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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 396
ExperimentalInvestigationofGraphenecoatedAlcuboidcrammedwithPCM`s
forEfficientThermalEnergyStorageandConversion.
Ch. Abhinav1, K. Vamsi Krishna Reddy2, G. Goutham Raju3, K. Subramanyam4
1,2,3B. Tech in Mechanical Engineering, Raghu Institute of Technology, JNTU Kakinada, Visakhapatnam, India.
4 Nano Technology Research laboratory, Raghu Engineering College, Visakhapatnam, India.
-----------------------------------------------------------------------***--------------------------------------------------------------------
Abstract: In this paper, we report on the development of a composite cuboid (20x20x20/A cm3) which can absorb, store and
supply heat consistently for longer periods even the heat source is turned off. The main frame of this composite cuboid is made
up of aluminium, whose top surface which faces the heat source is coated with graphene. The hollow space inside the cuboid is
filled with paraffin wax pellets for latent heat storage. This cuboid is placed inside an insulated thermocol box whose interior
is concealed with reflective aluminium foil. a 100-watt incandescent bulb is used as a heat source. Due to the high thermal
conductivity of graphene the thermal conductivity of the aluminium increases, resulting in the high amount of heat
absorption. Heat is absorbed by the paraffin wax resulting in the phase change from solid to liquid. This latent heat storage
liberates heat uniformly until the phase is altered to its original state. This resulted in a maximum temperature of 105°C in 80
minutes and took 148 min to reach room temperature (240c). In contrast, the normal aluminium box without coating and
PCM reached a maximum temperature of 77°C in 30 min and a cooling time of 40 min. The results show that the usage of
PCM’s decreased the rate of cooling and graphene coat increased the heat transfer through the surface.
Key Words: Composites, Coating, Graphene, Latent Heat Storage, PCM`s.
1. INTRODUCTION
Mankind has been highly reliant on fossil fuels which are being used in wide applications ranging from
combustion engines to electricity. This unceasing usage of non-renewable resources from several decades led to the
diminishing of existing fossil fuels and even led to increase of greenhouse gases. This problem can be solved either by
using renewable resources or implementation of efficient energy storage systems. But, most of the renewable energy
sources are not consistent round the clock. The intensity of the energy output from these renewable sources can
sometimes reach more than requirement experience a sudden drop. Thus, energy storage systems play a crucial role in
diminishing the gap between energy supply and energy usage. The heat energy can be stored in several types of materials
as sensible heat or latent heat which results either in temperature rise or a change in phase. The energy stored in solid or
liquid by raising its temperature is called sensible heat storage and heat storage acquired by a change in phase is called
latent heat storage. Latent heat energy storage is efficient due to the reason that its ability to store and maintain heat at
constant temperature. Properties like phase transition temperature and high latent heat of transition and good heat
transfer need to be considered while selecting a PCM. In general paraffin wax (CH3-CH2-CH3) is used as PCM’s. The chain
length of the paraffin wax can affect both melting point and latent heat of fission. Moreover, paraffin wax is less expensive,
non-corrosive, predictable, safe and reliable.
In most of the developed countries majority of the energy is consumed for conditioning air in the buildings to
ensure indoor thermal comfort. This led to a surge in energy consumption and air pollution caused by the greenhouse gas
emission. To increase the efficiency and decrease negative effects on the environment, energy storage systems are a great
solution. In recent constructions of green buildings, microencapsulated Phase change materials are incorporated within
concrete walls. This PCM’s in the concrete wall absorbs heat from the sun during the day maintaining the human thermal
temperature at 23°c but during cooler nights PCM’s releases the stored heat and solidifies. In the same way, this storage
module can increase the efficiency of heat exchangers, solar water heater, and food drying machines. Graphene is one of
the very few materials with high thermal conductivity which ranges from (4.84 ± 0.44) x 103 to (5.30 ± 0.48) x 103 W/mK.
Single layer graphene has higher thermal conductivity. The number of layers influences its thermal conductivity further,
the thermal conductivity decreases from 2800 to 1300 W/mK with an increase in the number of the atomic planes from 2
to 4. Phonons are the reason behind its high thermal conductivity. On the other hand, graphene possesses high elastic
properties. When graphene is reinforced with aluminium alloys the resultant metal matrix composites show high thermal
conductivity than ordinary aluminium alloys. Moreover, the thermal conductivity of aluminium metal matrix composites
increases by 15% at 250°C. These concepts of graphene and PCM’s are used in developing our composite cuboid. Graphene
coating resulted in an increase in max temperature by 30o than the normal aluminium sheet. The addition of phase change
material made the composite cuboid to store and supply heat for nearly four times the time than the regular metal.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 397
2. EXPERIMENTAL SETUP
The experimental setup can be broadly classified into
A. Aluminium box setup.
B. Heating system.
A. Aluminium box setup: -
Aluminium sheet of 0.1cm thickness is used to make a tray of 20x20x4 cm3 (1600 cm3) by using tin smithy which
has an opening at the top. This tray rests on a hollow box of dimensions 22x22x12 cm3 (5808 cm3) with the help of
clamps on its inner edges closing the top side of the hollow box. This results in a decrease in volume of the hollow
box from 5808 cm3 to 3872 cm3, which is the control volume and its temperature is recorded.
