SECTION 3—DESIGN
3.1 JOINTS
3.1.1 Definitions
The definitions in 3.1.1.1 through 3.1.1.8 apply to tank
joint designs (see 7.1 for definitions that apply to welders and
welding procedures).
3.1.1.1 double-welded butt joint:
A joint between two
abutting parts lying in approximately the same plane that is
welded from both sides.
3.1.1.2 single-welded butt joint with backing:
A
joint between two abutting parts lying in approximately the
same plane that is welded from one side only with the use of a
strip bar or another suitable backing material.
3.1.1.3 double-welded lap joint:
A joint between two
overlapping members in which the overlapped edges of both
members are welded with fillet welds.
3.1.1.4 single-welded lap joint:
A joint between two
overlapping members in which the overlapped edge of one
member is welded with a fillet weld.
3.1.1.5 butt-weld:
A weld placed in a groove between
two abutting members. Grooves may be square, V-shaped
(single or double), or U-shaped (single or double), or they
may be either single or double beveled.
3.1.1.6 fillet weld:
A weld of approximately triangular
cross section that joins two surfaces at approximately right
angles, as in a lap joint, tee joint, or corner joint.
3.1.1.7 full-fillet weld:
A fillet weld whose size is equal
to the thickness of the thinner joined member.
3.1.1.8 tack weld:
A weld made to hold the parts of a
weldment in proper alignment until the final welds are made.
3.1.2 Weld Size
3.1.2.1
The size of a groove weld shall be based on the
joint penetration (that is, the depth of chamfering plus the
root penetration when specified).
3.1.2.2
The size of an equal-leg fillet weld shall be based
on the leg length of the largest isosceles right triangle that can
be inscribed within the cross section of the fillet weld. The
size of an unequal-leg fillet weld shall be based on the leg
lengths of the largest right triangle that can be inscribed
within the cross section of the fillet weld.
3.1.3 Restrictions on Joints
3.1.3.1
Restrictions on the type and size of welded joints
are given in 3.1.3.2 through 3.1.3.5.
3.1.3.2
Tack welds shall not be considered as having any
strength value in the finished structure.
3.1.3.3
The minimum size of fillet welds shall be as follows:
On plates 5 mm (
3
/
16
in.) thick, the weld shall be a full-fillet
weld, and on plates more than 5 mm (
3
/
16
in.) thick, the weld
thickness shall not be less than one-third the thickness of the
thinner plate at the joint and shall be at least 5 mm (
3
/
16
in.).
3.1.3.4
Single-welded lap joints are permissible only on
bottom plates and roof plates.
3.1.3.5
Lap-welded joints, as tack-welded, shall be lapped
at least five times the nominal thickness of the thinner plate
joined; however, with double-welded lap joints, the lap need
not exceed 50 mm (2 in.), and with single-welded lap joints,
the lap need not exceed 25 mm (1 in.).
3.1.4 Welding Symbols
Welding symbols used on drawings shall be the symbols of
the American Welding Society.
3.1.5 Typical Joints
3.1.5.1 General
Typical tank joints are shown in Figures 3-1, 3-2, 3-3A, 3-
3B, and 3-3C. The wide faces of nonsymmetrical V- or U-butt
joints may be on the outside or the inside of the tank shell at
the option of the manufacturer. The tank shell shall be
designed so that all courses are truly vertical.
3.1.5.2 Vertical Shell Joints
a. Vertical shell joints shall be butt joints with complete penetration
and complete fusion attained by double welding or
other means that will obtain the same quality of deposited
weld metal on the inside and outside weld surfaces to meet
the requirements of 5.2.1 and 5.2.3. The suitability of the
plate preparation and welding procedure shall be determined
in accordance with 7.2.
b. Vertical joints in adjacent shell courses shall not be aligned
but shall be offset from each other a minimum distance of 5
t
,
where
t
is the plate thickness of the thicker course at the point
of offset.
3.1.5.3 Horizontal Shell Joints
a. Horizontal shell joints shall have complete penetration and
complete fusion; however, as an alternative, top angles may
be attached to the shell by a double-welded lap joint. The
suitability of the plate preparation and welding procedure
shall be determined in accordance with 7.2.
b. Unless otherwise specified, abutting shell plates at horizontal
joints shall have a common vertical centerline.
