1.1 General
1.1.1 The following requirements relate to the determination of
scantlings of the primary supporting members within 0.4 L amidships and those
outside 0.4 L amidships provided that the geometry and fixation of primary
supporting member is similar with those amidships.
1.1.2 The section modulus and shear area criteria for primary
supporting members contained in this sub-section apply to structural configurations
shown in Pt 1, Ch 1, Sec 1, Figure 3 and are applicable to the following structural
elements:
- a) Floors and girders within the double bottom,
- b) Deck transverses,
- c) Side transverses within double side structure,
- d) Vertical web frames on longitudinal bulkheads with or without
cross ties,
- e) Horizontal stringers on transverse bulkheads, except those
fitted with buttresses or other intermediate supports,
- f) Cross ties in wing cargo and centre cargo tanks.
1.1.3 Floors, horizontal stringers, side transverses and vertical webs
adjacent to transverse bulkheads which get additional supports by horizontal stringers
or buttresses are excluded from the application of this section.
1.1.4 Webs of the primary supporting members are to be stiffened in
accordance with Pt 1, Ch 8, Sec 2, [4].
1.1.5 Webs of the primary supporting members are to have a depth of
not less than given by the requirements of [1.5.1], [1.7.1] and [1.8.1], as applicable.
1.1.6 In any case, primary supporting members that have open slots
for stiffeners are to have a depth not less than 2.5 times the depth of the slots if
slots are not closed.
1.1.7 Where it is impracticable to fit a primary supporting member
with the required web depth, then it is permissible to fit a member with reduced depth
provided that the fitted member has equivalent moment of inertia or deflection to the
required member. The required equivalent moment of inertia is to be based on an
equivalent section given by the effective width of plating at mid span with required
plate thickness, web of required depth and thickness and face plate of sufficient width
and thickness to satisfy the required mild steel section modulus.
The equivalent moment of inertia may be also demonstrated by an equivalent
member having the same deflection as the required member.
All other rule requirements, such as minimum thicknesses, slenderness ratio,
section modulus and shear area, are to be satisfied for the member of reduced depth.
1.2 Design load sets
1.2.1 The design load sets for the evaluation of primary supporting
members are given in Table 1.
Table 1 : Design load sets for
primary supporting members
Item
|
Design load set (1) (5) (6)
|
Load component
|
Draught
|
Design load
|
Loading condition
|
Double bottom floors and girders
(3)
|
SEA-1
|
Pex
|
0.9Tsc
(2)
|
S+D
|
Sea pressure only
|
SEA-2
|
Pex
|
TSC
|
S
|
OT-4
|
Pin – Pex
|
0.6Tsc
|
S+D
|
Net pressure difference between cargo
pressure and sea pressure
|
OT-5
|
Pin – Pex
|
(4)
|
S
|
Side transverses (3)
|
SEA-1
|
Pex
|
0.9Tsc
|
S+D
|
Sea pressure only
|
SEA-2
|
Pex
|
Tsc
|
S
|
OT-1
|
Pin
|
TSC
|
S+D
|
Cargo pressure only
|
OT-2
|
Pin
|
0.6Tsc
|
S+D
|
OT-3
|
Pin
|
-
|
S
|
Deck transverses
|
SEA-1
|
Pex
|
Tsc
|
S+D
|
Green sea pressure only or other loads on deck
|
OT-1
|
Pin
|
TSC
|
S+D
|
Cargo pressure only
|
OT-2
|
Pin
|
0.6Tsc
|
S+D
|
OT-3
|
Pin
|
-
|
S
|
Vertical web frames on longitudinal
bulkheads
|
OT-1
|
Pin
|
TSC
|
S+D
|
Pressure from one side only. Full cargo tank
with adjacent cargo tank empty
|
OT-2
|
Pin
|
0.6Tsc
|
S+D
|
OT-3
|
Pin
|
-
|
S
|
Horizontal stringers on transverse
bulkhead
|
OT-1
|
Pin
|
TSC
|
S+D
|
Pressure from one side only. Full cargo
tank with adjacent forward or aft cargo tank empty.
|
OT-2
|
Pin
|
0.6Tsc
|
S+D
|
OT-3
|
Pin
|
-
|
S
|
Cross ties in centre tanks
|
OT-1
|
|
TSC
|
S+D
|
Full wing cargo tanks, centre tank
empty.
|
OT-2
|
|
0.6Tsc
|
S+D
|
OT-3
|
Pin
|
-
|
S
|
Cross ties in wing tanks
|
OT-6
|
|
Tsc
|
S+D
|
Full centre tank, wing cargo tanks
empty.
|
OT-7
|
|
0.6Tsc
|
S+D
|
OT-8
|
|
Tsc
|
S
|
where:
Pin-pt : Design pressure from port side
wing cargo tank, in kN/m2.
