A shell and-tube heat exchanger is required for the following
service:
Hot stream | Cold Stream | |
Aromatic Stream | Cooling Water | |
inlet Temperature (oC) | 85 | 20 |
outlet Temperature (oC) | 40 | 35 |
Mass Flowrate x heat Capacity (kW/oC) | 85.2 |
Hot Stream | cold stream (Cooling water) | |
Heat Capacity (J/kg K) | 2840 | 4193 |
Density (kg/m3) | 750 | 999 |
Viscosity (cP) | 0.34 | 1.016 |
Thermal conductivity (W/m.K) | 0.19 | 0.594 |
Fouling Factor (m2.oC/W | 0.00018 | 0.000176 |
? The cooling water is allocated to the tube-side of the
exchanger.
? It is preferable to employ a fixed-tubesheet heat exchanger for
the service.
? 25.4 mm OD tubes (2.1 mm wall thickness) on a 1.25 x OD
triangular pitch are available. The
thermal conductivity of the tube material is kw = 51 W/m?K.
? Consider four (4) tube passes.
? The maximum tube length that can be employed is 6.098 m i.e. L
< or = 6.098 m
? Assume 1-shell pass. The shell diameter should not exceed 1.5 m
i.e. Ds < or = 1.5 m
? Baffle cut is set at 25% and the baffle spacing (lb) is assumed
to be 0.5 x Ds
? The maximum allowable tube-side and shell-side pressure drops are
70 kPa and 50 kPa
respectively.
? Total annual cost (TAC) is given as follows:
TAC = 123 A^(0.59) + 1.31 [ delta Ptube .
mtube/ densitytube + delta Pshell
. mshell/ densityshell ]
where A is the area of the exchanger in m2, TAC is in
$/year, ?delta P is in Pa, m in kg/s and density? in
kg/m3
2.2 Provide a mathematical expression for the following
constraints:
o the tube side velocity,
o the shell-side velocity, and
{Hint: Note: cooling water in the tubes}
2.3 Derive an expression for the number of tubes in terms of the
tube-side velocity, number of tube
passes, mass flowrate and tube inside diameter.
2.4 Calculate the number of tubes at the minimum and maximum
tube-side velocities
2.1). Show the calculations and summarise your answers in a
table.
{It is convenient to use a spreadsheet for this calculation}
2.5 For each of the number of tubes calculated in 2.4, determine
the shell diameter Ds. (you can fit a straight
line to the data if you would rather like to use an equation). Show
the calculations and summarise
your answers in a table.
2.6 Plot a graph of tube length vs shell diameter for the
minimum and maximum velocity as well as
the maximum shell diameter. Discuss your findings.
2.7 Select various shell diameters between the limits found in
Coulson. {4 to 5 values should be sufficient}.
For each shell diameter, determine the tube length at the maximum
tube-side pressure drop.
Show the calculations and summarise your answers in a table.
2.8 Using the same shell diameters selected in 2.7, determine the
tube length at the maximum shellside
pressure drop. Show the calculations and summarise your answers in
a table.
2.9 For each shell diameter, determine the tube length based on the
heat transfer duty i.e. Q=UA?Tm
{You need to determine the heat transfer coefficients on the tube
and shell-side}. Show the
calculations and summarise your answers in a table.
2.10 Plot your results from 2.7, 2.8 and 2.9 on a graph of tube
length (x-axis) vs shell diameter (yaxis).
{Please use a spreadsheet to do this. Do not submit hand-drawn
plots}. Identify the feasible
region.
2.11 Determine the exchanger with the minimum cost. Discuss your
approach and findings.
2.12 How does the above approach of exchanger design
compare/contrast with the standard
method?
A-2.4)
Ovrall HTC | 600 | W/m2K Taken from R c vol. 6 |
Tube ID (di) | 19 | mm |
No. of Tube pass | 4 | |
Mass flow rate | 30 | kg/sec |
Heat Transfer Area | 260 | m2 |
Tube Length | Tube Side velocity | No. of Tubes |
1.83 | 0.237085 | 2381.437 |
2.44 | 0.316113 | 1786.077 |
3.66 | 0.474170 | 1190.718 |
4.88 | 0.632227 | 893.039 |
6.1 | 0.790283 |
714.431 |
A-2.5
Tube Length | Tube Side velocity | No. of Tubes | Tube Bundle Dia | Clearance | Shell Dia |
1.83 | 0.237085 | 2381.437 | 1636.5790 | NA | - |
2.44 | 0.316113 | 1786.077 | 1442.9763 | 80 | 1522.9763 |
3.66 | 0.474170 | 1190.718 | 1208.3568 | 77 | 1285.3568 |
4.88 | 0.632227 | 893.039 | 1065.4116 | 73 | 1138.4116 |
6.1 | 0.790283 | 714.431 | 966.2867 | 71.5 | 1037.7867 |
WHere k1=0.175 & N1=2.285 for 4 passes at tube side
FOr Tube bundle shell clearance refer graph 12.10 and for tune bundle dia refer table no. 12.4 of RC vol.6
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