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Chemical Engineering
Apparatus Design
BY: ABEBE EDESSA
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING ACADEMIC YEAR 2020
PRESSURE VESSELS
INTRODUCTION
▪ The pressure vessels (i.e. cylinders or tanks) are used to store
fluids under pressure.
▪ The pressure vessels are designed with great care because rupture
of a pressure vessel means an explosion which may cause loss of life
and property.
▪ The material of pressure vessels may be brittle such as cast iron,
or ductile such as mild steel.
By: ABEBE EDESSA
2
ACADEMIC YEAR 2020
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
They are used in a variety of industries like
▪Petroleum refining
▪Chemical
▪Power
▪Food & beverage
▪Pharmaceutical
3
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Classification of Pressure Vessels
According to the dimensions:
The pressure vessels, according to their dimensions, may be
classified as thin shell or thick shell.
If the wall thickness of the shell (t) is less than 1/10 of the
diameter of the shell (d), then it is called a thin shell.
If the wall thickness of the shell is greater than 1/10 of the
diameter of the shell, then it is said to be a thick shell.
4
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
According to the end construction:
The pressure vessels, according to the end construction,
may be classified as open end or closed end.
A simple cylinder with a piston, such as cylinder of a press
is an example of an open end vessel, whereas a tank is an
example of a closed end vessel.
5
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
There are three main types of pressure vessels in general
❑Horizontal Pressure Vessels
❑Vertical Pressure Vessels
❑Spherical Pressure vessels
However there are some special types of Vessels like Regeneration
Tower, Reactors but these names are given according to their use
only.
6
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
HORIZONTAL PRESSURE VESSEL
7
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
VERTICAL PRESSURE VESSEL
8
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
SPHERICAL PRESSURIZED STORAGE VESSEL
9
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
MAIN COMPONENTS OF PRESSURE VESSEL
The main pressure vessel components are as follow:
✓ Shell
✓ Head
✓ Nozzle
✓ Support
10
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
Shell
The shell is the primary component that contains the pressure.
Pressure vessel shells are welded together to form a structure that
has a common rotational axis. Most pressure vessel shells are
cylindrical, spherical and conical in shape.
11
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Head
All pressure vessel shells must be closed at the ends by heads (or
another shell section). Heads are typically curved rather than flat.
Curved configurations are stronger and allow the heads to be
thinner, lighter, and less expensive than flat heads.
Heads can also be used inside a vessel. Heads are usually categorized
by their shapes. Ellipsoidal, Hemispherical, Torispherical, Conical,
Toriconical and flat are the common types of heads. Ellipsoidal (2:1)
would be the most common type of heads, which is used during the
designing of pressure vessels.
12
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
13
Types of Heads
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Nozzle
A nozzle is a cylindrical component that penetrates the shell or heads
of a pressure vessel. The nozzle ends are usually flanged to allow for
the necessary connections and to permit easy disassembly for
maintenance or access.
Nozzles are used for the following applications:
▪ Attach piping for flow into or out of the vessel.
▪ Attach instrument connections, (e.g., level gauges or pressure gauges).
▪ Provide access to the vessel interior at manways.
▪ Provide for direct attachment of other equipment items, (e.g., a heat
exchanger or mixer).
14
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Support
The type of support that is used depends primarily on the size and
orientation of the pressure vessel. In all cases, the pressure vessel
support must be adequate for the applied weight, wind, and
earthquake loads.
Typical kinds of supports are as follow:
➢ Saddle
➢ Leg
➢ Skirt
➢ Lug
15
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Saddle
Horizontal drums are typically supported at two locations by saddle
supports. A saddle support spreads the weight load over a large area
of the shell to prevent an excessive local stress in the shell at the
support points. The width of the saddle, among other design details, is
determined by the specific size and design conditions of the pressure
vessel. One saddle support is normally fixed or anchored to its
foundation. The other support is normally free to permit unrestrained
longitudinal thermal expansion of the drum.