3.1.5.4 Lap-Welded Bottom Joints
Lap-welded bottom plates shall be reasonably rectangular.
Additionally, plate may be either square cut or may have mill
edges. Mill edges to be welded shall be relatively smooth and
uniform, free of deleterious deposits, and have a shape such
that a full fillet weld can be achieved. Three-plate laps in tank
05
3-2 API S
TANDARD
650
bottoms shall be at least 300 mm (12 in.) from each other,
from the tank shell, from butt-welded annular-plate joints,
and from joints between annular plates and the bottom. Lapping
of two bottom plates on the butt-welded annular plates
does not constitute a three-plate lap weld. When annular
plates are used or are required by 3.5.1, they shall be buttwelded
and shall have a radial width that provides at least 600
mm (24 in.) between the inside of the shell and any lapwelded
joint in the remainder of the bottom. Bottom plates
need to be welded on the top side only, with a continuous fullfillet
weld on all seams. Unless annular bottom plates are
used, the bottom plates under the bottom shell ring shall have
the outer ends of the joints fitted and lap-welded to form a
smooth bearing for the shell plates, as shown in Figure 3-3B.
3.1.5.5 Butt-Welded Bottom Joints
Butt-welded bottom plates shall have their parallel edges
prepared for butt welding with either square or V grooves.
Butt-welds shall be made using an appropriate weld joint configuration
that yields a complete penetration weld. Typical
permissible bottom butt-welds without a backing strip are the
same as those shown in Figure 3-1. The use of a backing strip
at least 3 mm (
1
/
8
in.) thick tack welded to the underside of the
plate is permitted. Butt-welds using a backing strip are shown
in Figure 3-3A. If square grooves are employed, the root openings
shall not be less than 6 mm (
1
/
4
in.). A metal spacer shall
be used to maintain the root opening between the adjoining
plate edges unless the manufacturer submits another method
of butt-welding the bottom for the purchaser’s approval.
Three-plate joints in the tank bottom shall be at least 300 mm
(12 in.) from each other and from the tank shell.
3.1.5.6 Bottom Annular-Plate Joints
Bottom annular-plate radial joints shall be butt-welded in
accordance with 3.1.5.5 and shall have complete penetration
and complete fusion. The backing strip, if used, shall be compatible
for welding the annular plates together.
3.1.5.7 Shell-to-Bottom Fillet Welds
a. For bottom and annular plates with a nominal thickness
12.5 mm (
1
/
2
in.), and less, the attachment between the bottom
edge of the lowest course shell plate and the bottom plate
shall be a continuous fillet weld laid on each side of the shell
plate. The size of each weld shall not be more than 12.5 mm
(
1
/
2
in.) and shall not be less than the nominal thickness of the
thinner of the two plates joined (that is, the shell plate or the
bottom plate immediately under the shell) or less than the following
values:
Nominal Thickness
of Shell Plate
Minimum Size of
Fillet Weld
(mm) (in.) (mm) (in.)
5 0.1875 5
3
/
16
> 5 to 20 > 0.1875 to 0.75 6
1
/
4
> 20 to 32 > 0.75 to 1.25 8
5
/
16
> 32 to 45 > 1.25 to 1.75 10
3
/
8
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01
Figure 3-1—Typical Vertical Shell Joints
Figure 3-2—Typical Horizontal Shell Joints
Single-V butt joint
Single-U butt joint
Double-V butt joint
Square-groove butt joint Double-U butt joint
Note: See 3.1.5.2 for specific requirements for vertical shell joints.
Optional
outside angle
Angle-to-shell
butt joint
complete penetration
Alternative
angle-to-shell joint
Square-groove
butt joint
complete penetration
Single-bevel
butt joint
complete penetration
Double-bevel
butt joint
complete penetration
Note: See 3.1.5.3 for specific requirements for horizontal
shell joints.