As the size of the cuboid surface is large there is no available equipment for us to coat Graphene. So, the top
surface of the cuboid box is coated with a mixture of black enamel paint and graphene powder. To ensure the
uniformity, graphene powder is sieved while the paint is wet and the excess is dusted. Half of the empty space
inside the cuboid box is filled with wax. Various view of the aluminium box setup is shown in figures 1-4 below.
FIG.1-4: shows the box setup with hollow box and tray
B. Heating system: -
Heating system is further classified into
1) Heat Source.
2) Insulation.
3) Temperature measuring devices.
A thermocol box of dimensions 30x34x40 cm3 (40800 cm3) is constructed whose interior is insulated with a white
drawing chart which acts as an insulator and protects the thermocol from melting. This chart is covered with Aluminium
foil to ensure there is no heat loss, most of the heat stays inside the thermocol box. A 100W incandescent tungsten filament
bulb is used as a heat source at 220V AC power source and to record the temperature inside the control volume a K-type
thermocouple is installed which records the temperature change throughout the process. Various view of the setup is
shown in Fig. 5-8 below.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 398
FIG. 5-8 shows the heating system
FIG. 7 shows the graphene-coated lid inside heating system
Temperature representations:
 The temperature inside the control volume: T1.
 The temperature outside the control volume (Outside the aluminium box and inside the thermocol box): T2.
3. EXPERIMENT
The aluminium box setup is placed inside the thermocol box and its lid is closed. The initial temperature of the setup is
recorded. Though our ultimate result of the setup coated with Graphene and filled with PCM is the main goal, we wanted to
do a comparative analysis hence, we experimented with four variations as shown in table 1 below.
Table 1: Experiment Variations
Expt. No. Box Material Aluminium box
setup
PCM Graphene + Paint
Mixture
1 Aluminium  - -
2 Aluminium  - 
3 Aluminium   -
4 Aluminium   
For all the experiments initially, the heat source is turned on and the setup is heated until it reaches a steady maximum
temperature and is recorded, Later the source is turned off and the time taken to reach the room temperature is also
recorded. Here the temperature inside the control volume i: e T1 is considered as mainly notable.
4. EXPERIMENTAL RESULTS
Exp. No.1 (Only the Aluminium Box Setup):-
It took nearly 30 minutes to reach a maximum temperature of 770c T1. In just 14 minutes the temperature has
raised to 500c from 220c (room temperature). The rise in temperature is quick till it reached 500c, later it took 16 minutes
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 399
for a 270c rise from 500c to 770c. When the source is turned off, it took 40 minutes to get back to room temperature from
saturated temperature.
Exp. No.2 (Top Surface of Cuboid Coated with Graphene Paint Mixture):-
When the top surface is coated with graphene, the maximum temperature reached is around 850c. It took 35
minutes to reach the maximum temperature and the rise in temperature was very quick from 220c to 770c later the time
taken for every degree rise is increased. When the source is turned off, it took 55 minutes to reach the room temperature.
In general, the temperature inside the control volume of coated setup is 40c-80c more when compared to normal
aluminium setup. For instance, if T2 is 400C thenT1 (without graphene coat) is 240C and inside the graphene-coated one is
280C (T1), When T2 is 600c, the inner temperature is around 300c for noncoated one and is 360c for coated one.
Exp. No.3 (Hollow space filled with PCM without Graphene coat):-
This experiment is subdivided into two parts based on the PCM`s. Half of the hollow space is filled with PCM`s. In
the first part, we smashed a household candle and in the second experiment, we used wax pellets from the chemical store.
In both the experiments we heated for 40 minutes which resulted in a temperature of 770c raised from 210c (room
temperature). But, in the previous experiments, the time taken to reach 770c is around 30 minutes. This is due to the
reason that, the heat supplied is absorbed by wax present in the hollow space. Then the heat source is turned off. In the
case of candle wax, it took 80 minutes to reach the room temperature. On the other hand, it took nearly 134 minutes to
reach room temperature when candle wax is replaced with wax pellets. This may be due to the small size and purity of wax
pellets. In both experiments the temperature fall from 770c to 400c is very fast, it took around 1-2 minutes. This is a
stunner that even degree temperatures stayed for a long time than the odd temperatures; 360c (2m 8s), 340c (3m 30s),
320c (10m 30s), 300c (23m), 280c (24m) and so-on. In contrast, the odd temperatures; like 390c, 370c, 350c, 330c stayed for
lesser than 30s. There are also similarities with the previous experiments like a sharp decrease in temperature from 770c
to 400c and 55 minutes for 400c to 300c. Further, the time still increased for the fall of temperature from 300c to 220c.