16
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
17
A typical scheme of saddle support
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Leg
Small vertical drums are typically supported on legs that are welded
to the lower portion of the shell. The maximum ratio of support leg
length to drum diameter is typically 2:1. The number of legs needed
depends on the drum size and the loads to be carried.
Support legs are also typically used for spherical pressurized storage
vessels. The support legs for small vertical drums and spherical
pressurized storage vessels may be made from structural steel
columns or pipe sections, whichever provides a more efficient design.
Cross bracing between the legs is typically used to help absorb wind
or earthquake loads
18
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Skirt
Tall, vertical, cylindrical pressure vessels (e.g., the tower and reactor)
are typically supported by skirts. A support skirt is a cylindrical shell
section that is welded either to the lower portion of the vessel shell
or to the bottom head (for cylindrical vessels).
Skirts for spherical vessels are welded to the vessel near the mid-
plane of the shell. The skirt is normally long enough to provide enough
flexibility so that radial thermal expansion of the shell does not cause
high thermal stresses at its junction with the skirt
19
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Lug
Lugs that are welded to the pressure vessel shell and used to support
vertical pressure vessels. The use of lugs is typically limited to vessels
of small to medium diameter (1 to 10 ft.) and moderate height-to-
diameter ratios in the range of 2:1 to 5:1.
Lug supports are often used for vessels of this size that are located
above grade within structural steel. The lugs are typically bolted to
horizontal structural members to provide stability against overturning
loads; however, the bolt holes are often slotted to permit free radial
thermal expansion of the drum
20
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
21
Typical Scheme of lug
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Thin Cylindrical Shell under Internal Pressure
The analysis of stresses induced in a thin cylindrical shell are made on
the following assumptions:
➢ The effect of curvature of the cylinder wall is neglected.
➢ The tensile stresses are uniformly distributed over the section of the
walls.
➢ The effect of the restraining action of the heads at the end of the
pressure vessel is neglected.
When a thin cylindrical shell is subjected to an internal pressure, it is
likely to fail in the following two ways:
➢ It may fail along the longitudinal section (i.e. circumferentially) splitting
the cylinder into two troughs, as shown in Fig. a.
➢ It may fail across the transverse section (i.e. longitudinally) splitting
the cylinder into two cylindrical shells, as shown in Fig. b.
22
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
23
Failure of a cylindrical shell
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
24
Circumferential or Hoop Stress
A tensile stress acting in a direction tangential to the circumference
is called circumferential or hoop stress. In other words, it is a
tensile stress on longitudinal section (or on the cylindrical walls).
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY By: ABEBE EDESSA
25
Total force acting on longitudinal section
= 𝐼𝑛𝑡𝑒𝑛𝑠𝑖𝑡𝑦 𝑜𝑓 𝑝𝑟𝑒𝑠𝑠𝑢𝑟𝑒 × 𝑃𝑟𝑜𝑗𝑒𝑐𝑡𝑒𝑑 𝑎𝑟𝑒𝑎 = 𝑃 × 𝐷 × 𝑙 (i)
Total resisting force acting on the cylinder walls
= 𝜎 × 2𝑡 × 𝑙 (ii)
From equations (i) and (ii), we have
𝜎 × 2𝑡 × 𝑙 = 𝑝 × 𝐷 × 𝑙 or
𝜎 =
𝑃𝐷
2𝑡
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
26
Longitudinal Stress
A tensile stress acting in the direction of the axis is called
longitudinal stress. In other words, it is a tensile stress acting on
the transverse or circumferential section Y-Y (or on the ends of the
vessel).