W
ELDED
S
TEEL
T
ANKS
FOR
O
IL
S
TORAGE
3-3
b. For annular plates with a nominal thickness greater than
12.5 mm (
1
/
2
in.), the attachment welds shall be sized so that
either the legs of the fillet welds or the groove depth plus the
leg of the fillet for a combined weld is of a size equal to the
annular-plate thickness (see Figure 3-3C), but shall not
exceed the shell plate thickness.
c. Shell-to-bottom fillet welds for shell material in Groups
IV, IVA, V, or VI shall be made with a minimum of two
passes.
d. Shell-to-bottom fillet weld around low-type reinforcing
pads shown in Figure 3-5, Details a and b or around shell
insert plates that extend beyond the outside surface of the
adjacent tank shell shall be sized as required by paragraphs a,
b or c.
e. The bottom or annular plates shall be sufficient to provide
a minimum 13 mm (
1
/
2
in.) from the toe of the fillet weld referenced
in 3.1.5.7d to the outside edge of the bottom or
annular plates.
3.1.5.8 Wind Girder Joints
a. Full-penetration butt-welds shall be used for joining ring
sections.
b. Continuous welds shall be used for all horizontal top-side
joints and for all vertical joints. Horizontal bottom-side joints
shall be seal-welded if specified by the purchaser. Seal-welding
should be considered to minimize the potential for
entrapped moisture, which may cause corrosion.
3.1.5.9 Roof and Top-Angle Joints
a. Roof plates shall, as a minimum, be welded on the top side
with a continuous full-fillet weld on all seams. Butt-welds are
also permitted.
b. Roof plates shall be attached to the top angle of a tank
with a continuous fillet weld on the top side only, as specified
in 3.10.2.5.
c. The top-angle sections for self-supporting roofs shall be
joined by butt-welds having complete penetration and fusion.
Joint efficiency factors need not be applied in conforming to
the requirements of 3.10.5 and 3.10.6.
Figure 3-3A—Typical Roof and Bottom Joints
ROOF-PLATE JOINT
ROOF-TO-SHELL JOINTS
ALTERNATIVE ROOF-TO-SHELL JOINT
(SEE NOTE 2)
BOTTOM-TO-SHELL JOINT
BOTTOM-PLATE JOINTS
Single-welded
full-fillet lap joint
Single-welded butt joint
with backing strip
Optional
V groove
Bottom or annular Inside
bottom plate
12
t
1.75
t ≤ R ≤ 3t
Inside of shell
t
t
Optional
outside angle
Inside
Tack weld
Notes:
1. See 3.1.5.4 through 3.1.5.9 for specific requirements for roof
and bottom joints.
2. The alternative roof-to-shell joint is subject to the limitations of
3.1.5.9, item f.
Figure 3-3B—Method for Preparing Lap-Welded
Bottom Plates Under Tank Shell (See 3.1.5.4)
Shell plate
Bottom plate
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TANDARD
650
d. At the option of the manufacturer, for self-supporting
roofs of the cone, dome, or umbrella type, the edges of the
roof plates may be flanged horizontally to rest flat against the
top angle to improve welding conditions.
e. Except as specified for open-top tanks in 3.9, for self-supporting
roofs in 3.10.5 and 3.10.6, and for tanks with the
flanged roof-to-shell detail described in item f below, tank
shells shall be supplied with top angles of not less than the
following sizes: for tanks with a diameter less than or equal to
11 m (35 ft), 51
・~
51
・~
4.8 mm (2
・~
2
・~
3
/
16
in.); for tanks
with a diameter greater than 11 m (35 ft) but less than or
equal to 18 m (60 ft), 51
・~
51
・~
6.4 mm (2
・~
2
・~
1
/
4
in.); and
for tanks with a diameter greater than 18 m (60 ft), 76
・~
76
・~
9.5 mm (3
・~
3
・~
3
/
8
in.). At the purchaser’s option, the outstanding
leg of the top angle may extend inside or outside the
tank shell.
f. For tanks with a diameter less than or equal to 9 m (30 ft)
and a supported cone roof (see 3.10.4), the top edge of the
shell may be flanged in lieu of installing a top angle. The
bend radius and the width of the flanged edge shall conform
to the details of Figure 3-3A. This construction may be used
for any tank with a self-supporting roof (see 3.10.5 and
3.10.6) if the total cross-sectional area of the junction fulfills
the stated area requirements for the construction of the top
angle. No additional member, such as an angle or a bar, shall
be added to the flanged roof-to-shell detail.
