basics of reactor design mac2
TRANSCRIPT
Prof. A. B. PanditInstitute of Chemical Technology
University of Mumbai
Basics of Reactor Design & Selection
Mechanically Agitated Contactors
Design Variables
Independent Variables
1. Reactor Geometry : Diameter, Height
2. Impeller type
3. Impeller diameter
4. Impeller Position
5. Impeller rotational speed
Minor Variables
6. No. of baffles / baffle width
7. No. of nozzles / nozzle diameters
8. Other reactor internals : coil, sampling point, foam breaker etc
Function of Impeller
1. Mixing of liquid / liquids
2. Disperse gas / vapors
3. Suspend solid particles
4. Achieve certain heat transfer
Dependent Variables
Parameters defining them:
1) PowerImportant design variable; decides the operating cost
P = Power (watts) = NP N3 D5
NP – power number, function of impeller type and a weak function of geometry of vessel, strong function of Reynolds number, Re for Re< 104
– density of fluid, kg/m3 N – speed of rotation, rev/sec
D – diameter of impeller, m
PPower/unit volume =
2π T H4
• Good overall criteria for heat transfer, solid suspension and gas dispersion
• Not so good for mixing, except shear sensitive material
Dependent Variables
2) Torque
Useful for drive consideration / selection
3 5PNPowerTorque = τ = = ρN D
2 π N 2 π
• Also useful for selection of gear box, sizing of shaft
• Good criteria for flow velocity sensitive operations
Dimensionless Numbers
1) Power Number : P 3 5L
PN =
ρ N D
2) Reynolds Number :2ND ρ Inertial forces
Re =Viscous forces
– viscosity of fluid at operating conditions, kg/m s, mPas
1 cp = 1mPas = 0.001 kg/m s
Relation between NP & Re
P 3 5L
PN =
ρ N D
2ND ρRe =
Different impeller type
10 100 1041000 105
10
1
100
NP independent of
Re for Re 104
Dimensionless Numbers
3) Froude No. : 2N D Acceleration due to impeller
Acceleration due to gravityg
Useful in mixing of different density liquids
4) Weber Number : 2 3N D inertial forces
surface tension forces
Useful in deciding gas dispersion or liquid emulsion
– surface / interfacial tension, N/m
5) Blend Number : NB = N
N – speed of agitation, rev/sec
– mixing time to achieve specific homogeneity
Dimensionless Numbers
4) Pumping Number / coefficient : Q 3
QN =
ND
Useful in correlating pumping capacity of various impellers
Experimental observations : Q
DN
T
0.5
Q 3
DQ TNND
Q – pumping rate, m3/s
4) Richardson Number :
Concept of turnover
L2 2
L
Δρρ g HRi =
ρ N D
Certain Critical Impeller Speeds
1) Minimum impeller speed for gas dispersion :
3) Minimum impeller speed for solids suspension :
2) Minimum impeller speed for surface aeration :
2
1.25Cg
N DQ
T Constant as a function of type
0.450.1 0.2 0.11 -0.85
JS PgΔρN =Sυ d X Dρ
S – function of impeller type
0.191.98
1.11.34SN D g
T
Geometric Consideration
T
D
H
C
B
1) D/T ratio : 0.2 ≤D/T ≤0.5
Low D/T : low purchase price
low power
high shear/ low pumping
High D/T : Higher operating costs
Higher price
Low price / High pumping
2) H/T ratio : 0.5 ≤H/T ≤1.0
Multiple impellers for H/T ≥ 1.0
3) C/T ratio : 0.1 ≤C/T ≤0.3
Solid suspension, low C/T etc.
4) B = Baffles, 4 in No. diametrically opposite
B/T 1/10 to 1/12
Heat Transfer
Correlation for Reactor side HTC :
-0.14
0.59 0.33 -0.1wallRPr Fr
bulk
μh T=1.35 Re N N
k μ
…..For jacket heating / cooling
-0.14
0.64 0.33 -0.1wallRPr Fr
bulk
μh T= 0.87 Re N N
k μ
…..For coil
Overall heat transfer coefficient ‘U’ :
R m o
1 1 x 1= + +
U h k h x – metal thickness
Km – metal conductivity
ho – outside heat transfer coeff. (k.cal/hr m2 OC)
fluid
x
ho
hR
km
walllimpet
Typical Processes
Equal fluid Motion by far the most common actual mixing requirement: Adequate for heat transfer and solid suspension or
gas dispersion.