Exp. No.4(Complete setup): -
In this experiment, the top layer of the cuboid is coated with graphene-paint mixture and graphene powder is
sieved over the wet paint surface 3 times to ensure a uniform surface. The half of the hollow space of the cuboid is filled
with wax pellets. The total time taken to reach the maximum temperature is 80 minutes and the maximum temperature is
1050c. We can observe from the readings below that there is a gradual decrease in time from 240c to 430c, later the time
has increased gradually reaching a peak of 9:33 minutes for 69-73 degrees rise. Further, the time followed a similar
pattern to that of previous intervals reaching a maximum time of 11:09 minutes for the 100-105 interval. All Intervals and
their time patterns are given in table 2 below.
Table 2: Heating and Cooling patterns.
S.no Heating Cooling
Temperature interval Time Temperature interval Time
1 24-28 2:11 105-101 1:28
2 29-33 1:27 100-96 1:17
3 34-38 1:39 95-91 1:11
4 39-43 1:22 90-86 1:11
5 44-48 2:28 85-81 1:45
6 49-53 2:31 80-76 1:40
7 54-58 3:14 75-71 2:21
8 59-63 6:50 70--65 2:06
9 64-68 7:01 65-61 3:40
10 69-73 9:33 60-56 3:35
11 74-78 5:52 55-51 8:00
12 79-83 5:23 50-46 9:33
13 84-88 4:23 45-41 17:08
14 89-93 6:26 40-36 36:47
15 94-99 9:00 35-31 32:27
16 100-105 11:09 30-24 24:11
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 400
5. EXPERIMENT UNDER THE SUN
Though the 100 watts incandescent bulb with a combination of yellow and red light mimics the sunlight spectrum,
there are many factors that affect the temperature which includes the humidity, consistency in ambient temperature etc.
So, we need to test out the setup in the natural environment to check whether the changes still exist. The experiment is
done during August 2017 on an open rooftop in Akkayyapalem, Visakhapatnam, Andhra Pradesh, India. The ambient
temperatures are recorded to be fluctuating from 280c to 340c during the time 10 A.M to 3 P.M. Initially the temperature
inside the control volume is nearly the same or matched with the ambient temperature, later as the module got heated up
and the temperature inside is raised to a maximum of 360c with a difference of 20c from the ambient temperature. As time
passed the ambient temperature decreased, the temperature in the box remained undisturbed for some time.
6. SEM ANALYSIS OF GRAPHENE COATED SURFACE
The graphene-paint coated aluminium surface is examined under scanning electron microscope and Fig. 9-12 are
images at different magnification.
Fig 9-12: SEM Images of Coating at various magnifications
The above Pictures reveals that there are formations of spherical structures (Spherical Morphology) with non uniform
grain size. Further, with variations of resolution, we can see the observation that there are lumps deposited in one place
and followed by small grain structures i.e. with less agglomeration. As this coating is done with a paintbrush and not with a
specific instrument through the surface seems to be uniform, it is not. Here various characteristics come into play that
includes the type of brush chosen, the quantity of the Graphene added, Weight: Volume ratio of Graphene: Paint, Number
of strokes.
7. OTHER PROPERTIES OF GRAPHENE COATED ALUMINIUM SHEET
Graphene coat on aluminium sheet not only increased the heat transfer but also the electrical properties are altered.
When the resistance of the normal aluminium sheet is measured by using Multi meter, it is around 1.1-1.2 ohms. But the
resistance is decreased to 0.8 ohms when one side is coated with graphene-paint mixture.
8. CONCLUSION
The aluminium box setup is much efficient in energy storage and conversion and can be used in solar based food
drying machines and can be used in other places where there is the inconsistency of heat generation but require a
consistent and distributed heat inside a control volume.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 401
9. REFERENCES
1. Ch. Jeon, Yh. Jeong, JJ. Seo, Material Properties of Graphene/Aluminium Metal Matrix Composites Fabricated by
Friction Stir process, IJPEM, 2014, 1235-1239.
2. A. A. Balandin, Thermal Properties of Graphene and Nanostructured Carbon Materials, NMAT, 2011, 569-581.
3. E. Pop, V. Varshey, A. K. Roy, Thermal Properties of Graphene: Fundamentals and Applications, MRS Bulletin,
2012, 1273-1281.
4. J. Wang, Z. Li, G. Fan, H. Pan, Reinforcement with Graphene Nano-Sheets in Aluminium Matrix Composites, Acta
Materialia, 2012, 594-597.
5. K. V. K. Reddy, Ch. Abhinav, Brief Review of Thermal Properties of Graphene-Aluminium Metal Matrix Composites,
IJAENT, 2016, 13-17.
6. A. Cao, Molecular dynamics Simulation study on heat transport in monolayer Graphene sheet with various
geometries, J. Appl. Phys, 2012, 111.
7. A. A. Balandin, S. Ghosh, W. Bao, Superior Thermal Conductivity of Single-Layer Graphene, Nano Lett, 2008, 902-
907.
8. A. A. Balandin, S. Ghosh, D. L. Nika, Extraordinary Thermal Conductivity of Graphene: Possible Applications in
Thermal Management, ECS Transactions, 2010, 63-71.
9. S. Ghosh, D. L. Nika, A. A. Balandin, Heat Conduction in Graphene: Experimental Study and Theoretical
Interpretation, NJP, 2009, 11.