3.2 DESIGN CONSIDERATIONS
3.2.1 Loads
Loads are defined as follows:
a. Dead load (
D
L
): the weight of the tank or tank component,
including any corrosion allowance unless otherwise noted.
b. Stored liquid (
F
): the load due to filling the tank to the
design liquid level (see 3.6.3.2) with liquid with the design
specific gravity specified by the purchaser.
c. Hydrostatic test (
H
t
): the load due to filling the tank with
water to the design liquid level.
d. Minimum roof live load (
L
r
): 1.0 kPa (20 lbf/ft
2
) on the
horizontal projected area of the roof.
e. Snow (
S
): The ground snow load shall be determined from
ASCE 7, Figure 7-1 or Table 7-1 unless the ground snow load
that equals or exceeds the value based on a 2% annual probability
of being exceeded (50 year mean recurrence interval) is
specified by the purchaser. The design snow load shall be
0.84 times the ground snow load. Alternately, the design snow
load shall be determined from the ground snow load in accordance
with ASCE 7. The design snow load shall be reported
to the purchaser.
f. Wind (
W
): The design wind speed (
V
) shall be 190 km/hr
(120 mph), the 3 second gust design wind speed determined
from ASCE 7, Figure 6-1, or the 3-second gust design wind
speed specified by the purchaser [this specified wind speed
shall be for a 3-second gust based on a 2% annual probability
of being exceeded (50-year mean recurrence interval)]. The
design wind pressure shall be 0.86 kPa [
V
/190]
2
, [(18 lbf/
ft
2
)(
V
/120)
2
] on vertical projected areas of cylindrical surfaces
and 1.44 kPa (
V
/190)
2
, [(30 lbf/ft
2
)(
V
/120)
2
] uplift (see
item 2) on horizontal projected areas of conical or doubly
curved surfaces, where
V
is the 3-second gust wind speed.
The 3-second gust wind speed used shall be reported to the
purchaser.
1. These design wind pressures are in accordance with
ASCE 7 for wind exposure Category C. As an
alternative, pressures may be determined in accordance
with ASCE 7 (exposure category and importance
Figure 3-3C—Detail of Double Fillet-Groove Weld for Annular Bottom Plates With a Nominal
Thickness Greater Than 13 mm (
1
/
2
in.) (See 3.1.5.7, item b)
Shell plate
6 mm (
1/4 in.) minimum
13 mm (
1/2 in.) maximum
Annular bottom plate
A = B for
up to 25 mm
(1 in.) annular
plate
A + B minimum
B
A:
A
B
B
A
Notes:
1. A = Fillet weld size limited to 13 mm (
1/2 in.) maximum.
2. A + B = Thinner of shell or annular bottom plate thickness.
3. Groove weld B may exceed fillet size A only when annular plate is thicker than 25 mm (1 inch).
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W
ELDED STEEL TANKS FOR OIL STORAGE 3-5
factor provided by purchaser) or a national standard for
the specific conditions for the tank being designed.
2. The design uplift pressure on the roof (wind plus internal
pressure) need not exceed 1.6 times the design
pressure
P determined in F.4.1.
3. Windward and leeward horizontal wind loads on the
roof are conservatively equal and opposite and therefore
they are not included in these pressures.
4. Fastest mile wind speed times 1.2 is approximately
equal to 3 second gust wind speed.
g. Design internal pressure (
Pi): shall not exceed 18 kPa (2.5
lbf/in
2).
h. Test pressure (
Pt): as required by F.4.4 or F.7.6.
i. Design external pressure (
Pe): shall not be less than 0.25
kPa (1 in. of water) and shall not exceed 6.9 kPa (1.01 lbf/
in.
2)
j. Seismic (
E): seismic loads determined in accordance with
Appendix E.
3.2.2 Design Factors
The purchaser shall state the design metal temperature
(based on ambient temperature), the design specific gravity,
the corrosion allowance (if any), and the maximum design
temperature.
3.2.3 External Loads
The purchaser shall state the magnitude and direction of
external loads or restraint, if any, for which the shell or shell
connections must be designed. The design for such loadings
shall be a matter of agreement between the purchaser and the
manufacturer.
3.2.4 Protective Measures
The purchaser should give special consideration to foundations,
corrosion allowance, hardness testing, and any other
protective measures deemed necessary.
3.2.5 External Pressure
See Appendix V for minimum requirements in the design
of tanks subject to partial internal vacuum exceeding 0.25 kPa
(1 in. of water). Tanks that meet the requirements of this standard
may be subjected to a partial vacuum of 0.25 kPa (1 in.
of water), without the need to provide any additional supporting
calculations.