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
27
Total force acting on transverse section
= 𝐼𝑛𝑡𝑒𝑛𝑠𝑖𝑡𝑦 𝑜𝑓 𝑝𝑟𝑒𝑠𝑠𝑢𝑟𝑒 × 𝐶𝑟𝑜𝑠𝑠 𝑠𝑒𝑐𝑡𝑖𝑜𝑛𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝑃 ×
𝜋
4
× 𝐷2
(i)
Total resisting force
= 𝜎 × 𝜋 × 𝐷 × 𝑙 (ii)
From equations (i) and (ii), we have
𝜎 =
𝑃𝐷
4𝑡
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
Thick Cylindrical Shell under Internal Pressure
When a cylindrical shell of a pressure vessel, hydraulic cylinder, gun
barrel and a pipe is subjected to a very high internal fluid pressure, then
the walls of the cylinder must be made extremely heavy or thick.
In thin cylindrical shells, we have assumed that the tensile stresses are
uniformly distributed over the section of the walls. But in the case of
thick wall cylinders, the stress over the section of the walls cannot be
assumed to be uniformly distributed. They develop both tangential and
radial stresses with values which are dependent upon the radius of the
element under consideration.
The distribution of stress in a thick cylindrical shell, the tangential
stress is maximum at the inner surface and minimum at the outer
surface of the shell. The radial stress is maximum at the inner surface
and zero at the outer surface of the shell.
28
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
29
Stress distribution in thick cylindrical shells subjected to internal pressure
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
Lame’s equation.
Assuming that the longitudinal fibers of the cylindrical shell are
equally strained, Lame has shown that the tangential stress at any
radius x is:
and radial stress at any radius x
30
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
Since we are concerned with the internal pressure ( 𝑃𝑖 = 𝑃) only,
therefore substituting the value of external pressure, 𝑃𝑜 = 0.
Tangential stress at any radius x
Radial stress at any radius x
31
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
The tangential stress is always a tensile stress whereas the radial
stress is a compressive stress. The tangential stress is maximum
at the inner surface of the shell (i.e. when x = ri ) and it is
minimum at the outer surface of the shell (i.e. when x = ro).
Substituting the value of x = ri and x = ro in equation (i), we find
that the maximum tangential stress at the inner surface of the
shell.
Minimum tangential stress at the outer surface of the shell
32
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
The radial stress is maximum at the inner surface of the shell
and zero at the outer surface of the shell. Substituting the value
of x = ri and x = ro in equation (ii).
Maximum radial stress at the inner surface of the shell
Minimum radial stress at the outer surface of the shell
33
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
In designing a thick cylindrical shell of brittle material (e.g. cast iron,
hard steel and cast aluminum) with closed or open ends and in
accordance with the maximum normal stress theory failure, the
tangential stress induced in the cylinder wall
Since ro = ri + t, therefore substituting this value of ro in the above
expression:
The value of σt for brittle materials may be taken as 0.125 times the
ultimate tensile strength (σu).
34
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
In case of cylinders made of ductile material, Lame’s equation is
modified according to maximum shear stress theory.
Maximum principal stress at the inner surface
Minimum principal stress at the outer surface
Maximum shear stress
35
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
The value of shear stress (𝜏) is usually taken as one-half the
tensile stress (σt). Therefore the above expression may be
written as
From the above expression, if the internal pressure ( p) is
equal to or greater than the allowable working stress (σt or
τ), then no thickness of the cylinder wall will prevent failure.
Thus, it is impossible to design a cylinder to withstand fluid
pressure greater than the allowable working stress for a
given material.
36
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
OPTIMUM VESSEL PROPORTIONS
37
V =vessel volume, cu ft
P = internal pressure, PSlG
L=length, ft
D =diameter, ft
C =corrosion allowance, in.
F2 =vessel ratios
S =allowable stress, psi
E =joint efficiency
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
OPTIMUM VESSEL PROPORTIONS
38
Method
1. Calculate F2.
2. From Figure determine L/D
ratio.
3. From the L/D ratio, calculate the
diameter, D.
4. Use D and V to calculate the
required length, L.
