Agitator Design
Short Description
Agitator Design...
Description
Project :
PEDC
Design Calculations for : Calc by N M Patel Checked by
500 KL SS Storage Tank
Job No. Date Date
22/11/10
DESIGN OF 500 KL SS STORAGE TANK QTY.
3
Design Calculation No:
FZD- 01
DATA Sr
Parameter
Nom
Unit
Value
1 Content
Ethylene glycol
2 Working Capacity
VL
KL/MT
15
3 Vessel Diameter
D
M
2.6
4 Height
H
M
2.9
5 Specific Gravity
G
6 Corrosion Allowance
C
1.2 mm
0
7 MOC
SS 316
8 Viscosity
u
9 Ratio ,H/D
Ni
CP
30 1.12
10 Sweep Diameter
Da
M
0.9
11 TIP Speed
Ts
M/s
2
12 Blade type
3 Bladed pitch turbine
13 Nos of Blade
Nb
14 Distance Between Impeller
Si
3 M
1.3
15 Ratio of Si/Da
1.50
17 Type of impeller 16 Nos of impeller
multiimpeller
17 Type of Seal
Mechanical seal LS
M
3.4
19 Weight of 1st impeller
W a1
Kg
18
20 Weight of 2nd impeller
W a2
Kg
18
18 Length of Shaft
18
Page 1 of 9
Nos of Impeller =
2 3
1 Speed of impeller:
N=
Where Da = Sweep Diameter,M
60 τ S
= D/3
ΠD a N=
44.1 33.0
RPM
2 Pumping Rate, Q in M3/sec
Q=N Q ND
a3
Q=
Impeller Type Nos of Baffles Propeller 0 Propeller 3 to 8 Turbine,VT blade 0 Turbine,VT blade 4 Pitch Turbine,45◦ 0 Pitch Turbine,45◦ 4 Anchor 0
0.9 Np 0.3 0.33 -0.37 0.93 -1.08 3 to 5 0.7 1.3-1.4 0.28
Where NQ = Pumping Number
12.9
NQ 0.3 0.4-0.55 0.33-0.34 0.7-0.85 0.3 0.6-0.87 0.28
0.6
M3/min
3 Mixing Time,in Min for 100 volume to be change
QS =100
( QV ) Qs =
116
min
4 Reynold Number,Re
ND Re =
a2
ρ
u =Viscosity in Kg.M/hr
μ =
108
16524
Hence,Re >10000 Flow is Turbulent Power Number for Reynold and For 3 bladed pitch turbine is Np = 5
0.8
Power Required : PL =Power loss , =
H . P=1. 1
[
FN P ρN 3 D S
735
= Provided H.P=
a
5
+ PL
]
0.41
H.P
1
H.P
0.2 0.5
For Mechanical Seal For Stuffing Box
F= Multi impellerFactor Pi / Da
0.1 to 0.5 0.5 to 1.0 1.0 to 1.5 1.5 to 2.0 2.0 to 3.0 3.0 to 4.0 >4
Page 2 of 9
1.6
Multi impeller factor
F 1.4 1.5 1.6 1.7 1.8 1.9 2
Page 3 of 9
6 Width of Blade,mm W=
40
mm
7 Diameter of Shaft,mm
d s =100
[
J m ( H . P ) ΣL D a NN i
ds = Provided ds =
]
0. 33
Drive length =
0.5
Ls=Length of Shaft ,M =
3.8
Where,Jm =Jamming Factor EL =Overhung length=
58.2 60
M
1.5 to 2 2
Jm = L1+L2
5.55 2.8 L1 =Distance from Centre of Bottom First Impeller to
mm mm
to Vessel Top Surface
=
3.4
M
L2 =Distance from Centre of BottomSecond Impeller to Vessel Top Surface =
2.15
M
8 Thickness of Blade,mm
H.P t b =555 NN i N b W
(
tb =
0. 5
)
+2CA
5.1
mm
3
mm
Provided tb = 9 Critical Speed,RPM Nc=
[
1 1 . 92 W S L
EI S3
2. 67
+Wa1 L
a1 2
( La 1 + L 1 ) +W a2 L a2 2 ( La 2 + L 1 ) +W c L c2 ( Lc + L 1 )
]
0. 5
¿ ¿ ¿¿ ¿ ¿
Where E=Modulas of Elasticity = I=Moment of Inertia,cm4 = W S=Weight of Shaft,Kg = = Bearing Span,L1
= W C=Weight of Coupling,Kg=
1800000
Kg/cm2
63.6
cm4
[dS2LS/159] 86.0
Kg
0.3
M
20
Kg
Lc =Distance from Centre of Coupling to tanks Top height = NC =
97.6
0.8
M
RPM
Hence,Operating Speed Should be