3.2.6 Tank Capacity
3.2.6.1
The purchaser shall specify the maximum capacity
and the overfill protection level (or volume) requirement (see
API Recommended Practice 2350).
3.2.6.2
Maximum capacity is the volume of product in a
tank when the tank is filled to its design liquid level as defined
in 3.6.3.2 (see Appendix L).
3.2.6.3
The net working capacity is the volume of available
product under normal operating conditions. The net
working capacity is equal to the maximum capacity (3.2.6.2)
less the minimum operating volume remaining in the tank,
less the overfill protection level (or volume) requirement (see
Appendix L).
3.3 SPECIAL CONSIDERATIONS
3.3.1 Foundation
The selection of the tank site and the design and construction
of the foundation shall be given careful consideration, as
outlined in Appendix B, to ensure adequate tank support. The
adequacy of the foundation is the responsibility of the purchaser.
3.3.2 Corrosion Allowances
When necessary, the purchaser, after giving consideration
to the total effect of the liquid stored, the vapor above the liquid,
and the atmospheric environment, shall specify the corrosion
allowance to be provided for each shell course, for the
bottom, for the roof, for nozzles and manholes, and for structural
members.
3.3.3 Service Conditions
When the service conditions might include the presence of
hydrogen sulfide or other conditions that could promote
hydrogen-induced cracking, notably near the bottom of the
shell at the shell-to-bottom connections, care should be taken
to ensure that the materials of the tank and details of construction
are adequate to resist hydrogen-induced cracking. The
purchaser should consider limits on the sulfur content of the
base and weld metals as well as appropriate quality control
procedures in plate and tank fabrication. The hardness of the
welds, including the heat-affected zones, in contact with these
conditions should be considered. The weld metal and adjacent
heat-affected zone often contain a zone of hardness well
in excess of Rockwell C 22 and can be expected to be more
susceptible to cracking than unwelded metal is. Any hardness
criteria should be a matter of agreement between the purchaser
and the manufacturer and should be based on an evaluation
of the expected hydrogen sulfide concentration in the
product, the possibility of moisture being present on the
inside metal surface, and the strength and hardness characteristics
of the base metal and weld metal.
3.3.4 Weld Hardness
When specified by the purchaser, the hardness of the weld
metal for shell materials in Group IV, IVA, V, or VI shall be
evaluated by one or both of the following methods:
a. The welding-procedure qualification tests for all welding
shall include hardness tests of the weld metal and heataffected
zone of the test plate. The methods of testing and the
acceptance standards shall be agreed upon by the purchaser
and the manufacturer.
b. All welds deposited by an automatic process shall be hardness
tested on the product-side surface. Unless otherwise
05
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3-6 API S
TANDARD 650
specified, one test shall be conducted for each vertical weld,
and one test shall be conducted for each 30 m (100 ft) of circumferential
weld. The methods of testing and the acceptance
standards shall be agreed upon by the purchaser and the
manufacturer.
3.4 BOTTOM PLATES
3.4.1
All bottom plates shall have a minimum nominal
thickness of 6 mm (
1/4 in.) [49.8 kg/m2 (10.2 lbf/ft2) (see
2.2.1.2)], exclusive of any corrosion allowance specified by
the purchaser for the bottom plates. Unless otherwise agreed
to by the purchaser, all rectangular and sketch plates (bottom
plates on which the shell rests that have one end rectangular)
shall have a minimum nominal width of 1800 mm (72 in.).
3.4.2
Bottom plates of sufficient size shall be ordered so
that, when trimmed, at least a 50 mm (2 in.) width will project
outside the shell or to meet the requirements of 3.1.5.7e,
whichever is greater.
3.4.3
Bottom plates shall be welded in accordance with
3.1.5.4 or 3.1.5.5.
3.5 ANNULAR BOTTOM PLATES
3.5.1
When the bottom shell course is designed using the
allowable stress for materials in Group IV, IVA, V, or VI, buttwelded
annular bottom plates shall be used (see 3.1.5.6).
When the bottom shell course is of a material in Group IV,
IVA, V, or VI and both the maximum product stress (see
3.6.2.1) for the first shell course is less than or equal to 160
MPa (23,200 lbf/in.