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
39
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
External pressure on cylindrical shells causes compressive forces that
could lead to buckling. The equations for the buckling of cylindrical
shells under external pressure are extremely cumbersome to use
directly in design (Jawad, 1994). However, these equations can be
simplified for design purposes by plotting them so that the minimum
buckling strain is expressed in terms of length, diameter and
thickness of the cylinder. These plots are utilized by the ASME.
40
External pressure
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
41
For an open-ended cylinder, the critical pressure to cause buckling Pc
is given by the following expression; Windenburg and Trilling (1934):
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
42
External Pressure for Cylinders with 𝐷 𝑜/𝑡 ≥ 10
The ASME uses plots to express the lowest critical strain, A, in
terms of the ratios L/Do and Do/t of the cylinder. The designer
calculates the known quantities L/Do and Do/t and then uses the
figure to determine buckling strain. A. To correlate buckling strain
to allowable external pressure, the designer uses the stress-strain
diagram to obtain a B value.
The Allowable External Pressure
𝑷 = (𝟒/𝟑)(𝑩)(𝑫 𝒐/𝒕)
When A falls to the left of the curves, the value of P is determined
𝑷 = 𝟐𝑨𝑬/𝟑(𝑫 𝒐/𝒕)
E = Modulus of Elasticity
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
43
External Pressure for Cylinders with 𝐷 𝑜/𝑡 < 10
When Do/t is less than 10, the allowable external pressure is taken
as the smaller of the values determined from the following two
equations:
𝑷 𝒂𝟏 = Τ𝟐. 𝟏𝟔𝟕 Τ𝑫 𝒐 𝒕 − 𝟎. 𝟎𝟖𝟑𝟑 𝑩
𝑷 𝒂𝟐 =
𝟐𝑺
Τ𝑫 𝒐 𝒕
Τ𝟏 − 𝟏 Τ𝑫 𝒐 𝒕
Where B is obtained as discussed above. For values of (Do/t) of less
than or equal to 4, the A value is calculated from
𝑨 = 𝟏. 𝟏/( Τ𝑫 𝒐 𝒕) 𝟐
For values of A greater than 0.10, use a value of 0.10
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
44
External Pressure for Cylinders with 𝐷 𝑜/𝑡 < 10
The value of S is taken as the smaller of two times the allowable
tensile stress, or 0.9 times the yield stress of the material at the
design temperature.
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
45
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
46
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
47
The major sources of dead weight loads are:
1. The vessel shell.
2. The vessel fittings: manways, nozzles.
3. Internal fittings: plates (plus the fluid on the plates);
heating and cooling coils.
4. External fittings: ladders, platforms, piping.
5. Auxiliary equipment which is not self-supported;
condensers, agitators.
6. Insulation.
7. The weight of liquid to fill the vessel
Weight loads
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
48
Weight loads
The approximate weight of a cylindrical vessel with domed ends, and
uniform wall thickness, can be estimated from the following equation:
For a steel vessel
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
49
Wind Loads (Tall Vessels)
The vessel under wind loading acts as a cantilever beam. For a
uniformly loaded cantilever the bending moment at any plane is
given by:
where x is the distance measured from the free end and w the
load per unit length (Newtons per meter run).
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
50
Dynamic wind pressure
The load imposed on any structure by the action of the wind will
depend on the shape of the structure and the wind velocity.
Wind Loads (Tall Vessels)
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
51
A wind speed of 160 km/h (100 mph) can be used for preliminary
design studies; equivalent to a wind pressure of 1280 N/m2 (25
lb/ft2).
The loading per unit length of the column can be obtained from the
wind pressure by multiplying by the effective column diameter: the
outside diameter plus an allowance for the thermal insulation and
attachments, such as pipes and ladders.