10. S. Ghosh, W. Bao, D. L. Nika, A. A. Balandin, Dimensional Crossover of Thermal transport in few-layer Graphene,
NMAT, 2010, 555-564.
11. D. Singh, J. Y. Murthy, T. S. Fisher, Mechanism of Thermal Conductivity reduction in Few-Layer Graphene, J. Appl.
Phys, 2011, 110.
12. A. Alofi, G. P. Srivastava, Thermal Conductivity of Graphene and Graphite, PhysRevB, 2013, 115421-1-10.
13. M. M. Sadeghi, M. T. Pettes, Thermal Transport in Graphene, J. SSC, 2012, 1321-1330.
14. P. G. Klemens, D. F. Pedraza, Thermal Conductivity of Graphite in the basal Plane, 1993, 735-741.
15. V. Adamyan, V. Zavalniuk, Lattice Thermal conductivity of Graphene with Conventionally Isotopic Defects, PACS
numbers, 1-12.
16. S. Ghosh, I. Calizo, A. A. Balandin, Extremely high Thermal Conductivity of Graphene: Prospects for Thermal
Management Applications in nanoelectronic circuits.
17. J. K. Chen, I. S. Huang, Thermal Properties of Aluminium- Graphite by Powder Metallurgy, j.compositesb, 2013,
698-703.
18. J. D. Renteria, D. L. Nika, A. A. Balandin, Graphene Thermal Properties: Applications in Thermal management and
Energy Storage, Appl. Sci, 2014, 525-547.
19. S. Stankovich, D. A. Dikin, Graphene-based composite Materials, nature let 2006, 282-286.
20. S. Ghosh, A. A. Balandin, Thermal Properties of Graphene and Carbon-Based Materials: Prospects of Thermal
Management Applications, Mater. Res. Soc, 2011, 43-52.
21. S. Himran, R. Taraka, A. Duma, An Analysis on Thermal Energy Storage in Paraffin-Wax Using Tube Array on a
Shell and Tube Heat Exchanger, IJMAIMME, 2015, 1822-1829.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 402
22. C. Thirugnanam, P. Marimuthu, Experimental Analysis of Latent Heat Thermal Energy Storage Using Paraffin Wax
as Phase Change Material, IJEIT, 372-376.
23. V. K. Dwivedi, P. Tiwari, Sumit Tiwari, Importance of Phase Change Material in Solar Thermal Applications: A
review, IEEE.
24. M. V. Kulkarni, D. S. Deshmukh, Improving Efficiency of Solar Water Heater Using Phase Change Materials, IJSSBT,
2014, 39-44.
25. Heat Transfer Enhancement of paraffin wax using Graphite foam for Thermal Energy Storage, Solar Energy
Materials, 2010, 1011-1014.
26. TC. Ling, CS. Poon, Use of Phase Change Materials for Thermal Energy Storage in Concrete: An Overview,
Construction, and Building Materials, 2013, 55-62.
27. A. Gracia, L, Cabeza, Phase Change Materials and Thermal Energy storage for Building, Energy, and Buildings,
2015, 414-419.
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Applications, Elsevier, 2009, 318-345.
29. L. G. Socaciu, Thermal Energy Storage with Phase Change Material, LEJPT, 2012, 75-98.
10. ACKNOWLEDGEMENT
We sincerely express our gratitude to Dr. K. Subrahmanyam, Professor, Department of Mechanical engineering, RAGHU
Educational Institutions, Vishakhapatnam; Dr. R.S. Kiran, Professor, Department of Mechanical Engineering, Raghu
Educational Institutions, Vishakhapatnam; Dr. Vijaya Babu, Professor, Department of Mechanical Engineering, Andhra
University; Dr. k. Ramji, Professor, Department of Mechanical Engineering, Andhra University; Dr. R. P. VijayaLakshmi,
Professor, Department of Physics, Sri Venkateshwara University for assisting and guiding us throughout the analysis.
11. BIBLIOGRAPHY
K. Subramanyam is a professor in Raghu Engineering College and Co-Ordinator of Nano Technology Research Center,
Raghu Engineering College, Visakhapatnam. He published many papers related to NanoMaterials is various international
Journals. His research interests include Nano Materials, Dilute Magnetic Semiconductors, Composites, Catalysts and
Ceramic Materials.
K. Vamsi Krishna Reddy is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge
in Material Science, Thermal engineering, and Nano Technology through internships in Steel Plant, Visakhapatnam, and
NTPC, Visakhapatnam. He is an author of a research paper titled “Brief Review on Graphene-Aluminium Metal Matric
composites”. His areas of Interest include Heat Transfer and Nanotechnology.
Ch. Abhinav is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge in Material
Science and Nano Technology through an internship in Steel Plant, Visakhapatnam. He is an author of a research paper
titled “Brief Review on Graphene-Aluminium Metal Matric composites”. His areas of Interest include Material Science and
Nanotechnology.