Equal fluid Motion
1. Most common mixing requirement
2. Constant torque per unit volume
3. Ensure motion throughout the tank
4. Solid suspension application
5. Blend time increases with increase in the reactor diameter
6. Flow velocity sensitivity operations e.g. heat transfer
Typical Processes
Solid Suspension
1. Scale-up rules can vary
2. P/V decreases with increase in tank diameter
3. T/V can be constant
Surface Effects
1. Vortex formulation
2. Dry solids drawdown
3. Foam breading / non-wetting nature
Dispersion
1. Constant P/V
2. Usually high shear , radial turbine
3. Gas dispersion
4. Emulsification
5. Shear sensitivity operations
High Viscosity Special Cases
Special Impellers : Close wall clearance
Anchors, Helical ribbons, screws / draft tubes
Range of applications :
Anchor : 10,000 cp – 1,50,000 cp
Ribbon : 30,000 cp – 1,50,000 cp
Power response can be calculated from
NP x Re = Constant
3 5constantP= ρN D
ReRe
NP
Blend time can be roughly estimated from
N = 50
Scale up techniques
Criteria for scale-up
N = constant. or constant tip velocity
Scale up criteria Validity of operation
1. Dimensionless Number (hT/K) Good for heat transfer
2. Impeller rotational speed (N) Good for mixing time
3. Power (P/V) Fluid motion, dispersion (but not solids suspension)
4. Torque Fluid motion (including suspension)
Impeller type & flow patterns
1) Radial flow : Turbine, paddles
Two loops with exchange at impeller plane
Impeller type & flow patterns
2) Axial flow : Propeller, Hydrofoil (fans)
Single loop : Low velocity
Impeller type & flow patterns
3) Mixed Flow :
Pitched blade turbines
4) Complex Flow :
Ribbons / screw
Two superimposed loops with greater
exchange
No loop : no mixing
Utility of the relations in design
Problem Statement : Dehydration and esterification of long / medium oil is to be carried out as per the recipe.
Process Conditions : Max temp. 260oC
Reactor charge : 3235 kgs of oil
Starting temp. of oil : 30oC
Solvent used : Xylene (100 kgs)
Other raw materials : Penta, pthalic in solid form
Neglecting reaction kinetics and assuming no heat effects associated with
the reaction.
The Reactor is expected to carry out the following physical operations
1. Mixing of solid / liquid raw material
2. Mixing of xylene for the removal of water of dehydration and or reaction
3. Supply of heat with thermic fluid to achieve temperature as per recipe.
Utility of the relations in design
Now let us assign some time frame to the above operations
Operation Alloted time (sec) Why this time
1. Heating oil to 150oC 1 hr Could be reduced
2. Heating to M. G. temp. 245oC
1 hr / 1 hr 15 min Thermic fluid as limiting temp
3. Cooling to 170oC 30 min Cooling media temp
4. Heating to 170oC 30 min Phthalic reactions(not too fast)
5. Esterification 6 to 7 hrs Reported O. K.
Utility of the relations in design
Total occupancy : 6o% of the geometric volume
Geometric volume = (3235+100)/0.6 = 5.56 K. L.
Let H/T 1.0 H = T = 1.92 m
Dished ends : Ease of drainage / discharging
Actual diameter to be selected in consultation with the fabricator :
Available plate size, no waste
Let T = 2.0 m, Hence rough geometry
2.0 m
2.0 m
4 in no. (0.2m)
A) Selection of Geometry :
Utility of the relations in design
B) Selection of heating surface /form/cooling :
1. Limpet coli 2. Jacket
Form of heating : steam or Thermic fluid
Max. temp. 260oC and hence hot fluid temp. 200oC very high steam pressure, increase in reactor wall thickness expensive
Thus : Thermic fluid : due to high viscosity it requires good velocities :
not possible in jacket due to large flow areas
and hence Limpet coils.
Cooling : Cooling oil or cold fluid through limpet coil.
