0% found this document useful (0 votes)
87 views7 pages

52 - Paper ID IJ60606050

52_Paper ID IJ60606050

Uploaded by

reifer
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
0% found this document useful (0 votes)
87 views7 pages

52 - Paper ID IJ60606050

52_Paper ID IJ60606050

Uploaded by

reifer
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 7

ISSN(Online) : 2319-8753

ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

Modeling and Analysis of Temperature


Distribution in the Industrial Gas Fired
Powder Coating Oven using Computational
Fluid Dynamic (CFD)
Vaibhav C. Dhanuskar1, Pramod R. Pachghare2
P.G. Student, Dept. of Mechanical Engineering, Govt. College of Engineering, Amravati, Maharashtra, India1
Asst. Professor, Dept. of Mechanical Engineering, Govt. College of Engineering, Amravati, Maharashtra, India2

ABSTRACT: In this paper, study focused on the modeling and analysis of temperature distribution in the industrial gas
fired powder coating oven having dimension of 2700 x 1900 x 2700 mm3 is analyzed using Computational Fluid
Dynamic (CFD). The CFD analysis of existing oven with few modifications in geometry is done to achieve uniform
temperature distribution. For CFD analysis ANSYS 14.5 is used. This study is particularly focused on the variations of
pressure and temperature inside the oven. With the existing geometry of the oven, it is found that there is non-uniform
temperature distribution inside the oven. Therefore, the geometry of an oven is modified. The Inlet opening to the oven is
made adjacent to the bottom of the oven and inlet to oven through the perforated bottom. From the result, it is cleared
that the inlet to the oven from slit adjacent to bottom and perforated bottom inlet shows uniform temperature distribution
in the oven.

I. INTRODUCTION

Now a days, powder coating technology is used for engineering components to improve the life and surface
finish of the components. Coating is a process of covering a surface of objects, called as substrate. The purpose of
coating may be functional, decorative or both. The two important types of coating are [1]: Liquid coating technology
(wet), which has been used for more than two centuries and Powder coating technology (dry), which has been used in
Industries for some 30 years. The use of Powder Coating technology has been increased tremendously in recent years
due to its relatively high performance over liquid coating technology. Various types of equipment are available for
powder coating to small and large end users. The parts which need to be coated are grounded neutral so that the particles
projected from spray gun can adhere to the parts and are held there until curing process is done in the oven [2]. The result
is a uniform, durable, high-quality finish. The present analysis of oven is done at GUKSS Industries, Amravati. The
geometry of gas fired convection oven is made and boundary conditions are analyzed. The problem in the oven at
GUKSS Industries is uneven distribution of temperature. The CFD analysis is done to achieve uniform temperature
distribution throughout the oven.
In 2003, Nantawan Therdthai et al. [3] suggested to modify the oven configuration for better heat distribution and
provided constructive information to achieve the optimum baking temperature profile by manipulating energy supply
and airflow pattern. Zinedine Khatir et al. [4] have studied the application of computational fluid dynamics (CFD) and
oven design optimization and reduce the effective baking time and hence improve the energy efficiency of the process.
Pumphruk Satithave [5] analyzed CFD modeling and validation of temperature distribution in the IR oven and found that
IR oven has better efficiency than the other traditional convection oven particularly for large objects having high
emissivity.

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10503


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

II. CFD MODELING AND SIMULATION

2.1. Oven geometry


The dimensions of the industrial oven are a length of 270 cm, a width of 190 cm and a height of 270 cm. There is one
burner which is situated in the centre of the top of the oven which has been designed to generate hot air from the
combustion of natural gas. The hot air is then circulated through the supply duct by the air circulation fan and into the
heating chamber. After the hot air has passed through the heating chamber, it then returns to the burner to be reheated,
and finally back into the supply duct via a recirculation fan located on top of oven. The whole oven is surrounded by
insulation made of glass wool, which is 10 cm thick. This is to stop the heat escaping to the atmosphere and make the
oven more efficient. Modeling assumptions are taken into consideration and simplified geometries of oven with proposed
modification are made in ICEM 14.5 as shown in Figure 2.1.

