Experience is typically what turns a good engineer into a great
engineer. An engineer that can look at a pipe and a flowmeter and guess the
pressure drop within 5%. Someone who can at least estimate the size of a vessel
without doing any calculations.
When I think of such rules, two authors come to my mind,
Walas and Branan. Dr. Walas' book, Chemical Process
Equipment: Selection and Design has
been widely used in the process industry and in chemical engineering education
for years. Mr. Branan has either helped write or edit numerous books concerning
this topic. Perhaps his most popular is Rules of Thumb for
Chemical Engineers. Here,
I'll share some of these rules with you along with some of my own. Now, be
aware that these rules are for estimation and are not necessary meant to
replace rigorous calculations when such calculations should be performed. But
at many stages of analysis and design, these rules can save you hours and
hours.
Physical Properties
Property
|
Units
|
Water
|
Organic Liquids
|
Steam
|
Air
|
Organic Vapors
|
Heat Capacity
|
KJ/kg 0C
|
4.2
|
1.0-2.5
|
2.0
|
1.0
|
2.0-4.0
|
Btu/lb 0F
|
1.0
|
0.239-0.598
|
0.479
|
0.239
|
0.479-0.958
|
|
Density
|
kg/m3
|
1000
|
700-1500
|
1.29@STP
|
||
lb/ft3
|
62.29
|
43.6-94.4
|
0.08@STP
|
|||
Latent Heat
|
KJ/kg
|
1200-2100
|
200-1000
|
|||
Btu/lb
|
516-903
|
86-430
|
||||
Thermal Cond.
|
W/m 0C
|
0.55-0.70
|
0.10-0.20
|
0.025-0.070
|
0.025-0.05
|
0.02-0.06
|
Btu/h ft 0F
|
0.32-0.40
|
0.057-0.116
|
0.0144-0.040
|
0.014-0.029
|
0.116-0.35
|
|
Viscosity
|
cP
|
1.8 @ 0 0C
|
**See Below
|
0.01-0.03
|
0.02-0.05
|
0.01-0.03
|
0.57 @ 50 0C
|
||||||
0.28 @ 100 0C
|
||||||
0.14 @ 200 0C
|
||||||
Prandtl Number
|
1-15
|
10-1000
|
1.0
|
0.7
|
0.7-0.8
|
|
Material
|
Advantage
|
Disadvantage
|
|
Carbon Steel
|
Low cost, easy to
fabricate, abundant, most common material. Resists most alkaline environments
well.
|
Very poor resistance
to acids and stronger alkaline streams. More brittle than other materials,
especially at low temperatures.
|
|
Stainless Steel
|
Relatively low cost,
still easy to fabricate. Resist a wider variety of environments than carbon
steel. Available is many different types.
|
No resistance to
chlorides, and resistance decreases significantly at higher temperatures.
|
|
254 SMO (Avesta)
|
Moderate cost, still
easy to fabricate. Resistance is better over a wider range of concentrations
and temperatures compared to stainless steel.
|
Little resistance to
chlorides, and resistance at higher temperatures could be improved.
|
|
Titanium
|
Very good resistance
to chlorides (widely used in seawater applications). Strength allows it to be
fabricated at smaller thicknesses.
|
While the material
is moderately expensive, fabrication is difficult. Much of cost will be in
welding labor.
|
|
Pd stabilized
Titanium
|
Superior resistance
to chlorides, even at higher temperatures. Is often used on sea water
application where Titanium's resistance may not be acceptable.
|
Very expensive
material and fabrication is again difficult and expensive.
|
|
Nickel
|
Very good resistance
to high temperature caustic streams.
|
Moderate to high
expense. Difficult to weld.
|
|
Hastelloy Alloy
|
Very wide range to
choose from. Some have been specifically developed for acid services where
other materials have failed.
|
Fairly expensive
alloys. Their use must be justified. Most are easy to weld.
|
|
Graphite
|
One of the few
materials capable of withstanding weak HCl streams.
|
Brittle, very
expensive, and very difficult to fabricate. Some stream components have been
know to diffusion through some types of graphites.
|
|
Tantalum
|
Superior resistance
to very harsh services where no other material is acceptable.
|
Extremely expensive,
must be absolutely necessary.
|
Power = m z1 R T1 [({P2 / P2}a - 1)] / a
|
Eq. (4)
|
T1 is the inlet
temperature
R is the gas constant
z1 is the compressibility
m is the molar flow rate
a = (k-1)/k
k = Cp/Cv
65% at compression ratios of 1.5
75% at compression ratios of 2.0
80-85% at compression ratios between 3 and 6
k =0.20 for P >90 torr, 0.08 for 3 < P < 20 torr, and 0.025 for P < 1 torr
V = equipment volume in cubic feet
Leakage = air leakage into equipment in lb/h
R is the gas constant
z1 is the compressibility
m is the molar flow rate
a = (k-1)/k
k = Cp/Cv
65% at compression ratios of 1.5
75% at compression ratios of 2.0
80-85% at compression ratios between 3 and 6
k =0.20 for P >90 torr, 0.08 for 3 < P < 20 torr, and 0.025 for P < 1 torr
V = equipment volume in cubic feet
Leakage = air leakage into equipment in lb/h
** Viscosities of organic
liquids vary widely with temperature
Liquid densities vary with temperature to this approximation
Materials of Construction
Compressors and Vacuum Equipment
A. The following chart is used to determine what type of
compressor is to be used:
B. Fans should be used to raise pressure about 3% (12 in water),
blowers to raise to less than 2.75 barg (40 psig), and compressors to higher
pressures.
C. The theoretical reversible adiabatic power is estimated by:
where:
D. The outlet for the adiabatic reversible flow, T2 = T1 (P2 / P1)a
E. Exit temperatures should not exceed 204 °C (400 °F).
F. For diatomic gases (Cp/Cv = 1.4) this corresponds to a
compression ratio of about 4
G. Compression ratios should be about the same in each stage for
a multistage unit, the ratio = (Pn / P1) 1/n, with n stages.
H. Efficiencies for reciprocating compressors are as follows:
I. Efficiencies of large centrifugal compressors handling 2.8 to
47 m3/s (6000-100,000 acfm) at suction is about 76-78%
J. Reciprocating piston vacuum pumps are generally capable of
vacuum to 1 torr absolute, rotary piston types can achieve vacuums of 0.001
torr.
K. Single stage jet ejectors are capable of vacuums to 100 torr
absolute, two stage to 10 torr, three stage to 1 torr, and five stage to 0.05
torr.
L. A three stage ejector requires about 100 lb steam/lb air to
maintain a pressure of 1 torr.
M. Air leakage into vacuum equipment can be approximated as
follows: Leakage = k V(2/3)
where:
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