Utility of the relations in design
C) Selection of Impeller :
Properties of fluid required for the same - viscosity at operating temperature or range of viscosities or max. 300
cp 3 poise 200oC
- density of fluid 900 kg/m3
Functions expected of impeller
Generate sufficient liquid motion : well directed to give
1) good mixing
2) good heat transfer
3) good solid suspension
4) good nitrogen dispersion (blanketing)
For the range of viscosities & densities encountered Anchor and / or ribbons are not required
Utility of the relations in design
Impeller type Its best usefulness
1. Radial flow Gas dispersion and heat transfer
2. Axial flow Good for mixing, good solid suspension
3. Mixed flow Multipurpose impeller
Better designs are available enhancing any of the above 4 functions
Radial flow : higher power consumptions
Axial flow : lower power but not good for dispersion
Thus MIXED FLOW IMPELLER IS SELECTED
Various designs are available : by varying pitch axial or radial component can be altered, by making it profiled, it could alter shear and flow levels etc.
Due to slightly higher viscosities D/T ratio used 0.5 and two impellers on the same shaft can be used
The final geometric design
2.0 m
2.0 m
0.75
1
0.75
Parameter selection
The only parameter remains to be selected is ‘ impeller speed’
We have number of choices
1. Impeller speed required for heat transfer
Largest heat duty : during esterification
Alloted time 6 hrs.
This time includes
1) 170 to dehydration temp
2) dehydration
3) esterification
The final design
Heat duty for each operation
1. m CpT = 3235 x 0.5 x (260-170) = 144575 kcal
2. Dehydration = water removed 80 kg
= 43200 kcal
3. Esterification = water removed 120 kg
= 64800 kcal
For 2 & 3 xylene is also evaporated
200 kgs of water is removed in 5 hrs. 40 kgs of water removed/ hr (if removed)
If less then accordingly : 100 kgs of xylene present
Based on the azeotropic concentration 1 kg of water is associated with 18kg of xylene
The final design
4. Heat duty required for xylene evaporation = 720 x 95 x 5 = 34200 kcal
Thus, total heat duty in 6 hrs is Q = 1 + 2 + 3 + 4 595000 kcal
1,00000 kcal/hrs
Total heat transfer area is 15.0 m2 of limpet coil
Average temp. gradient = o285-170 - 285-260
= ΔT =59 C115
ln25
Thermic fluid temp. is assumed to 285oC
Hence the required HTC Q 1,00000
= =A.ΔT 15.0×59
2o
kcalU =113
hrm C
The final design
Impeller speed required is calculated as follows
R m o
1 1 x 1= + +
U h k h R m
1 1 1 0.006= + +
113 h 800 k
R 2 o
kcalh 226
hr m C
2 3 0.241 32R w
o
h T μND ρ=0.485
k μ μCPk o 2o
kcalT=2.0m;k =0.163
hrm C
R 2o
kcalD=1.0m;h =226
hrm C
kg kg
=3 poise=0.3 1080ms m m
3P o
kcalC =0.5 ; 900kg m
kg C
N = 1.52 r/s 91 rpm (90 rpm)
Now check whether this impeller speed satisfies the other operational
requirements
The final design
Heating to 150oC in 1 hr.
Heat duty = m Cp T
= 3235 x 0.5 x (150-30) = 194000 kcal
Heat flux obtainable = U A T
= 113 x 15 x [(285-30)-(285-150)]/ln(255/135)
= 319816 kcal / hr.
Expected time of heating = 194000/319816 = 0.6 hrs 37 min.
Other parameters can also be checked
Cooling requirement also appear to be adequate if the thermic fluid is available at a temp. of 100oC or below
The final design
Mixing time calculations :
lengthofl ongest loopθ= ×5
Avg. circulation Velocity
4mt. 4×5= ×5= 21sec
0.1×2 ND 0.942
Final mixing depends upon the exchange between the two loops which is 35 %.
mix
21θ 60sec 1min
0.35
GOAL ACHIEVED
Process Reactor design is complete
Impeller drive selection
Parameter known : D = 1m, N = 1.5 rev/sec
Impeller type : Mixed flow, NP = 1.0 for Re > 104
22 1.5× 1 ×900ND ρReynoldsNumber= = =4500
μ 0.3
Thus, you can
• Expect NP to increase to about 1.1
• Actual power curve is necessary
Power, P = NP N3 D5 = 1.1 x 900 x (1.5)3 x (1)5 = 3341 watts
Now two such impellers
Total power = 1.9 x 3341 = 6348 watts = 8.5 HP
Thus with the knowledge of gear efficiency 10 HP motor should be adequate giving
3P=1.81Kw m
V{Normal Range is 1 to 5 kw/m3}
Thus quite satisfactory.