2) or the maximum hydrostatic test stress
(see 3.6.2.2) for the first shell course is less than or equal to
172 MPa (24,900 lbf/in.
2), lap-welded bottom plates (see
3.1.5.4) may be used in lieu of butt-welded annular bottom
plates.
3.5.2
Annular bottom plates shall have a radial width that
provides at least 600 mm (24 in.) between the inside of the
shell and any lap-welded joint in the remainder of the bottom.
Annular bottom plate projection outside the shell shall meet
the requirements of 3.4.2. A greater radial width of annular
plate is required when calculated as follows:
In SI units:
where
t
b
= thickness of the annular plate (see 3.5.3), in mm,
H
= maximum design liquid level (see 3.6.3.2), in m,
G
= design specific gravity of the liquid to be stored.
In US Customary units:
where
t
b
= thickness of the annular plate (see 3.5.3), (in.),
H
= maximum design liquid level (see 3.6.3.2), (ft),
G
= design specific gravity of the liquid to be stored.
3.5.3
The thickness of the annular bottom plates shall not
be less than the thicknesses listed in Table 3-1 plus any specified
corrosion allowance.
3.5.4
The ring of annular plates shall have a circular outside
circumference but may have a regular polygonal shape
inside the tank shell, with the number of sides equal to the
number of annular plates. These pieces shall be welded in
accordance with 3.1.5.6 and 3.1.5.7, item b.
3.5.5
In lieu of annular plates, the entire bottom may be
butt-welded provided that the requirements for annular plate
thickness, welding, materials, and inspection are met for the
annular distance specified in 3.5.2.
3.6 SHELL DESIGN
3.6.1 General
3.6.1.1
The required shell thickness shall be the greater of
the design shell thickness, including any corrosion allowance,
or the hydrostatic test shell thickness, but the shell thickness
shall not be less than the following:
3.6.1.2
Unless otherwise agreed to by the purchaser, the
shell plates shall have a minimum nominal width of 1800 mm
(72 in.). Plates that are to be butt-welded shall be properly
squared.
Paragraph deleted.
Paragraph deleted.
●
03
05
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215
tb
(
HG)0.5
------------------
Nominal Tank Diameter
(See Note 1)
Nominal Plate Thickness
(See Note 2)
(m) (ft) (mm) (in.)
< 15 < 50 5
3/16
15 to < 36 50 to < 120 6
1/4
36 to 60 120 to 200 8
5/16
> 60 > 200 10
3/8
Notes:
1. Unless otherwise specified by the purchaser, the nominal tank
diameter shall be the centerline diameter of the bottom shell-course
plates.
2. Nominal plate thickness refers to the tank shell as constructed.
The thicknesses specified are based on erection requirements.
3. When specified by the purchaser, plate with a minimum nominal
thickness of 6 millimeters may be substituted for
1/4-inch plate.
390
tb
(
HG)0.5
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ELDED STEEL TANKS FOR OIL STORAGE 3-7
3.6.1.3
The calculated stress for each shell course shall not
be greater than the stress permitted for the particular material
used for the course. No shell course shall be thinner than the
course above it.
3.6.1.4
The tank shell shall be checked for stability against
buckling from the design wind speed in accordance with 3.9.7.
If required for stability, intermediate girders, increased shellplate
thicknesses, or both shall be used.
3.6.1.5
The manufacturer shall furnish to the purchaser a
drawing that lists the following for each course:
a. The required shell thicknesses for both the design condition
(including corrosion allowance) and the hydrostatic test
condition.
b. The nominal thickness used.
c. The material specification.
d. The allowable stresses.
3.6.1.6
Isolated radial loads on the tank shell, such as those
caused by heavy loads on platforms and elevated walkways
between tanks, shall be distributed by rolled structural sections,
plate ribs, or built-up members.
3.6.2 Allowable Stress
3.6.2.1
The maximum allowable product design stress, Sd,
shall be as shown in Table 3-2. The net plate thicknesses—the
actual thicknesses less any corrosion allowance—shall be
used in the calculation. The design stress basis,
Sd, shall be
either two-thirds the yield strength or two-fifths the tensile
strength, whichever is less.
3.6.2.2
The maximum allowable hydrostatic test stress, St,
shall be as shown in Table 3-2. The gross plate thicknesses,
including any corrosion allowance, shall be used in the calculation.