Wind Loads (Tall Vessels)
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
52
Stresses Analysis
Pressure stresses:
Dead weight stress: Bending stresses:
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING
By: ABEBE EDESSA
53
DIRE DAWA UNIVERSITY
INSTITUTE OF TECHNOLOGY
SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA

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Chemical engineering apparatus desisgn

  • 1. Chemical Engineering Apparatus Design BY: ABEBE EDESSA DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING ACADEMIC YEAR 2020
  • 2. PRESSURE VESSELS INTRODUCTION ▪ The pressure vessels (i.e. cylinders or tanks) are used to store fluids under pressure. ▪ The pressure vessels are designed with great care because rupture of a pressure vessel means an explosion which may cause loss of life and property. ▪ The material of pressure vessels may be brittle such as cast iron, or ductile such as mild steel. By: ABEBE EDESSA 2 ACADEMIC YEAR 2020 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING
  • 3. They are used in a variety of industries like ▪Petroleum refining ▪Chemical ▪Power ▪Food & beverage ▪Pharmaceutical 3 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 4. Classification of Pressure Vessels According to the dimensions: The pressure vessels, according to their dimensions, may be classified as thin shell or thick shell. If the wall thickness of the shell (t) is less than 1/10 of the diameter of the shell (d), then it is called a thin shell. If the wall thickness of the shell is greater than 1/10 of the diameter of the shell, then it is said to be a thick shell. 4 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 5. According to the end construction: The pressure vessels, according to the end construction, may be classified as open end or closed end. A simple cylinder with a piston, such as cylinder of a press is an example of an open end vessel, whereas a tank is an example of a closed end vessel. 5 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 6. There are three main types of pressure vessels in general ❑Horizontal Pressure Vessels ❑Vertical Pressure Vessels ❑Spherical Pressure vessels However there are some special types of Vessels like Regeneration Tower, Reactors but these names are given according to their use only. 6 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 7. HORIZONTAL PRESSURE VESSEL 7 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 8. VERTICAL PRESSURE VESSEL 8 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 9. SPHERICAL PRESSURIZED STORAGE VESSEL 9 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 10. MAIN COMPONENTS OF PRESSURE VESSEL The main pressure vessel components are as follow: ✓ Shell ✓ Head ✓ Nozzle ✓ Support 10 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 11. Shell The shell is the primary component that contains the pressure. Pressure vessel shells are welded together to form a structure that has a common rotational axis. Most pressure vessel shells are cylindrical, spherical and conical in shape. 11 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 12. Head All pressure vessel shells must be closed at the ends by heads (or another shell section). Heads are typically curved rather than flat. Curved configurations are stronger and allow the heads to be thinner, lighter, and less expensive than flat heads. Heads can also be used inside a vessel. Heads are usually categorized by their shapes. Ellipsoidal, Hemispherical, Torispherical, Conical, Toriconical and flat are the common types of heads. Ellipsoidal (2:1) would be the most common type of heads, which is used during the designing of pressure vessels. 12 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 13. 13 Types of Heads DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 14. Nozzle A nozzle is a cylindrical component that penetrates the shell or heads of a pressure vessel. The nozzle ends are usually flanged to allow for the necessary connections and to permit easy disassembly for maintenance or access. Nozzles are used for the following applications: ▪ Attach piping for flow into or out of the vessel. ▪ Attach instrument connections, (e.g., level gauges or pressure gauges). ▪ Provide access to the vessel interior at manways. ▪ Provide for direct attachment of other equipment items, (e.g., a heat exchanger or mixer). 