Additional Process Calculations
• Separator design
• Nozzle selection
• Nozzle location
3D ×RPMHP=
CC = 50, for only torsional
= 80, for torsional + bending
= 130 for
Mechanical design i.e. shaft diameter, critical speed
in consultation with the fabricator.
Selection and design of accessories
Basic Reactor Configuration:
B
C
AA – Reactor
B – Condenser for reflux
C – Separator for xylene return
& water removal
A – Reactor design has been complete
Condenser Design
B – Design of condenser :
Maximum heat duty of condenser = Maximum heat supplied to the reactor
= Q = 100000 kcal/hr
Cooling media = water at 30oC
Let the vapors be condensed and cooled at 30oC
Let it be a Shell and Tube Heat Exchanger
Vapors might be cooled due to atmospheric heat losses by the time they come to the condenser
Let the vapor temperature be 150oC ( as against 260oC)
Condenser Design150oC
37oC
30oC
80oC
o
150-37 - 80-30LMTD =
150-30ln
80-30
= 77 C
For water on shell side and vapors (condensing) on tube side, overall heat transfer coefficient (U) can be assumed to be 500 kcal / hr m2 oC
2
Q 100000Condenser Area, A =
U LMTD 500 77
2.58 3m
Due to pthalic evaporation, considerable fouling is observed,
Thus, Let A 10m2
Mounted Vertical : Washing of vapors and preheating of returned liquid
Fouling : Tube dia ≥ ¾”, periodic clearing
Cooling water requirement
Total heat removed = 1,00, 000 kcal/hr
(T)water = 37-30 = 7oC
Q = m CP T
1, 00, 00 = m x 1 x 7
m = 14285 kgs/hr 15 m2/hr
Pump required with of 50%
Power = h g Q = [30 x 1000 x 9.81 x (15/3600)]/0.5
= 3.3 HP 3.5 HP 3KW
Conclusions
Condenser type = Shell & Tube
Tube size 3/4”
Area 10 m2
Vertical Mounting
Cooling water : 15 m3/hr
at 3 kg/cm2 head
3 KW motor
Design of Separator
Options : Horizontal (larger space)
Vertical (less efficient)
Design information required
A. Time of separation of xylene / water
B. Reflux rate of xylene
A. 4 to 5 seconds : Lab experiments
B. 720 + 40 (xylene + water) : 760 kgs / hr
950 lits / hr 265 ccs/s
Mean residence time of mixture 10 times of separation
60 seconds or 1 min
Volume of the separator = 265 x 60 = 15900 cm3 16 lits
Design of Separator
Separation is taking place with continual agitation due to falling liquid
Net liquid velocity 10 mm/s
C/s area of separator = 265/1 (cm3/s)/(cm/s) = 265 cm2
Diameter of separator 20 cm
Height or length = 50 cm
Separator Arrangements
vap
liquidwater
xylene
AB
vapors
water
Xylene to reactor
vaporsC
Other Utilities
1) Thermic fluid boiler – 2, 00, 000 kcal/hr
Hytherm 600 – max. operating temp. 300oC
2) Cooling water
3) Electricity : Flame – proof connection
Design Problem
Problem Statement : To design a reactor for emulsion polymerization
Important Criteria
1) Size of the droplets
2) Heat of reaction to be removed
3) Controlling the molecular wt. distribution
Experimental work in the lab should provide the following information
1) Reaction kinetics : Rate of consumption of monomer as a function of reaction conditions, monomer concentration and the form (droplet surface area)
2) Heat effects associated with it
3) Effect of speed of agitation (shear) on the emulsion quality :
Droplet size distribution
Design Problem
Interpretation of lab results
Formulation of mathematical model
Material Balance : Reaction RA = k1 CAm
1 1i i i i 1 -k t
i i i
C k V t Ce
C -k V Co
- flow rate, m3/s
k1 – rate constant 1/s
C - initial conc. gmole/m3
Vi – initial volume, m3
Ci – molar conc. in inlet flow (gmoles/m3)
C1 – conc. at time, t1
Design Problem
Heat Balance : Including the heat of reaction
Enthalpy in – enthalpy out + enthalpy generated = Accumulation of enthalpy
m CP Ti – (Atm. losses + heat removal) + R . HR = CPR T d/dt (mR)
m – mass of monomer + water input, kgs/s
CPi – sp. Heat of entering mass, k.cal/kg oC
Ti - inlet temp. oC
R – rate of reaction, gm/s
HR – Heat of polymerisation, k.cal/gm
CPR – sp. Heat of reaction mass, k.cal/ kg oC
TR – temp. of reactor, oC
mR – reactor mass, kg
(1)
Design Problem
Neglect atmospheric losses
Over a period of specified time period