G. Goutham Raju is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge in
Material Science through Internship in Steel Plant, Visakhapatnam. His areas of interest include Material Science and
Designing.

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Graphene-coated Al cuboid with PCMs

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 396 ExperimentalInvestigationofGraphenecoatedAlcuboidcrammedwithPCM`s forEfficientThermalEnergyStorageandConversion. Ch. Abhinav1, K. Vamsi Krishna Reddy2, G. Goutham Raju3, K. Subramanyam4 1,2,3B. Tech in Mechanical Engineering, Raghu Institute of Technology, JNTU Kakinada, Visakhapatnam, India. 4 Nano Technology Research laboratory, Raghu Engineering College, Visakhapatnam, India. -----------------------------------------------------------------------***-------------------------------------------------------------------- Abstract: In this paper, we report on the development of a composite cuboid (20x20x20/A cm3) which can absorb, store and supply heat consistently for longer periods even the heat source is turned off. The main frame of this composite cuboid is made up of aluminium, whose top surface which faces the heat source is coated with graphene. The hollow space inside the cuboid is filled with paraffin wax pellets for latent heat storage. This cuboid is placed inside an insulated thermocol box whose interior is concealed with reflective aluminium foil. a 100-watt incandescent bulb is used as a heat source. Due to the high thermal conductivity of graphene the thermal conductivity of the aluminium increases, resulting in the high amount of heat absorption. Heat is absorbed by the paraffin wax resulting in the phase change from solid to liquid. This latent heat storage liberates heat uniformly until the phase is altered to its original state. This resulted in a maximum temperature of 105°C in 80 minutes and took 148 min to reach room temperature (240c). In contrast, the normal aluminium box without coating and PCM reached a maximum temperature of 77°C in 30 min and a cooling time of 40 min. The results show that the usage of PCM’s decreased the rate of cooling and graphene coat increased the heat transfer through the surface. Key Words: Composites, Coating, Graphene, Latent Heat Storage, PCM`s. 1. INTRODUCTION Mankind has been highly reliant on fossil fuels which are being used in wide applications ranging from combustion engines to electricity. This unceasing usage of non-renewable resources from several decades led to the diminishing of existing fossil fuels and even led to increase of greenhouse gases. This problem can be solved either by using renewable resources or implementation of efficient energy storage systems. But, most of the renewable energy sources are not consistent round the clock. The intensity of the energy output from these renewable sources can sometimes reach more than requirement experience a sudden drop. Thus, energy storage systems play a crucial role in diminishing the gap between energy supply and energy usage. The heat energy can be stored in several types of materials as sensible heat or latent heat which results either in temperature rise or a change in phase. The energy stored in solid or liquid by raising its temperature is called sensible heat storage and heat storage acquired by a change in phase is called latent heat storage. Latent heat energy storage is efficient due to the reason that its ability to store and maintain heat at constant temperature. Properties like phase transition temperature and high latent heat of transition and good heat transfer need to be considered while selecting a PCM. In general paraffin wax (CH3-CH2-CH3) is used as PCM’s. The chain length of the paraffin wax can affect both melting point and latent heat of fission. Moreover, paraffin wax is less expensive, non-corrosive, predictable, safe and reliable. In most of the developed countries majority of the energy is consumed for conditioning air in the buildings to ensure indoor thermal comfort. This led to a surge in energy consumption and air pollution caused by the greenhouse gas emission. To increase the efficiency and decrease negative effects on the environment, energy storage systems are a great solution. In recent constructions of green buildings, microencapsulated Phase change materials are incorporated within concrete walls. This PCM’s in the concrete wall absorbs heat from the sun during the day maintaining the human thermal temperature at 23°c but during cooler nights PCM’s releases the stored heat and solidifies. In the same way, this storage module can increase the efficiency of heat exchangers, solar water heater, and food drying machines. Graphene is one of the very few materials with high thermal conductivity which ranges from (4.84 ± 0.44) x 103 to (5.30 ± 0.48) x 103 W/mK. Single layer graphene has higher thermal conductivity. The number of layers influences its thermal conductivity further, the thermal conductivity decreases from 2800 to 1300 W/mK with an increase in the number of the atomic planes from 2 to 4. Phonons are the reason behind its high thermal conductivity. On the other hand, graphene possesses high elastic properties. When graphene is reinforced with aluminium alloys the resultant metal matrix composites show high thermal conductivity than ordinary aluminium alloys. Moreover, the thermal conductivity of aluminium metal matrix composites increases by 15% at 250°C. These concepts of graphene and PCM’s are used in developing our composite cuboid. Graphene coating resulted in an increase in max temperature by 30o than the normal aluminium sheet. The addition of phase change material made the composite cuboid to store and supply heat for nearly four times the time than the regular metal.