The hydrostatic test basis shall be either three-fourths
the yield strength or three-sevenths the tensile strength,
whichever is less.
3.6.2.3
Appendix A permits an alternative shell design
with a fixed allowable stress of 145 MPa (21,000 lbf/in.
2) and
a joint efficiency factor of 0.85 or 0.70. This design may only
be used for tanks with shell thicknesses less than or equal to
12.5 mm (
1/2 in.).
3.6.2.4
Structural design stresses shall conform to the
allowable working stresses given in 3.10.3.
3.6.3 Calculation of Thickness by the 1-Foot Method
3.6.3.1
The 1-foot method calculates the thicknesses
required at design points 0.3 m (1 ft) above the bottom of
each shell course. Appendix A permits only this design
method. This method shall not be used for tanks larger than
60 m (200 ft) in diameter.
3.6.3.2
The required minimum thickness of shell plates
shall be the greater of the values computed by the following
formulas:
In SI units:
where
t
d
= design shell thickness, in mm,
t
t
= hydrostatic test shell thickness, in mm,
D
= nominal tank diameter, in m (see 3.6.1.1, Note 1),
H
= design liquid level, in m,
= height from the bottom of the course under consideration
to the top of the shell including the top
angle, if any; to the bottom of any overflow that
limits the tank filling height; or to any other level
specified by the purchaser, restricted by an internal
floating roof, or controlled to allow for seismic
wave action,
G
= design specific gravity of the liquid to be stored,
as specified by the purchaser,
Table 3-1—Annular Bottom-Plate Thicknesses
SI Units
Nominal Plate
Thickness
a of First
Shell Course (mm)
Hydrostatic Test Stress
b in First Shell Course
(MPa)
≤
190 ≤ 210 ≤ 230 ≤ 250
t
≤ 19 6 6 7 9
19 <
t ≤ 25 6 7 10 11
25 <
t ≤ 32 6 9 12 14
32 <
t ≤ 38 8 11 14 17
38 <
t ≤ 45 9 13 16 19
US Customary
Nominal Plate
Thickness
a of First
Shell Course (in.)
Hydrostatic Test Stress
c in First Shell Course
(lbf/in
2)
≤
27,000 ≤ 30,000 ≤ 33,000 ≤ 36,000
t
≤ 0.75 1/4
1
/4
9
/32
11
/32
0.75 <
t ≤ 1.00 1/4
9
/32
3
/8
7
/16
1.00 <
t ≤ 1.25 1/4
11
/32
15
/32
9
/16
1.25 <
t ≤ 1.50 5/16
7
/16
9
/16
11
/16
1.50 <
t ≤ 1.75 11/32
1
/2
5
/8
3
/4
a
Nominal plate thickness refers to the tank shell as constructed.
b
Hydrostatic test stresses are calculated from [4.9D(H – 0.3)]/t
(see 3.6.3.2).
c
Hydrostatic test stresses are calculated from [2.6 D(H – 1]/t
(see 3.6.3.2).
Note: The thicknesses specified in the table, as well as the width
specified in 3.5.2, are based on the foundation providing uniform
support under the full width of the annular plate. Unless the foundation
is properly compacted, particularly at the inside of a concrete
ringwall, settlement will produce additional stresses in the
annular plate.
05
05
05
00
t
d
4.9
D(H – 0.3)G
S
d
= --------------------------------------- +
CA
t
t
4.9
D(H – 0.3)
S
t
= ----------------------------------
●
●
3-8 API S
TANDARD 650
CA
= corrosion allowance, in mm, as specified by the
purchaser (see 3.3.2),
S
d
= allowable stress for the design condition, in MPa
(see 3.6.2.1),
S
t
= allowable stress for the hydrostatic test condition,
in MPa (see 3.6.2.2).