Figure 2.1:(a) Geometry of existing setup, (b) Geometry with position variation of Inlet Slit,
(c) Geometry with inlet through perforated bottom
2.2. Modeling assumption
A three-dimensional model of oven is taken as the calculation domain. As the oven has a recirculation fan installed, the
flow inside the ducts would not be of laminar flow. This fan will cause the air in the oven to be influenced by forced
convection. Since the 3-D model is chosen, gravity is considered therefore natural convection is also included. Creating

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10504


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

the recirculation fan in a 3-D geometry is difficult to model because Fluent would not recognize that the flow could
circulate so some modifications to the geometry were made. In order to overcome this problem, it is assumed that the air
would exist in the system where it was drawn into the fan and enter through the supply duct. The fan inside the oven is
represented with the pressure outlet and inlet which creates flow of air.

2.3. Boundary Conditions


Boundary conditions are a very important aspect of modeling in Fluent. There are four types of boundary conditions
affecting the oven; they are pressure inlet, pressure outlet, temperature inlet and wall properties. To represent the burner
in oven, an inlet condition with a specified temperature that corresponds to the burner is chosen. By choosing this type of
condition it enabled the heat to affect the cooler air exiting the heating chamber. As the fan was removed from the oven
geometry the pressure difference created by the fan was modeled using the pressure inlet and outlet. The values for these
boundary conditions are shown in Table 2.1

Table 2.1: Boundary Conditions for Inlets and Outlets


Boundary Name Boundary Type Temp (°K) Pressure (Pa) Turbulence type
Inlet_Left Pressure inlet 500 150 k-ε
Inlet_Right Pressure inlet 500 141 k-ε
Outlet Pressure outlet 300 310 k-ε

Since the conditions during operation are not known for the steel wall and bottom, they were modeled as solid faces with
the material property steel.

2.4. Material Properties


There are three types of materials that data is required in order to model the oven using Fluent. They are the heated air,
the insulation, and the steel inside the oven. The Table 2.2 shows the material properties.

Table 2.2: Material properties used in the oven calculations


Material Density (kg/m3 ) Cp (J/Kg K) Thermal Conductivity (W/m k)
Air 0.552 1053 0.04395
Insulation 80 1200 0.11
Steel 7801 473 43

2.5. Generation of Mesh


Geometry is created to represent the boundaries and fluid domain for analysis. This geometry is created in 3-D using
workbench ICEM 14.5.Once all the critical points are placed, they are joined together by lines to create the edges of the
oven geometry (insulation, bottom, inlets and outlets, curves). From these edges and faces are created which represents
the fluid domain (air inside the oven). The next step in the creation of the geometry is to generate the mesh on edges and
faces. ICEM 14.5 offers many choices with regards to the number of nodes on the edges either by giving the number of
nodes or the spacing between the nodes. In this instance, the structured rectangular type of meshing is used to generate
mesh. The total numbers of nodes generated are 1472086.Now the generated mesh is converted to unstructured mesh and
then 3-D mesh is exported to Fluent.
2.6. Flow Equations
To analyze the air flow inside the oven correctly, the correct model needs to be chosen. Since there is a recirculation of
the gases inside the oven due to the fan, turbulent flow is predicted. The models used in Fluent for turbulence are two-
equation turbulence models or the Reynolds stress model. The standard two-equation (k-ε) model has been chosen to
carry out the analysis on the oven as it is reasonably accurate over a wide range of turbulent flow [6].
2.6.1. Mass Conservation
The conservation of mass or continuity equation is given by:
+ ρ = 0………………..…………………………………………..……………………………..………….……………..................................... 2.1