14 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 15. Support The type of support that is used depends primarily on the size and orientation of the pressure vessel. In all cases, the pressure vessel support must be adequate for the applied weight, wind, and earthquake loads. Typical kinds of supports are as follow: ➢ Saddle ➢ Leg ➢ Skirt ➢ Lug 15 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 16. Saddle Horizontal drums are typically supported at two locations by saddle supports. A saddle support spreads the weight load over a large area of the shell to prevent an excessive local stress in the shell at the support points. The width of the saddle, among other design details, is determined by the specific size and design conditions of the pressure vessel. One saddle support is normally fixed or anchored to its foundation. The other support is normally free to permit unrestrained longitudinal thermal expansion of the drum. 16 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 17. 17 A typical scheme of saddle support DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 18. Leg Small vertical drums are typically supported on legs that are welded to the lower portion of the shell. The maximum ratio of support leg length to drum diameter is typically 2:1. The number of legs needed depends on the drum size and the loads to be carried. Support legs are also typically used for spherical pressurized storage vessels. The support legs for small vertical drums and spherical pressurized storage vessels may be made from structural steel columns or pipe sections, whichever provides a more efficient design. Cross bracing between the legs is typically used to help absorb wind or earthquake loads 18 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 19. Skirt Tall, vertical, cylindrical pressure vessels (e.g., the tower and reactor) are typically supported by skirts. A support skirt is a cylindrical shell section that is welded either to the lower portion of the vessel shell or to the bottom head (for cylindrical vessels). Skirts for spherical vessels are welded to the vessel near the mid- plane of the shell. The skirt is normally long enough to provide enough flexibility so that radial thermal expansion of the shell does not cause high thermal stresses at its junction with the skirt 19 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 20. Lug Lugs that are welded to the pressure vessel shell and used to support vertical pressure vessels. The use of lugs is typically limited to vessels of small to medium diameter (1 to 10 ft.) and moderate height-to- diameter ratios in the range of 2:1 to 5:1. Lug supports are often used for vessels of this size that are located above grade within structural steel. The lugs are typically bolted to horizontal structural members to provide stability against overturning loads; however, the bolt holes are often slotted to permit free radial thermal expansion of the drum 20 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 21. 21 Typical Scheme of lug DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 22. Thin Cylindrical Shell under Internal Pressure The analysis of stresses induced in a thin cylindrical shell are made on the following assumptions: ➢ The effect of curvature of the cylinder wall is neglected. ➢ The tensile stresses are uniformly distributed over the section of the walls. ➢ The effect of the restraining action of the heads at the end of the pressure vessel is neglected. When a thin cylindrical shell is subjected to an internal pressure, it is likely to fail in the following two ways: ➢ It may fail along the longitudinal section (i.e. circumferentially) splitting the cylinder into two troughs, as shown in Fig. a. ➢ It may fail across the transverse section (i.e. longitudinally) splitting the cylinder into two cylindrical shells, as shown in Fig. b. 22 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 23. 23 Failure of a cylindrical shell DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 24. 24 Circumferential or Hoop Stress A tensile stress acting in a direction tangential to the circumference is called circumferential or hoop stress. In other words, it is a tensile stress on longitudinal section (or on the cylindrical walls). DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY By: ABEBE EDESSA
