gyeongsang national university hanshik chung. contents background of study introduction &...
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Basic Designing of Mechanical Vapor Compressor in Multi-Effect Distillation for Fresh Water Production
Gyeongsang National UniversityHanshik Chung
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CONTENTS
Background of Study
Introduction & Objective
Results and discussion
Conclusions
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Fresh Water Generation System ;
(Phase-change)
(Single-Phase)
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Why and What is MED ?
• MSF ( Multi Stage Flash Desalination )
•MED ( Multi Effect Desalination )
(1) MED-TVC : MED by TVC (Thermo Vapor Compressor)
(2) MED-MVC : MED by MVC (Mechanical Vapor Compressor)
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MVC and MED System
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Mechanical vapor compressor design.
Assumptions and Simulation Conditions• Steady state conditions • 3D periodic model with CFD software package (CFX 12)• To reduce the computational cost, only single passage• 119,291 nodes and 613,893 elements
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NUMERICAL MODELING
3-Grid computational domain
The inlet boundary conditions;• Subsonic inlet, temperature and total pressure• The turbulence intensity : 5%.• Periodic boundary conditions were applied • Blade hub and shroud : adiabatic walls.
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Governing Equation• 3-D Reynolds averaged compressible Navier-Stokes equations• SST k-ω turbulence model
(1) 0
ii
ux
(2) 3
2
3
2
ijl
lt
i
j
j
it
jl
lij
i
j
j
i
jiji
i x
uk
x
u
x
u
xx
u
x
u
x
u
x
p
x
puu
x
(3) ])[()()( *
jtk
jj
iijj
j x
k
xk
x
ukU
xk
t
(4) 1
)1(2])[()()( 1*
jjjtk
jj
iijj
j xx
kF
x
k
xk
x
ukU
xk
t
Mass and momentum conservation equations
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Number of rotor blades @ each stage 14Number of stator blades 15
Diameter impeller 1 Inside : 282 mmOutside : 750 mm
Diameter impeller 2Inside: 298 mm
Outside : 792 mm
Diameter guide vaneInside : 298 mm
Outside : 792 mmBasic rotating speed 3650 rpm
Total pressure @ inlet 24.1 kPaSpecific enthalpy @ inlet 2.62×106J /kgSpecific entropy @ inlet 7.84 ×103 J /kg.K
Static temperature @ inlet 64.1oC
Details of geometry and flow condition in inlet
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Fluid properties
SETTING TYPE
Inlet Total pressure, total temperature
OutletAverage static pressureMass flow out
Interface Models Frozen Rotor
Blade Heat transfer adiabaticMass and Momentum no slip wallWall roughness smooth wall
PROPERTY VALUE
Molar mass 18.015 kg/kmol
Critical Volume 55.95 cm3/mol
Critical Temperature647.14 K
Critical Pressure 220.64 bar
Boiling temperature 64.1o C
Acentric Factor0.344
Properties of saturated steam. Boundary conditions.
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RESULTS AND DISCUSSION
Inlet mass flow rate (kg/s)
0.0 0.2 0.4 0.6
Pre
ssu
re r
atio
1.10
1.15
1.20
1.25
1.30
1.35
3000 rpm3650 rpm4000 rpm4500 rpm5000 rpm
Compressors performance map at various rotational speeds.
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Inlet mass flow rate (kg/s)
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7
t-t i
sent
ropi
c ef
ficie
ncy
0.45
0.50
0.55
0.60
0.65
0.70
0.75
0.80
0.85
3000 rpm3650 rpm4000 rpm
4500 rpm5000 rpm
Mass flow rates and efficiencies for various Rotational speeds.
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Outlet temperature (K)
350 360 370 380 390
Dis
char
ge p
ress
ure
(kP
a)
25
26
27
28
29
30
31
32
3000 rpm3650 rpm4000 rpm4500 rpm5000 rpm
.Temperature and discharge pressure at various rotational speeds.
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0
10
20
30
40
50
60
0.0
0.2
0.4
0.6
0.8
1.0
0.00.2
0.40.6
0.8
velo
city
guide vane blade
PS
SS
Hub
Shroud
0
10
20
30
40
50
60
70
0.0
0.2
0.4
0.6
0.8
1.0
0.00.2
0.40.6
0.81.0
velo
city
impeller stage 2
PS
SS
Hub
Shroud
0
20
40
60
80
0.0
0.2
0.4
0.6
0.8
1.0
0.00.2
0.40.6
0.81.0
velo
city
impeller stage 1
PS
SS
Hub
Shroud
(a) (b)
(c)
Flow field at blade in blade passage at (a) 16.6%, (b) 50%, and (c) 83.3%
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Contour of static entropy and plot of velocity vector for 4500 rpm rotational speed at low suction mass flow rate.
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Three-dimensional flow structure in flow passage (a, b, and c) and blade loading at rotor and stator at low suction mass flow rate.
(a) (b)
(c)
(d)
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CONCLUSION
• The effects of various operating conditions on the compressor performance have been investigated.
At a high discharge pressure, the blockage effect was very dominant, restricting the flow rate.
• A detailed flow analysis was performed in this simulation, along with an examination of secondary phenomena.
• The results clearly show the flow characteristics inside the compressor under different operating conditions.
• This simulation showed that the widest stable operating zone was located at a high rotational speed.
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