(a)
Tutorial on Scale-Up The following expression for a fully baffled stirred bioreactor with a single impeller has been derived by dimensionless analysis: ππ = π(ππ
π ) π
where
Np
is power number
N Re c
is Reynoldβs number
π
is an exponent
is a constant dependent on vessel geometry
Plots of power number against Reynolds number on log-log coordinates for various bioreactor configurations based on Figure 1 can be constructed from experimentally obtained data as in Figure 2, with the value of the exponent π changing with flow regimes. Explain the significance of these curves in terms of scaling up a fermentation process in geometrically similar bioreactors in each of laminar, transient, and turbulent regions.
Figure 1
(b)
(5 marks)
A fermentation process in a pilot-scale stirred-tank bioreactor with four baffles and two impellers each comprising of a disc with six vertical flat-blade impellers with dimensions as below was found to produce the maximum yield when the impeller speed was N = 0.27 rps.
Dt (Fermenter diameter)
=
1.00 m
Da (Impeller diameter)
=
0.33 m
E (Height of lowest impeller)
=
0.33 m
L (Length of blade)
=
0.0825 m
W (Width of blade)
=
0.066 m
J (Baffle width)
=
0.10 m
H (Distance between impellers)
=
1.00 m
The fermentation broth fulfilled the criteria for a Newtonian fluid throughout the fermentation, and has the following characteristics: Density Viscosity
ο² ο½ 1300 kgm ο3 ο ο½ 0.03 kgm ο1s ο1
The following relationships apply:
ππ = πππ30π·5
Power number
π
π0 = πππ 3 π·π5 π0 = πππ 2 π·π3 2
π ππ
π = πππ· π
where
(turbulent flow)
(laminar flow)
Reynoldβs number
ο² = liquid density
ο = liquid viscosity N = impeller rotational speed
π·π = impeller diameter
Po = power consumption for un-gassed fluid You are required to scale-up this fermentation process using the method of βconstant power per unit volumeβ to a geometrically similar production-scale
bioreactor 50 times its volume. Estimate the impeller speed of the productionscale bioreactor.
A log-log graph paper is provided in the Appendix 1.
(25 marks)
Figure 2.
Solution (a) This typical power curve can be divided up into 3 clearly defined regions, as shown in Fig. 2 and described in Table 1 below:
Table 1: Regions in a Power Curve
(ο£ )
Region
Reynolds number
Laminar flow
<101
-1
Transition
101 - 104
Variable
Turbulent flow
>104
0
Slope of plot
The Reynolds number is thus a criterion for the degree of turbulence within the system and may be used to reveal the flow regime which exist. (3 Marks) If the experimentally determined value of the exponent ο£ are substituted into equation 1, the following expressions results:
P ο½ cο²N 3 D 5 P ο½ cοN 2 D 3
(turbulent flow) (laminar flow)
These two equations are widely used to predict the effects of operating variables upon power consumption in scale-up of fermentation based on un-gassed fluids. (2 Marks) (b)
From the dimensions given, we can determine, which curve on the plot of Np against Rei that corresponds to curve A.
Check if the system is in the transition flow region: Calculate the value of the Reynolds number (NRe) on the small scale under the defined optimal conditions.
ο²N i Da2 Rei = ο Where Ni = impeller speed of agitation in rps = 0.27 rps.
Da (Impeller diameter) = 0.33 m ο² ο½ 1300 kgm ο3
Density
ο ο½ 0.03 kgm ο1s ο1
Viscosity Therefore, Rei =
ο²N i Da2 1300 ο΄ 0.27 ο΄ 0.332 = 1,274.13 ο½ ο 0.03
The value of Reynolds no. indicates that the flow is in the transition region. The following procedure can be used for scale-up in the transition region: (ii)
Find the corresponding value of the power number at small scale (N P1) by interpolating the power curve. From the power curve, the corresponding value of NP1 is 4.8. With two impellers, NP1 = 2 Γ 4.8 = 9.6
(iii)
Calculate power of the small scale from power number equation:
P1 ο½ N P1 ο²N13 D15
ο P = 9.6 Γ 1300 Γ 0.273 Γ 0.335 = 0.96 W (iv) Calculate the required power consumption on the large scale:
ο¦V P2 ο½ P1 * ο§ο§ 2 ο¨ V1 (v)
οΆ ο·ο· = 0.96 * 50 = 48 W οΈ
For the large fermenter, calculate values of the Reynolds number over a range of different impeller speed :
ο¦ ο²N 2 D22 οΆ ο·ο· N Re ο½ ο§ο§ ο¨ ο οΈ First, what is the value of
D22 ?