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 397 2. EXPERIMENTAL SETUP The experimental setup can be broadly classified into A. Aluminium box setup. B. Heating system. A. Aluminium box setup: - Aluminium sheet of 0.1cm thickness is used to make a tray of 20x20x4 cm3 (1600 cm3) by using tin smithy which has an opening at the top. This tray rests on a hollow box of dimensions 22x22x12 cm3 (5808 cm3) with the help of clamps on its inner edges closing the top side of the hollow box. This results in a decrease in volume of the hollow box from 5808 cm3 to 3872 cm3, which is the control volume and its temperature is recorded. As the size of the cuboid surface is large there is no available equipment for us to coat Graphene. So, the top surface of the cuboid box is coated with a mixture of black enamel paint and graphene powder. To ensure the uniformity, graphene powder is sieved while the paint is wet and the excess is dusted. Half of the empty space inside the cuboid box is filled with wax. Various view of the aluminium box setup is shown in figures 1-4 below. FIG.1-4: shows the box setup with hollow box and tray B. Heating system: - Heating system is further classified into 1) Heat Source. 2) Insulation. 3) Temperature measuring devices. A thermocol box of dimensions 30x34x40 cm3 (40800 cm3) is constructed whose interior is insulated with a white drawing chart which acts as an insulator and protects the thermocol from melting. This chart is covered with Aluminium foil to ensure there is no heat loss, most of the heat stays inside the thermocol box. A 100W incandescent tungsten filament bulb is used as a heat source at 220V AC power source and to record the temperature inside the control volume a K-type thermocouple is installed which records the temperature change throughout the process. Various view of the setup is shown in Fig. 5-8 below.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 398 FIG. 5-8 shows the heating system FIG. 7 shows the graphene-coated lid inside heating system Temperature representations:  The temperature inside the control volume: T1.  The temperature outside the control volume (Outside the aluminium box and inside the thermocol box): T2. 3. EXPERIMENT The aluminium box setup is placed inside the thermocol box and its lid is closed. The initial temperature of the setup is recorded. Though our ultimate result of the setup coated with Graphene and filled with PCM is the main goal, we wanted to do a comparative analysis hence, we experimented with four variations as shown in table 1 below. Table 1: Experiment Variations Expt. No. Box Material Aluminium box setup PCM Graphene + Paint Mixture 1 Aluminium  - - 2 Aluminium  -  3 Aluminium   - 4 Aluminium    For all the experiments initially, the heat source is turned on and the setup is heated until it reaches a steady maximum temperature and is recorded, Later the source is turned off and the time taken to reach the room temperature is also recorded. Here the temperature inside the control volume i: e T1 is considered as mainly notable. 4. EXPERIMENTAL RESULTS Exp. No.1 (Only the Aluminium Box Setup):- It took nearly 30 minutes to reach a maximum temperature of 770c T1. In just 14 minutes the temperature has raised to 500c from 220c (room temperature). The rise in temperature is quick till it reached 500c, later it took 16 minutes
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 399 for a 270c rise from 500c to 770c. When the source is turned off, it took 40 minutes to get back to room temperature from saturated temperature. Exp. No.2 (Top Surface of Cuboid Coated with Graphene Paint Mixture):- When the top surface is coated with graphene, the maximum temperature reached is around 850c. It took 35 minutes to reach the maximum temperature and the rise in temperature was very quick from 220c to 770c later the time taken for every degree rise is increased. When the source is turned off, it took 55 minutes to reach the room temperature. In general, the temperature inside the control volume of coated setup is 40c-80c more when compared to normal aluminium setup. For instance, if T2 is 400C thenT1 (without graphene coat) is 240C and inside the graphene-coated one is 280C (T1), When T2 is 600c, the inner temperature is around 300c for noncoated one and is 360c for coated one. Exp. No.3 (Hollow space filled with PCM without Graphene coat):- This experiment is subdivided into two parts based on the PCM`s. Half of the hollow space is filled with PCM`s. In the first part, we smashed a household candle and in the second experiment, we used wax pellets from the chemical store. In both the experiments we heated for 40 minutes which resulted in a temperature of 770c raised from 210c (room temperature). But, in the previous experiments, the time taken to reach 770c is around 30 minutes. This is due to the reason that, the heat supplied is absorbed by wax present in the