●
Table 3-2—Permissible Plate Materials and Allowable Stresses
Plate
Specification Grade
Minimum
Yield Strength
MPa (psi)
Minimum
Tensile Strength
MPa (psi)
Product
Design Stress
Sd
MPa (psi)
Hydrostatic
Test Stress
St
MPa (psi)
ASTM Specifications
A 283M (A 283) C (C) 205 (30,000) 380 (55,000) 137 (20,000) 154 (22,500)
A 285M (A 285) C (C) 205 (30,000) 380 (55,000) 137 (20,000) 154 (22,500)
A 131M (A 131) A, B, CS
(A, B, CS)
235 (34,000) 400 (58,000) 157 (22,700) 171 (24,900)
A 36M (A 36) — 250 (36,000) 400 (58,000) 160 (23,200) 171 (24,900)
A 131M (A 131) EH 36 (EH 36) 360 (51,000) 490
a (71,000a) 196 (28,400) 210 (30,400)
A 573M (A 573) 400 (58) 220 (32,000) 400 (58,000) 147 (21,300) 165 (24,000)
A 573M (A 573) 450 (65) 240 (35,000) 450 (65,000) 160 (23,300) 180 (26,300)
A 573M (A 573) 485 (70) 290 (42,000) 485
a (70,000a) 193 (28,000) 208 (30,000)
A 516M (A 516) 380 (55) 205 (30,000) 380 (55,000) 137 (20,000) 154 (22,500)
A 516M (A 516) 415 (60) 220 (32,000) 415 (60,000) 147 (21,300) 165 (24,000)
A 516M (A 516) 450 (65) 240 (35,000) 450 (65,000) 160 (23,300) 180 (26,300)
A 516M (A 516) 485 (70) 260 (38,000) 485 (70,000) 173 (25,300) 195 (28,500)
A 662M (A 662) B (B) 275 (40,000) 450 (65,000) 180 (26,000) 193 (27,900)
A 662M (A 662) C (C) 295 (43,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 537M (A 537) 1 (1) 345 (50,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 537M (A 537) 2 (2) 415 (60,000) 550
a (80,000a) 220 (32,000) 236 (34,300)
A 633M (A 633) C, D (C, D) 345 (50,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 678M (A 678) A (A) 345 (50,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 678M (A 678) B (B) 415 (60,000) 550
a (80,000a) 220 (32,000) 236 (34,300)
A 737M (A 737) B (B) 345 (50,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 841M (A 841) Class 1 (Class 1) 345 (50,000) 485
a (70,000a) 194 (28,000) 208 (30,000)
A 841M (A 841) Class 2 (Class 2) 415 (60,000) 550
a (80,000a) 220 (32,000) 236 (34,300)
CSA Specifications
G40.21 260W (38W) 260 (38,000) 410 (60,000) 164 (24,000) 176 (25,700)
G40.21 300W (44W) 300 (44,000) 450 (65,000) 180 (26,000) 193 (27,900)
G40.21 350WT (50WT) 350 (50,000) 480
a (70,000a) 192 (28,000) 206 (30,000)
G40.21 350W (50W) 350 (50,000) 450 (65,000) 180 (26,000) 193 (27,900)
01
05
05
W
ELDED STEEL TANKS FOR OIL STORAGE 3-9
In US Customary units:
where
t
d
= design shell thickness (in.),
t
t
= hydrostatic test shell thickness (in.),
D
= nominal tank diameter, in ft (see 3.6.1.1, Note 1),
H
= design liquid level, (ft),
= height from the bottom of the course under consideration
to the top of the shell including the top
angle, if any; to the bottom of any overflow that
limits the tank filling height; or to any other level
specified by the purchaser, restricted by an internal
floating roof, or controlled to allow for seismic
wave action,
G
= design specific gravity of the liquid to be stored,
as specified by the purchaser,
CA
= corrosion allowance, (in.), as specified by the purchaser
(see 3.3.2),
S
d
= allowable stress for the design condition, (lbf/in.2)
(see 3.6.2.1),
S
t
= allowable stress for the hydrostatic test condition,
(lbf/in.
2) (see 3.6.2.2).
3.6.4 Calculation of Thickness by the Variable-
Design-Point Method
Note: This procedure normally provides a reduction in shell-course
thicknesses and total material weight, but more important is its
potential to permit construction of larger diameter tanks within the
maximum plate thickness limitation. For background information,
see L. P. Zick and R. V. McGrath, “Design of Large Diameter Cylindrical
Shells.”
15
3.6.4.1
Design by the variable-design-point method gives
shell thicknesses at design points that result in the calculated
stresses being relatively close to the actual circumferential
shell stresses. This method may only be used when the purchaser
has not specified that the 1-foot method be used and
when the following is true:
In SI units:
where
L
= (500 Dt)0.5, in mm,
D
= tank diameter, in m,
t = bottom-course shell thickness, excluding
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