ο¦ Di For geometrically similar vessels, ο§ 1 ο§ Di ο¨ 2
1
οΆ ο¦ V1 οΆ 3 ο·ο½ο§ ο· ο· ο§ο¨ V2 ο·οΈ οΈ
1
1 ο¦V οΆ3 ο D ο½ ο§ο§ 2 ο·ο· Di1 ο½ ο¨50ο©3 ο΄ 0.33 ο½ 1.2m ο¨ V1 οΈ
Now, calculate values of the Reynolds number over a range of different impeller speeds:
Ni(2)
Rei(2)
0.025
1560
0.050
3120
0.075
4680
0.100
6240
0.125
7800
0.150
9360
0.175
10920
0.200
12480
Transition Region
Turbulent Region
Presumably the speed of agitation is between 0.1 and 0.17 because they fall in the transition region. (vi)
Find the values of the power numbers corresponding to these Reynolds numbers by interpolating the power curve. Ni(2)
(vii)
Rei(2)
Np
0.025
1560
4.8
0.050
3120
5.4
0.075
4680
5.8
0.100
6240
6.0
0.125
7800
6.0
0.150
9360
6.0
0.175
10920
6.0
0.200
12480
6.0
Calculate the power consumption on the large scale at each selected value of impeller speed from the normal power number equation: P2 ο½ N P 2 ο²N 23 D25 Since the large scale is geometrically the same with the small scale, hence with 2 impellers, NP(2) = 2 Γ NP (obtained from the curve). Therefore,
Ni(2)
Np
2Np
ο²ο
0.025
4.8
9.6
1300
1.2 0.0000156
2.488
0.485
-1.60
-0.31
0.05
5.4
10.8
1300
1.2
0.000125
2.488
4.367
-1.30
0.64
0.075
5.8
11.6
1300
1.2
0.000422
2.488
15.830
-1.12
1.20
0.1
6
12
1300
1.2
0.001000
2.488
38.818
-1.00
1.59
0.125
6
12
1300
1.2
0.001953
2.488
75.816
-0.90
1.88
0.15
6
12
1300
1.2
0.00338
2.488
131.010
-0.82
2.12
0.175
6
12
1300
1.2
0.005
2.488
208.039
-0.76
2.32
0.107334
6
12
1300
1.2
0.001
2.488
48.000
-0.97
1.68
(vii)
Ni(2)3
Da(2)
Da(2)5
P2
log Ni(2)
log (P2)
Plot power consumption against impeller speed on log-log coordinates for the large fermenter. Or use Goal Seek in Excel to determine what is the value of Impeller speed that corresponds to P2 = 48 W.
From Goal Seek, we shall obtain the Ni2 = 0.107 rps. Or Solve using the normal calculation, by substituting the values of P2 as 48 W into the power no equation. P2 ο½ N P 2 ο²N 23 D25 48 ο½ 12.0 ο΄ 1300 ο΄ N 23 ο΄ 1.25 48 ο½ 38816 N 23 N 23 ο½ 1.237 ο΄ 10ο 3 N 2 ο½ 3 1.237 ο΄ 10ο 3 ο½ 0.107 rps
From the curve of P2 against Ni(2), at P2 =48 W, the value of Ni(2) was found to be 0.107rps. And from the plot of log P2 against log Ni(2), at log 48 = 1.68, the value of log Ni(2) was found to be -0.96. Therefore, the value of Ni(2) is 10-0.96 = 0.107 rps.
4.8
Re = 1,274.13
QUESTION 2
(PO2, PO6, CO3, C3, C3, C5)
Two geometrically similar stirred tanks with a flat-blade turbine impeller of the following dimensions are to be operated at 30ο°C as pilot-scale and production-scale aerobic fermenters.
Scale Pilot Production
Impeller diameter, Di (m) 0.24 0.8
Liquid volume, V (m 3)
Tank diameter (m)
0.17 6.28
0.50 1.6
Satisfactory results were obtained with the pilot-scale fermentor at a rotational impeller speed Ni of 1.5 s-1 and volumetric air flow rate, Q of 0.0083 m3 s-1. The density and viscosity of the broth are 1050 kgm-3 and 0.002 kg/m.s, respectively. Vanβt Riet (1979) has discovered a correlation for oxygen mass transfer coefficient, k La as the scale-up criterion in relation with the following equations: β3
ππΏ π = 2.0 Γ 10
ππ 0.7 0.2 ( ) π£π π β0.20
ππ π β0.25 ππ2 π·π4 = 0.10 ( ) ( ) π0 ππ π πππ π 2β3 where
Pa
=
aerated power (W)
vs
=
superficial gas velocity (m/s)
Wi
=
impeller blade width
P0
=
power consumption for unaerated bioreactor.
g
=
gravitational acceleration = 9.81 ms-2
(a) By referring to Curve 1 in Fig. 3, calculate the Reynolds number and hence determine the power consumption of aerated bioreactor at pilot scale. The following relationships apply:
ππ = πππ30π·5
π
Power number
π0 = πππ 3 π·π5 π0 = πππ 2 π·π3 2
π ππ
π = πππ· π
where
(turbulent flow)
(laminar flow)
Reynoldβs number
ο² = liquid density
ο = liquid viscosity N = impeller rotational speed
π·π = impeller diameter
Po = power consumption for ungassed fluid (7 marks)
Figure 3. The power number-Reynolds number relationship for various impellers.