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10505


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

2.6.2. Momentum Conservation


The conservation of momentum otherwise known as the Navier-Stokes equation which is given by:
ρ ρ τ
+ =− + + ρ + Fi……..………..………………...………………………….………………………….……….……………...........2.2
Where p is the static pressure,τ is the stress tensor described by equation following equation (2.3). ρ is the gravitational
body forces and Fi are the external body forces.
The stress tensor "τ " , is given by
τ = [μ( + )] − µ δ ……………..…..…………..……………………………………………………….…….….…..………….….….…….....2.3
where μ is the molecular viscosity and δij is the effect of volume dilation.
2.6.3. Conservation of Energy
The energy conservation equation is needed to solve for the temperature and the heat transfer which is given by
μ
(ρ ) + ρ = k+ + + (τ )eff + S ……………………..………….……………………………………….....2.4
Where h is the sensible enthalpy, k is the molecular conductivity, τ is the deviatoric stress sensor, µt is the turbulent
viscosity and P is the turbulent Prandtl number for temperature or enthalpy.

III. RESULT AND DISCUSSION

The results obtained for the existing boundary condition and geometry modification are explained below.
3.1. Oven at Existing Boundary Condition
The results of CFD analysis of the industrial oven for existing setup are obtained. The boundary conditions at which the
analysis is carried out are as shown in the Table 3.1.

Table 3.1: Boundary conditions for existing oven


Boundary Name Boundary Type Temperature (oK) Pressure (Pa)
Inlet_Left Pressure Inlet 500 150
Inlet_Right Pressure Inlet 500 141

Figure 3.1: Contours of temperature distribution in the oven for existing boundary conditions

From the Figure 3.1, it is observed that the temperature near the bottom of the oven is around 495 oK-500 oK. This is due
to the fact that, the inlet slits to the oven are at some height from the bottom, the region is developed where almost

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10506


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

stagnation condition occurred. The temperature goes on reducing in the upward direction of oven. At the top right corner,
the temperature is much lower than the oven surrounding which is 450 oK. The results obtained from the CFD analysis
are significantly equivalent to the TTR done prior to the problem identification.

3.2. Effect of Position Variation of Inlet Slit


The boundary conditions at which the analysis is carried out are as shown in Table 3.2.

Table 3.2: Boundary conditions for oven at slit position adjacent to the bottom
Boundary Name Boundary Type Temperature (oK) Pressure (Pa)
Inlet_Left Pressure Inlet 490 130
Inlet_Right Pressure Inlet 490 130

Figure 3.2: Contours of Temperature Distribution for oven at slit position adjacent to the bottom

The results of CFD analysis of the oven by varying the position of Inlet slits adjacent to bottom of oven are obtained.
With this geometry modification, the temperature contours obtained from the CFD analysis shows that the temperature
inside the oven ranges in between 488oK to 490 oK. which is the specified range of operation. From this it is concluded
that maintaining constant pressure on both the left and right inlet with slit inlets adjacent to the bottom, the uniform
temperature can be achieved throughout the oven as shown in Figure 3.2

3.3. Effect of Using Perforated Inlet through Bottom of oven


The boundary conditions at which the analysis is carried out are as shown in the Table 3.3.

Table 3.3: Boundary conditions for oven using Perforated Inlet through Bottom
Boundary Name Boundary Type Temperature (oK) Pressure (Pa)
Inlet_Left Pressure Inlet 480 130
Inlet_Right Pressure Inlet 480 130

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10507


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

Figure 3.3: Contours of Temperature Distribution through Perforated Inlet

Figure 3.3 shows the CFD analysis for the oven with inlet through the perforated bottom. The temperature contours
shows uniform temperature distribution inside the oven. Temperature varies in very narrow range of 488 oK to 490 oK.
The distribution of temperature contours is as shown in Figure 3.3.