t t
Pi i L P R0 0
t
PR R i0
mC T dt - Q C Z ΔT×t+R H dt
=C T m +m dt
L PwhereQ C ΔT. t=totalheat removedby coolingwater
From equation (1) and (2) total kinetic information can be obtained
(2)
Design Problem
Process parameter selectionGeometrical consideration : Same as before
1) Mixing 2 ) Heat transfer 3) Effect of agitation on product quality
Factor 3 will affect the impeller selection in the following way
1) High shear impeller: low D/T, high speed, smaller drops, large shear gradients, poor heat transfer at wall but good at interface
2) Low shear impeller : High D/T, low speed, larger drops, lesser shear gradient (less wide drop size distribution) good heat transfer at wall but poor at interface
Thus, unless these effects on product quality are assessed in labs.
“Impeller selection is difficult”
Say we generate this information in labs, the design procedure is identical
Additional Impeller speed criteria
0.6
0.4 0.2
32 -0.1
c
d
σ
P V ρCd =a
μμ
Design Problem
We require, one impeller speed for good mixing
second for good heat transfer
Third for good dispersion (emulsion)
fourth for particular drop size distribution
Now, all these impeller speeds are function of the following additional parameters
1. Physical properties of system
2. Type and size of impeller
3. Required production rate (also dependent on temp. & catalyst conc.)
Thus number of combinations need to be tried for an optimum design
Again : parameter might be different for different recipes
Thus finding a compromise, suitable for all recipies
These are the general consideration in Reactor Design, many specific are related to individual processes
Mechanical Aspects
Material of Construction
Type of Services
• Continuous – Slow speed
• Otherwise – high speed
• Future changes / Experiments (built in flexibility)
• variable speed
Power for agitator
Absorbed for agitator
Add for baffles and fittings
Dip pipes (10%) and thermo wells (40%)
Transmission Losses
Worm wheel < 85%
Helical gears > 90%
Planetary gears > 96%
V belts 90 to 95 %
Gland Losses
Higher of ½ HP or 10%
Motor Aspects
Oversize for start up
oversize for settling solids
next higher standard size
Mechanical Aspects
Shaft diameter / size
• Slow speed : have design for (1.5 x full load motor torque)
• high speed : have design for (2.5 x full load motor torque)
Concerns
• Jamming
• Fatigue Failure
• Pitting / corrosion
• Deflection
Mechanical AspectsShaft diameter
dt
0.75 r
2r
L
S
Tm = 2.5 Tc ton.inc
3300×12×HPT =
2 n×2240
mm
TForce, F = ton
0.75r
Moment Mm = Fm x L ton.in
Shaft deflection
m
y 3
t
32 MStress, f =
d
0.75 r x
3m
4
F L448x= =
9 D E
Mechanical AspectCritical Speed
If ‘x’ is the critical speed we must not work at (0.7 x) RPM to (1.3 x) RPM
4s
EIx=k
W lRev / min.
E : Young’s Modulus
I : Moment of Intertia
Ws : Weight of shaft
K : from graph
k
= L/S
= length / distance from bearing
MixingTypes
• Liquid – Liquid (most common) a) density difference b) viscosity difference
• Solid – Liquid a) slurry b) suspension c) dissolution
• Gas – Liquid a) dispersion
• Liquid – Liquid (immiscible) a) emulsion / dispersion
Requirement
Energy to be supplied for moving the different phases
a) Supplied internally : e.g. Mechanically Agitated Contactors
b) Supplied externally : e.g. use of pumps, compressors, blowers
Devices Used
a) Stirred vessels
b) jet mixing
c) static mixing / mixers
Usually mixing is accompanied by other operations
Jet Mixing
a) liquid jet : low to medium viscosity liquids
Liquid velocity generated through the external pump
1 2L
4 61 6 1 6i o
Z TMixingtime = θ =
Re ν d g
Jet Mixing
b) gas jet : medium to high viscosity liquids
Use of external compressor : different fluid
Multipoint Single point
Static Mixers
Number of different designs are available
Simplest : baffle in heat exchanger shells
Job : divert the flow by putting an obstacle in its path
Energy associated with the moving fluid is used for mixing, i.e. if fluid is made to go everywhere in the reactor / vessel uniformity (mixing) will be achieved.