hollow space. Then the heat source is turned off. In the case of candle wax, it took 80 minutes to reach the room temperature. On the other hand, it took nearly 134 minutes to reach room temperature when candle wax is replaced with wax pellets. This may be due to the small size and purity of wax pellets. In both experiments the temperature fall from 770c to 400c is very fast, it took around 1-2 minutes. This is a stunner that even degree temperatures stayed for a long time than the odd temperatures; 360c (2m 8s), 340c (3m 30s), 320c (10m 30s), 300c (23m), 280c (24m) and so-on. In contrast, the odd temperatures; like 390c, 370c, 350c, 330c stayed for lesser than 30s. There are also similarities with the previous experiments like a sharp decrease in temperature from 770c to 400c and 55 minutes for 400c to 300c. Further, the time still increased for the fall of temperature from 300c to 220c. Exp. No.4(Complete setup): - In this experiment, the top layer of the cuboid is coated with graphene-paint mixture and graphene powder is sieved over the wet paint surface 3 times to ensure a uniform surface. The half of the hollow space of the cuboid is filled with wax pellets. The total time taken to reach the maximum temperature is 80 minutes and the maximum temperature is 1050c. We can observe from the readings below that there is a gradual decrease in time from 240c to 430c, later the time has increased gradually reaching a peak of 9:33 minutes for 69-73 degrees rise. Further, the time followed a similar pattern to that of previous intervals reaching a maximum time of 11:09 minutes for the 100-105 interval. All Intervals and their time patterns are given in table 2 below. Table 2: Heating and Cooling patterns. S.no Heating Cooling Temperature interval Time Temperature interval Time 1 24-28 2:11 105-101 1:28 2 29-33 1:27 100-96 1:17 3 34-38 1:39 95-91 1:11 4 39-43 1:22 90-86 1:11 5 44-48 2:28 85-81 1:45 6 49-53 2:31 80-76 1:40 7 54-58 3:14 75-71 2:21 8 59-63 6:50 70--65 2:06 9 64-68 7:01 65-61 3:40 10 69-73 9:33 60-56 3:35 11 74-78 5:52 55-51 8:00 12 79-83 5:23 50-46 9:33 13 84-88 4:23 45-41 17:08 14 89-93 6:26 40-36 36:47 15 94-99 9:00 35-31 32:27 16 100-105 11:09 30-24 24:11
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 400 5. EXPERIMENT UNDER THE SUN Though the 100 watts incandescent bulb with a combination of yellow and red light mimics the sunlight spectrum, there are many factors that affect the temperature which includes the humidity, consistency in ambient temperature etc. So, we need to test out the setup in the natural environment to check whether the changes still exist. The experiment is done during August 2017 on an open rooftop in Akkayyapalem, Visakhapatnam, Andhra Pradesh, India. The ambient temperatures are recorded to be fluctuating from 280c to 340c during the time 10 A.M to 3 P.M. Initially the temperature inside the control volume is nearly the same or matched with the ambient temperature, later as the module got heated up and the temperature inside is raised to a maximum of 360c with a difference of 20c from the ambient temperature. As time passed the ambient temperature decreased, the temperature in the box remained undisturbed for some time. 6. SEM ANALYSIS OF GRAPHENE COATED SURFACE The graphene-paint coated aluminium surface is examined under scanning electron microscope and Fig. 9-12 are images at different magnification. Fig 9-12: SEM Images of Coating at various magnifications The above Pictures reveals that there are formations of spherical structures (Spherical Morphology) with non uniform grain size. Further, with variations of resolution, we can see the observation that there are lumps deposited in one place and followed by small grain structures i.e. with less agglomeration. As this coating is done with a paintbrush and not with a specific instrument through the surface seems to be uniform, it is not. Here various characteristics come into play that includes the type of brush chosen, the quantity of the Graphene added, Weight: Volume ratio of Graphene: Paint, Number of strokes. 7. OTHER PROPERTIES OF GRAPHENE COATED ALUMINIUM SHEET Graphene coat on aluminium sheet not only increased the heat transfer but also the electrical properties are altered. When the resistance of the normal aluminium sheet is measured by using Multi meter, it is around 1.1-1.2 ohms. But the resistance is decreased to 0.8 ohms when one side is coated with graphene-paint mixture. 8. CONCLUSION The aluminium box setup is much efficient in energy storage and conversion and can be used in solar based food drying machines and can be used in other places where there is the inconsistency of heat generation but require a consistent and distributed heat inside a control volume.
