EW IW LMR C RMR R Fig. 5
  • 25. 30 25 20 temperature 15 To 10 5 0 -5 TCTB -10 -15 ∆t time 0.0 5.0 10.0 15.0 20.0 25.0 30.0 35.0 40.0 45.0 50.0 55.0 60.0 Fig.7
  • 26. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 3000 6000 9000 12000 15000 18000 time, s Fig. 8
  • 27. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 2500 5000 7500 10000 time, s Fig. 9
  • 28. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 2500 5000 7500 10000 time, s Fig. 10
  • 29. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 2000 4000 6000 time, s Fig. 11
  • 30. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 250 500 750 1000 1250 1500 time, s Fig. 12
  • 31. 25 TF 20 EW IW 15 LMR temperature, ºC C 10 RMR 5 0 -5 -10 0 200 400 600 800 1000 1200 1400 time, s Fig. 13
  • 32. 14000 12000 10000 aluminum acrylic 8000 brass pvc 6000 4000 2000 0 0 0.5 1 1.5 CR, ºC/min Fig. 14
  • 33. 100% 80% PVC ACRYLIC BRASS 60% ALUMINUM NS 40% 20% 0% -10 -8 -6 -4 -2 0 TTF , ºC Fig. 15
  • 34. 100% 80% PVC ACRYLIC BRASS ALUMINUM 60% NF 40% 20% 0% -10 -8 -6 -4 -2 0 TTF, ºC Fig. 17 Fig. 16
  • 35. 0.0 0.5 dendritic ice liquid water 1.0 1.5 2.0 2.5 Fig. 17
  • 36. 0 67 ice ice in dendritic 120 structure dendrites + liquid water 184 243 277 Fig. 18
  • 37. 0 43 209 ice liquid water 306 355 370 Fig. 19