(b) Calculate the superficial gas velocity, vs and estimate the oxygen mass transfer π coefficient, kLa for pilot scale. Given that ππ = π΄
where A = cross-sectional area of the bioreactor, Q = volumetric flowrate of air sparged into the fermentor, (5 marks)
(c) Estimate the kLa for the production scale by employing constant superficial gas velocity and constant power consumption per unit volume as scale up criteria and comment on the value obtained in comparison with the value of k La in (b).
Given that, correlation for speed of agitation in terms of volume is 2β 9
π2 π1 =( ) π1 π2
The subscript 1 and 2 refer to pilot scale and production scale, respectively. (15 marks)
Solution: (i)
ππ
π =
ππ·2 π π
=
1050Γ1.5Γ0.242 0.002
= 45,360 (turbulent flow) (2 marks)
From Curve 1 in Fig. 1, Np = 5
Then power consumption for un-aerated bioreactor, π = ππ ππ 3 π·π5 ο5 Γ 1050 Γ 1.53 Γ 0.245 = 14 W.
(1 marks)
Then the aerated power consumption can be calculated by the given formula;
β0.20
ππ π β0.25 ππ2 π·π4 = 0.10 ( ) ( ) π ππ π πππ π 2β3 ο
ππ π
= 0.10 (
0.10(2.35) (
1.5Γ0.17 0.024
9.81ππ
Given that,
β0.25
0.0083
ππ
)
(
1.52 Γ0.244
2 9.81ππ Γ0.173
β0.20
β0.20
)
=
)
(1 mark)
= 0.2
π·π
(1 mark)
Therefore, Wi = 0.2Di = 0.2 Γ 0.24 = 0.048 m
(1 mark)
By substituting P = 14 W and Wi = 0.048 m into the above equation,
ο
ππ 14
= (0.235) (
0.024 9.81Γ0.048
β0.20
)
= 0.426
Then, Pa = 14 Γ 0.426 = 5.97 W.
(1 mark)
ii) Cross-sectional area of the stirred tank, given that DT = 0.5 m
A=π
π·π2 4
Then, ππ
=π
=
π π΄
0.52 4
=
=0.196 m2
0.0083 0.196
= 0.042 π/π
(2 marks)
hence, β3
ππΏ π = 2.0 Γ 10 β3
ππΏ π = 2.0 Γ 10
ππ 0.7 0.2 ( ) π£π π
5.97 0.7 ( ) 0.0420.2 0.17
ππΏ π = 2.0 Γ 10β3 Γ 12.07 Γ 0.53 = 0.0128π β1
(3 marks)
(iii) The rotational speed of agitator for production scale can be determined from,
2β 9
π2 π1 =( ) π1 π2
2β 9
π2 0.17 =( ) 1.5 6.28
οN2 = 0.67 rps
(3 marks)
From constant power consumption for unaerated bioreactor per unit volume where,
P1 P ο½ 2 V1 V2 π
14
Then P2 = π1 π2 = 0.17 (6.28) = 517 π 1
(2 marks)
Then the aerated power consumption can be calculated by the given formula; β0.20
ππ π β0.25 ππ2 π·π4 = 0.10 ( ) ( ) π ππ π πππ π 2β3
π
From the constant superficial gas velocity, ππ = π΄2 = 0.042π/π 2
where A2 = π
π·π2
=π
4
1.62 4
=2 m2
Therefore, Q2 = A2vs = 2 Γ 0.042 = 0.084 m3/s marks)
ο
ππ π
= 0.10 (
0.10(2.66) (
)
0.67Γ6.28 0.054
9.81ππ
Given that,
β0.25
0.084
ππ π·π
β0.20
(
0.672 Γ0.84
2 9.81ππ Γ6.283
)
= 0.2
Therefore, Wi = 0.2Di = 0.2 Γ 0.8 = 0.16 m
(2
β0.20
)
=
By substituting P = 517 W and Wi = 0.16 m into the above equation,
ο
ππ 517
= (0.266) (
0.054 9.81Γ0.16
β0.20
)
= 0.52
Then, Pa = 517 Γ 0.52 = 269.8 W.
(4 marks)
hence, β3
ππΏ π = 2.0 Γ 10 ππΏ π = 2.0 Γ 10
β3
ππ 0.7 0.2 ( ) π£π π
269.8 0.7 ( ) 0.0420.2 6.28
ππΏ π = 2.0 Γ 10β3 Γ 13.876 Γ 0.53 = 0.0147π β1
(1 mark)
Percentage error between the 2 kLa values are defined by, (0.0147β0.0128) 0.0128
Γ 100 = 14.8%
(1 mark)
Theoretically, the two values should be similar, however, it is very difficult to achieve a constant kLa values because of the correlation (Vanβt Riet) used here is very general that applies to this calculation. In addition, the aeration in larger scale will consume more power and cost that will affect the kLa values. (2 marks)