  • 25. 25 Total force acting on longitudinal section = 𝐼𝑛𝑡𝑒𝑛𝑠𝑖𝑡𝑦 𝑜𝑓 𝑝𝑟𝑒𝑠𝑠𝑢𝑟𝑒 × 𝑃𝑟𝑜𝑗𝑒𝑐𝑡𝑒𝑑 𝑎𝑟𝑒𝑎 = 𝑃 × 𝐷 × 𝑙 (i) Total resisting force acting on the cylinder walls = 𝜎 × 2𝑡 × 𝑙 (ii) From equations (i) and (ii), we have 𝜎 × 2𝑡 × 𝑙 = 𝑝 × 𝐷 × 𝑙 or 𝜎 = 𝑃𝐷 2𝑡 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 26. 26 Longitudinal Stress A tensile stress acting in the direction of the axis is called longitudinal stress. In other words, it is a tensile stress acting on the transverse or circumferential section Y-Y (or on the ends of the vessel). DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 27. 27 Total force acting on transverse section = 𝐼𝑛𝑡𝑒𝑛𝑠𝑖𝑡𝑦 𝑜𝑓 𝑝𝑟𝑒𝑠𝑠𝑢𝑟𝑒 × 𝐶𝑟𝑜𝑠𝑠 𝑠𝑒𝑐𝑡𝑖𝑜𝑛𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝑃 × 𝜋 4 × 𝐷2 (i) Total resisting force = 𝜎 × 𝜋 × 𝐷 × 𝑙 (ii) From equations (i) and (ii), we have 𝜎 = 𝑃𝐷 4𝑡 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING
  • 28. Thick Cylindrical Shell under Internal Pressure When a cylindrical shell of a pressure vessel, hydraulic cylinder, gun barrel and a pipe is subjected to a very high internal fluid pressure, then the walls of the cylinder must be made extremely heavy or thick. In thin cylindrical shells, we have assumed that the tensile stresses are uniformly distributed over the section of the walls. But in the case of thick wall cylinders, the stress over the section of the walls cannot be assumed to be uniformly distributed. They develop both tangential and radial stresses with values which are dependent upon the radius of the element under consideration. The distribution of stress in a thick cylindrical shell, the tangential stress is maximum at the inner surface and minimum at the outer surface of the shell. The radial stress is maximum at the inner surface and zero at the outer surface of the shell. 28 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 29. 29 Stress distribution in thick cylindrical shells subjected to internal pressure DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 30. Lame’s equation. Assuming that the longitudinal fibers of the cylindrical shell are equally strained, Lame has shown that the tangential stress at any radius x is: and radial stress at any radius x 30 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 31. Since we are concerned with the internal pressure ( 𝑃𝑖 = 𝑃) only, therefore substituting the value of external pressure, 𝑃𝑜 = 0. Tangential stress at any radius x Radial stress at any radius x 31 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 32. The tangential stress is always a tensile stress whereas the radial stress is a compressive stress. The tangential stress is maximum at the inner surface of the shell (i.e. when x = ri ) and it is minimum at the outer surface of the shell (i.e. when x = ro). Substituting the value of x = ri and x = ro in equation (i), we find that the maximum tangential stress at the inner surface of the shell. Minimum tangential stress at the outer surface of the shell 32 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 33. The radial stress is maximum at the inner surface of the shell and zero at the outer surface of the shell. Substituting the value of x = ri and x = ro in equation (ii). Maximum radial stress at the inner surface of the shell Minimum radial stress at the outer surface of the shell 33 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 34. In designing a thick cylindrical shell of brittle material (e.g. cast iron, hard steel and cast aluminum) with closed or open ends and in accordance with the maximum normal stress theory failure, the tangential stress induced in the cylinder wall Since ro = ri + t, therefore substituting this value of ro in the above expression: The value of σt for brittle materials may be taken as 0.125 times the ultimate tensile strength (σu). 34 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 35. In case of cylinders made of ductile material, Lame’s equation is modified according to maximum shear stress theory. Maximum principal stress at the inner surface Minimum principal stress at the outer surface Maximum shear stress 35 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 36. The value of shear stress (𝜏) is usually taken as one-half the tensile stress (σt). Therefore the above expression may be written as From the above expression, if the internal pressure ( p) is equal to or greater than the allowable working stress (σt or τ), then no thickness of the cylinder wall will prevent failure. Thus, it is impossible to design a cylinder to withstand fluid pressure greater than the allowable working stress for a given material. 36 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 37. OPTIMUM VESSEL PROPORTIONS 37 V =vessel volume, cu ft P = internal pressure, PSlG L=length, ft D =diameter, ft C =corrosion allowance, in. F2 =vessel ratios S =allowable stress, psi E =joint efficiency DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 38. OPTIMUM VESSEL PROPORTIONS 38 Method 1. Calculate F2. 