≥
1.3*NC
=
126.9
RPM
OR 0.7*N ≤ C
=
68.3
RPM
Page 4 of 9
18
Wa1
18
Wa2
M
10
Deflection,mm:
A Deflection due to 1st Impeller Weight Weight of 1st impeller W a1 =
[ ][
δ 1=
Wa1 X 6 EI
=
2 L a1 L1 +3 L a1 X− X 2 ] 2.24225
= 0.0224225
18
Kg
X=Distance from centre of lower bearing to distance at which deflection is to be measured = 3.4 M 340 Deflection at the end of 1st impeller ,X=La1
cm
cm M
=
3.4
Bearing Span,L1 = =
M
340
0.3 30
M cm
cm
B Deflection due to 2nd Impeller Weight Weight of 2nd impeller W a2 =
2 L a 2 L1 + 3 Lalignl ¿ ¿¿ Wa2 X [¿ X −X 2] δ 2= 6 EI
]
=
0.59370
cm
=
0.005937
M
= 2.15 M 215 Deflection at the end of 2nd impeller ,X=La2
=
2.15
Bearing Span,L1 = = C Deflection due to Shaft Weight
[
δ s=
WsL
s
8 EI
3
]
=
3.69
cm
=
0.03693
M
D Deflection due to coupling weight
δ3=
[ ][ WcX 6 EI
=
2 Lc L1 +3L c X− X 2 ] 0.00000
M
E Critical Speed at Overhung,Nc
[
30 g N C= Π δ 1 +δ 2 +δ 3 +δ s =
Kg
X=Distance from centre of lower bearing to distance at which deflection is to be measured
a2
[
18
117
0.5
]
Rpm
Page 5 of 9
M
215
0.3 30
M cm
cm
cm
11 Critical speed of shaft when shaft supported at two end 1 Deflection due to Shaft Weight
δ S=
5WS L
S3
5.371
384 EI
mm
2 Deflection due to 1st Impeller Weight
δ 1=
W1 L
2
a 12
( Ls −La 1 )
0.255163
3 EIL S
mm
3 Deflection due to 2nd Impeller Weight
δ 2=
W2 L
2
a2 2
( LS −La 2 )
3 EIL s
1.736142
mm
4 Deflection due to 3rd Impeller Weight
δ3=
W3 L
2
a3 2
( L S −La 3 )
3 EIL S
mm
0.882918
5 Critical Speed ,Nc
[
30 g N C= Π δ 1 +δ 2 +δ 3 +δ s NC =
329.55
0.5
]
RPM
Hence,Operating Speed Should be
≥
1.3*NC
=
428.4
RPM
OR ≤ 0.7*NC
=
230.7
RPM
Page 6 of 9
12 Design of Hub and Key Part Description
Yield stress Shear stress
MOC
σy in MPA
τ in MPA
Crushing stress σc in MPA
Shaft
SS-304
175
43.75
87.5
Hub
CS
180
45
90
Key
CS
180
45
90
Coupling
CS
180
45
90
bolt
CS
180
45
90
A Design of Hub 1 Outer Diameter of Hub,Dh in mm
Dh =2 d s
120
mm
2 Length of Hub,Lh in mm
Lh =1 .5 d s
90
mm
3 Induced shear stress in Hub 16TD h τ s= π D 4 −d 4
(
h
s
Torque
)
τs =
T = 215.981
0.679
Mpa
1 Width of key,W
15
mm
2 Thick of Key,t
15
mm
<
45
ok
B Design of Key For Square Key
3 Shaft strength reductin factor,e
e=1−0 .2
W h −1. 1 d d e=
0.8125
4 Length of Key,Lk
94
mm
5 Induced shear stress
τ is =
Torque
2T LK Wd s τis =
T=
4.14
215.98
Mpa
<
45
ok
Mpa
<
90
ok
6 Induced Crushing Stress
σ ic =
2T LK tds σic =
4.14
Page 7 of 9
N.M
N.M
Page 8 of 9
13 Design of Rigid coupling 1 Design of flange Hub Diameter,D
120
MM
Thick of flange,tf
30
mm
Checking for induced shear stress in flange
τ if =
2T πD 2 t f τif = 0.318444 Mpa
<
45
ok
2 Design for Bolts PCD of bolts,D1 = 3d
180
OD of Flange,D2 = 4d
mm
240
mm
3.36
mm
Nos of bolts n=
Bolt design under shear load
[
8T db= 4 πτ b nD 1
]
0. 5
db =
Bolt size 4nos of M6 size
Page 9 of 9
6
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