Common Examples
a) Kenics Twisted stripe
b) Sulzer SMXL / SMX
Inserted in pipes
Flow bifurcation takes place and the direction is changed
Energy for mixingStirred Vessel
P x mix = NP N3 D5 x mix joules
Typical = 0.2 to 0.4 %
Jet mixing
(Vg L g x volume) x mix
Typical = 0.03 to 0.8 % Due to pump or compressor
Static mixing
(P x volumetric flow rate) x (L/velocity)
Typical = 1 to 10 %
One of the most energy “Inefficient” operations
“Considerable Scope for improvement”
Problem Statement
1) To carry out blending of two liquids
2) To transfer O2 in the fermenter liquid by air sparging
3) To suspend the catalyst particle in a liquid – uniform suspension
4) To control the temperature of the reactor
5) Hydrogenation of fatty oils to saturated oils
a) Suspend Raney-Nickle catalyst
b) Sparge and distribute hydrogen
c) Control the hydrogenation temperature
Problem statement1) Blending of Two miscible liquids
e.g. Std. geometry, disk turbine
Estimation of ‘N’ (dimensionless mixing time)
AB
C D
E
Requirement
1) Length of loop, longest
2) Average velocity
3) No. of circulations
1) Length of the longest loop ‘ABCDE’
2) Average velocity Vrw = 0.53 (D/w) ND (D/T)7/6
3) No. of circulations 5 for 95% mixing
4 mix = 5 x circulation time
13/6aH+T T wNθ=9.43 D dT
Thus, loop length and average velocity
Problem Statement2) To transfer O2 in fermenter :
Requirement : 1) Good gas dispersion
2) Generate interfacial area
Rate of O2 transfer, gms/s = KLa x C* x V (1/s x gm/m3 x m3)
And
KL a = 0.025 (P/V)0.59 (VG)0.5
P/V – watts/m3, VG = superficial gas velocity, (m/s)
N
NPG/NP
QG/ND3
PG = NPG L N3 D5
Can be obtained by changing P/V or VG
Typical P/V – 1000 to 5000 watts / m3
VG 30 to 40 mm/s
P/V = g VG
Problem Statement3) To suspend catalyst particles
0.45
0.1 0.2 0.11 -0.85js p
gΔρN =S d x D
ρ
S – function of impeller type, location & geometry
jsG jsG 3N =Nb
GQxND
x – type of sparger / location and regime
b – extent of reduction in NPG
Thus knowing dp, , x & S. Select either Njs for a fixed D or select D for a
fixed Njs.
Now, Power N3 & D5. OPTIMISE / SCALE EFFECT
Problem Statement
-0.140.59 0.33 wallR
Prbulk
μh T=1.35 Re N
k μ
4) To control reactor temperature
Know heat flux Q = U A T
Know ‘A’ from reactor geometry
Know T from heat transfer medium conditions
Estimate U.
R m o
1 1 x 1Now, = + +
U h k h
Jacket
Coil
0.64 0.140.332R w
o
h T μND ρ=0.87
k μ μCPk
Optimise ‘ N & D’ in Re to get required ‘hR’
Problem Statement5) To control reactor temperature
a) Estimate Njs for the catalyst loading (Na)
typically, dp 5.0 x 10-6 m
x = 5 %
b) Estimate Required KL a (Nb)
i) Calculate NS = 1.25 QG 0.25 (T/D2)
ii) Estimate KL a or P/V (N) & VG to get the desired KL a
iii) Estimate H2 transfer rate
Estimate Njs again
c) Estimate N for the required heat transfer coefficient (Nc)
Select the higher of Na, Nb & Nc to satisfy all the requirement
Mixing time measurement methods