2. From Figure determine L/D ratio. 3. From the L/D ratio, calculate the diameter, D. 4. Use D and V to calculate the required length, L. DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 39. 39 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 40. External pressure on cylindrical shells causes compressive forces that could lead to buckling. The equations for the buckling of cylindrical shells under external pressure are extremely cumbersome to use directly in design (Jawad, 1994). However, these equations can be simplified for design purposes by plotting them so that the minimum buckling strain is expressed in terms of length, diameter and thickness of the cylinder. These plots are utilized by the ASME. 40 External pressure DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 41. 41 For an open-ended cylinder, the critical pressure to cause buckling Pc is given by the following expression; Windenburg and Trilling (1934): DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 42. 42 External Pressure for Cylinders with 𝐷 𝑜/𝑡 ≥ 10 The ASME uses plots to express the lowest critical strain, A, in terms of the ratios L/Do and Do/t of the cylinder. The designer calculates the known quantities L/Do and Do/t and then uses the figure to determine buckling strain. A. To correlate buckling strain to allowable external pressure, the designer uses the stress-strain diagram to obtain a B value. The Allowable External Pressure 𝑷 = (𝟒/𝟑)(𝑩)(𝑫 𝒐/𝒕) When A falls to the left of the curves, the value of P is determined 𝑷 = 𝟐𝑨𝑬/𝟑(𝑫 𝒐/𝒕) E = Modulus of Elasticity DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 43. 43 External Pressure for Cylinders with 𝐷 𝑜/𝑡 < 10 When Do/t is less than 10, the allowable external pressure is taken as the smaller of the values determined from the following two equations: 𝑷 𝒂𝟏 = Τ𝟐. 𝟏𝟔𝟕 Τ𝑫 𝒐 𝒕 − 𝟎. 𝟎𝟖𝟑𝟑 𝑩 𝑷 𝒂𝟐 = 𝟐𝑺 Τ𝑫 𝒐 𝒕 Τ𝟏 − 𝟏 Τ𝑫 𝒐 𝒕 Where B is obtained as discussed above. For values of (Do/t) of less than or equal to 4, the A value is calculated from 𝑨 = 𝟏. 𝟏/( Τ𝑫 𝒐 𝒕) 𝟐 For values of A greater than 0.10, use a value of 0.10 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 44. 44 External Pressure for Cylinders with 𝐷 𝑜/𝑡 < 10 The value of S is taken as the smaller of two times the allowable tensile stress, or 0.9 times the yield stress of the material at the design temperature. DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 45. 45 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 46. 46 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 47. 47 The major sources of dead weight loads are: 1. The vessel shell. 2. The vessel fittings: manways, nozzles. 3. Internal fittings: plates (plus the fluid on the plates); heating and cooling coils. 4. External fittings: ladders, platforms, piping. 5. Auxiliary equipment which is not self-supported; condensers, agitators. 6. Insulation. 7. The weight of liquid to fill the vessel Weight loads DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 48. 48 Weight loads The approximate weight of a cylindrical vessel with domed ends, and uniform wall thickness, can be estimated from the following equation: For a steel vessel DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 49. 49 Wind Loads (Tall Vessels) The vessel under wind loading acts as a cantilever beam. For a uniformly loaded cantilever the bending moment at any plane is given by: where x is the distance measured from the free end and w the load per unit length (Newtons per meter run). DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 50. 50 Dynamic wind pressure The load imposed on any structure by the action of the wind will depend on the shape of the structure and the wind velocity. Wind Loads (Tall Vessels) DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 51. 51 A wind speed of 160 km/h (100 mph) can be used for preliminary design studies; equivalent to a wind pressure of 1280 N/m2 (25 lb/ft2). The loading per unit length of the column can be obtained from the wind pressure by multiplying by the effective column diameter: the outside diameter plus an allowance for the thermal insulation and attachments, such as pipes and ladders. Wind Loads (Tall Vessels) DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 52. 52 Stresses Analysis Pressure stresses: Dead weight stress: Bending stresses: DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA
  • 53. 53 DIRE DAWA UNIVERSITY INSTITUTE OF TECHNOLOGY SCHOOL OF CHEMICAL AND BIO ENGINEERING By: ABEBE EDESSA