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 401 9. REFERENCES 1. Ch. Jeon, Yh. Jeong, JJ. Seo, Material Properties of Graphene/Aluminium Metal Matrix Composites Fabricated by Friction Stir process, IJPEM, 2014, 1235-1239. 2. A. A. Balandin, Thermal Properties of Graphene and Nanostructured Carbon Materials, NMAT, 2011, 569-581. 3. E. Pop, V. Varshey, A. K. Roy, Thermal Properties of Graphene: Fundamentals and Applications, MRS Bulletin, 2012, 1273-1281. 4. J. Wang, Z. Li, G. Fan, H. Pan, Reinforcement with Graphene Nano-Sheets in Aluminium Matrix Composites, Acta Materialia, 2012, 594-597. 5. K. V. K. Reddy, Ch. Abhinav, Brief Review of Thermal Properties of Graphene-Aluminium Metal Matrix Composites, IJAENT, 2016, 13-17. 6. A. Cao, Molecular dynamics Simulation study on heat transport in monolayer Graphene sheet with various geometries, J. Appl. Phys, 2012, 111. 7. A. A. Balandin, S. Ghosh, W. Bao, Superior Thermal Conductivity of Single-Layer Graphene, Nano Lett, 2008, 902- 907. 8. A. A. Balandin, S. Ghosh, D. L. Nika, Extraordinary Thermal Conductivity of Graphene: Possible Applications in Thermal Management, ECS Transactions, 2010, 63-71. 9. S. Ghosh, D. L. Nika, A. A. Balandin, Heat Conduction in Graphene: Experimental Study and Theoretical Interpretation, NJP, 2009, 11. 10. S. Ghosh, W. Bao, D. L. Nika, A. A. Balandin, Dimensional Crossover of Thermal transport in few-layer Graphene, NMAT, 2010, 555-564. 11. D. Singh, J. Y. Murthy, T. S. Fisher, Mechanism of Thermal Conductivity reduction in Few-Layer Graphene, J. Appl. Phys, 2011, 110. 12. A. Alofi, G. P. Srivastava, Thermal Conductivity of Graphene and Graphite, PhysRevB, 2013, 115421-1-10. 13. M. M. Sadeghi, M. T. Pettes, Thermal Transport in Graphene, J. SSC, 2012, 1321-1330. 14. P. G. Klemens, D. F. Pedraza, Thermal Conductivity of Graphite in the basal Plane, 1993, 735-741. 15. V. Adamyan, V. Zavalniuk, Lattice Thermal conductivity of Graphene with Conventionally Isotopic Defects, PACS numbers, 1-12. 16. S. Ghosh, I. Calizo, A. A. Balandin, Extremely high Thermal Conductivity of Graphene: Prospects for Thermal Management Applications in nanoelectronic circuits. 17. J. K. Chen, I. S. Huang, Thermal Properties of Aluminium- Graphite by Powder Metallurgy, j.compositesb, 2013, 698-703. 18. J. D. Renteria, D. L. Nika, A. A. Balandin, Graphene Thermal Properties: Applications in Thermal management and Energy Storage, Appl. Sci, 2014, 525-547. 19. S. Stankovich, D. A. Dikin, Graphene-based composite Materials, nature let 2006, 282-286. 20. S. Ghosh, A. A. Balandin, Thermal Properties of Graphene and Carbon-Based Materials: Prospects of Thermal Management Applications, Mater. Res. Soc, 2011, 43-52. 21. S. Himran, R. Taraka, A. Duma, An Analysis on Thermal Energy Storage in Paraffin-Wax Using Tube Array on a Shell and Tube Heat Exchanger, IJMAIMME, 2015, 1822-1829.
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 402 22. C. Thirugnanam, P. Marimuthu, Experimental Analysis of Latent Heat Thermal Energy Storage Using Paraffin Wax as Phase Change Material, IJEIT, 372-376. 23. V. K. Dwivedi, P. Tiwari, Sumit Tiwari, Importance of Phase Change Material in Solar Thermal Applications: A review, IEEE. 24. M. V. Kulkarni, D. S. Deshmukh, Improving Efficiency of Solar Water Heater Using Phase Change Materials, IJSSBT, 2014, 39-44. 25. Heat Transfer Enhancement of paraffin wax using Graphite foam for Thermal Energy Storage, Solar Energy Materials, 2010, 1011-1014. 26. TC. Ling, CS. Poon, Use of Phase Change Materials for Thermal Energy Storage in Concrete: An Overview, Construction, and Building Materials, 2013, 55-62. 27. A. Gracia, L, Cabeza, Phase Change Materials and Thermal Energy storage for Building, Energy, and Buildings, 2015, 414-419. 28. A. Sharma, V. V. Tyagi, C. R. Chen, D. Buddhi, Review on thermal energy storage with Phase Change Materials and Applications, Elsevier, 2009, 318-345. 29. L. G. Socaciu, Thermal Energy Storage with Phase Change Material, LEJPT, 2012, 75-98. 10. ACKNOWLEDGEMENT We sincerely express our gratitude to Dr. K. Subrahmanyam, Professor, Department of Mechanical engineering, RAGHU Educational Institutions, Vishakhapatnam; Dr. R.S. Kiran, Professor, Department of Mechanical Engineering, Raghu Educational Institutions, Vishakhapatnam; Dr. Vijaya Babu, Professor, Department of Mechanical Engineering, Andhra University; Dr. k. Ramji, Professor, Department of Mechanical Engineering, Andhra University; Dr. R. P. VijayaLakshmi, Professor, Department of Physics, Sri Venkateshwara University for assisting and guiding us throughout the analysis. 11. BIBLIOGRAPHY K. Subramanyam is a professor in Raghu Engineering College and Co-Ordinator of Nano Technology Research Center, Raghu Engineering College, Visakhapatnam. He published many papers related to NanoMaterials is various international Journals. His research interests include Nano Materials, Dilute Magnetic Semiconductors, Composites, Catalysts and Ceramic Materials. K. Vamsi Krishna Reddy is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge in Material Science, Thermal engineering, and Nano Technology through internships in Steel Plant, Visakhapatnam, and NTPC, Visakhapatnam. He is an author of a research paper titled “Brief Review on Graphene-Aluminium Metal Matric composites”. His areas of Interest include Heat Transfer and Nanotechnology. Ch. Abhinav is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge in Material Science and Nano Technology through an internship in Steel Plant, Visakhapatnam. He is an author of a research paper titled “Brief Review on Graphene-Aluminium Metal Matric composites”. His areas of Interest include Material Science and Nanotechnology. G. Goutham Raju is a recent Graduate Mechanical Engineer from JNTU Kakinada. He gained adequate knowledge in Material Science through Internship in Steel Plant, Visakhapatnam. His areas of interest include Material Science and Designing.