IV. CONCLUSION

The modeling and analysis of temperature distribution for gas fired convection oven at GUKSS Industries is carried out
by using CFD analysis. From the results obtained it is concluded that:
1. At existing shape and boundary condition, there is problem of non uniform temperature distribution in the oven.
In particular, the area near bottom of oven is overheated due to the stagnation of hot inlet air. The geometry
modification done to achieve uniform temperature distribution in the oven are having air entry to oven through
inlet slit adjacent to bottom and using perforated inlet through bottom.
2. From the CFD analysis of modified geometry, the uniform temperature distribution is obtained throughout the
oven section. The range of temperature variation is limited to ± 2 oK. This results in considerable saving in both
power and time.

Nomenclature Density (Kg m-3)


qk Amount of heat transferred by conduction (W) Gr Grashof Number (-)
k Thermal conductivity of the medium (W m-1 K-1) µ Dynamic Viscosity (Kg m-1 s-1)
A Area through which the heat is transferred (m2) Cp Specific Heat at Constant Pressure (J Kg-1 K-1)
dT
Temperature gradient normal to the area (k/m) α Thermal Diffusivity (m2 s-1)
dx
p Static pressure (N/m2)
qc Amount of heat transferred by convection (W)
τij Stress tensor (N m-2)
hc Average convection heat transfer coefficient
ρgi Gravitational body forces (N)
(W m-2 k-1)
ΔT Temperature Difference =(Ts − T∞) (K) Fi External body forces (N)
g Acceleration due to gravity (m s-2) h Sensible enthalpy (J)
β Coefficient of expansion (K-1) τ Deviatoric stress ensor (N m-2)
L Characteristic length (m) Prt Turbulent Prandtl number for temperature. (-)
ν Kinematic Viscosity (m2 s-1) µt Turbulent Viscosity (Kg m-1 s-1)
Pr Prandtl Number (-) τ Shear Stress (N m-2)
Nu Nusselt Number (-)

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10508


ISSN(Online) : 2319-8753
ISSN (Print) : 2347-6710

International Journal of Innovative Research in Science,


Engineering and Technology
(An ISO 3297: 2007 Certified Organization)

Website: www.ijirset.com
Vol. 6, Issue 6, June 2017

REFERENCES

[1]. “Complete Guide To Powder Coatings”, World Leader In Powder Technology,/Issue1, Nov 1999.
[2]. “Understanding gas fired convection curing equipment for powder coating”, Rodger Talbert, Powder Coating, (Nov 1994),35-41.
[3]. “Two-dimensional CFD modeling and simulation of an industrial continuous bread baking oven”, Nantawan Therdthai et al,/ Journal of Food
Engineering 60 (2003), 211–217.
[4]. “The Application of Computational Fluid Dynamics (CFD) And Oven Design Optimization In The British Bread-baking Industry”, Zinedine Khatir
et al,/ 8th International Conference on CFD in Oil & Gas, Metallurgical and Process Industries SINTEF/NTNU, Trondheim Norway, 21-23 June 2011.
[5]. “Computational Fluid Dynamic (CFD) Modeling and Validation of Temperature Distribution in the Infrared Oven”, Pumphruk Satit,/ School of
Engineering and Physical Sciences, Heriot-Watt University, Edinburgh, UK.
[6]. “Numerical Investigation of the Temperature Distribution in an Industrial Oven”, Andrew Lee,/ University of Southern Queensland.
[7]. “Assessment of simplified thermal radiation models for engineering calculations in natural gas-fired furnace”, D.A. Kontogeorgos et al,/
International Journal of Heat and Mass Transfer 50 (2007), 5260–5268.
[8]. “Concept of Computational Fluid Dynamics (CFD) and its Applications in Food Processing Equipment Design”, Pragati Kaushal and Sharma HK,/
Journal of Food Process Technology, Volume 3 Issue 1,2012.
[9]. “The Powder Coaters Manual”, Roger Talbert,/pg 1-98.

Copyright to IJIRSET DOI:10.15680/IJIRSET.2017.0606052 10509

You might also like