Pin-stb : Design pressure from
starboard side wing cargo tank, in kN/m2.
(1) The static and dynamic load components are to
be determined in accordance with Pt 1, Ch 4, Sec 7, Table 1.
(2) If the loading condition where the
combination of an empty cargo tank and a mean ship’s draught greater
than 0.9 Tsc is included in ship’s loading manual,
the maximum corresponding draught is to be considered.
(3) Draughts specified for bottom floors, girders
and side transverses are based on operational limits specified in Pt
1, Ch 4, Sec 8, [2] and Pt 1, Ch 4, Sec 8, [3]. Where the optional
loading conditions exceed the minimum Rule required loading
conditions, the draughts will be subject to special
consideration.
(4) For tankers with two oil-tight longitudinal
bulkheads, the draught is to be taken as 0.25 Tsc.
For tankers with a centreline bulkhead, the draught is to be taken
as 0.33 Tsc.
(5) When the ship’s configuration cannot be
described by the structural members or structural configurations
identified above, then the applicable Design Load Sets to determine
the scantling requirements of primary supporting member are to be
selected so as to specify all applicable cases from the
following:
- A full tank on one side of the member with the
tank or space on the other side empty.
- A full tank on one side of the member with the
external pressure minimised.
- External pressure maximised with the adjacent
tank or space empty.
The boundary is to be evaluated for loading from both
sides. Design Load Sets are to be selected based on the tank or
space contents and are to maximise the net pressure on the
structural boundary, the draught to use is to be taken in accordance
with the Design Load Set and this table. Design Load Sets covering
the S and S+D design load combinations are to be selected.
(6) For a void or dry space, the pressure
component from the void side is to be ignored.
|
1.3 Floors in double bottom
1.3.1 Structural arrangement
Plate floors are to be arranged in way of transverse bulkheads and bulkhead
stools.
1.3.2 Net shear area
The net shear area, Ashr-n50 in cm2, of the
floors at any position in the floor is not to be less than:
where:
Q : Design shear force, in kN.
fshr : Shear force distribution factor:
but not to be taken as less than 0.2.
fshr-i : Shear force distribution factor at the end of the
span, ℓshr, as given in Table 2.
ℓshr : Effective shear span, of the double bottom floor, in
m, as shown in Figure 2. In way of bracket ends, the effective shear span is measured to
the toes of the effective end bracket, as defined in Pt 1, Ch 3, Sec 7, [1.1.7]. Where
the floor ends on a girder at a hopper or stool structure, the effective shear span is
measured to a point that is one-half of the distance from the girder to the adjacent
bottom and inner-bottom longitudinal, as shown in Figure 2.
yi : Distance from the considered cross section of the floor to the
nearest end of the effective shear span, ℓshr in m.
P : Design pressure given in Table 1 for the design load set being considered,
calculated at mid point of effective shear span, ℓshr of a floor
located midway between transverse bulkheads or transverse bulkhead and wash bulkhead,
where fitted, in kN/m2.
Table 2 : Shear force distribution
factors of floors
Structural configuration
|
Centre tank (fshr3 in
Figure 1)
|
Wing tank
|
At inboard end (fshr2 in Figure
1)
|
At hopper knuckle end (fshr1 in Figure
1)
|
Ships with centreline longitudinal bulkhead
|
-
|
0.40
|
0.60
|
Ships with two longitudinal bulkheads
|
0.5
|
0.50
|
0.65
|
Figure 1 : Shear force distribution factors of floors
Figure 2 : Effective shear span of floors
1.4 Girders in double bottom
1.4.1 Structural arrangement
Continuous double bottom girders are to be arranged at the centreline or duct
keel, at the hopper side and in way of longitudinal bulkheads and bulkhead stools.
1.4.2 Net shear area of centre girders
For double bottom centre girders where no longitudinal bulkhead is fitted
above, the net shear area, Ashr-n50 in cm2, of the double
bottom centre girder in way of the first bay from each transverse bulkhead and wash
bulkhead, where fitted, is not to be less than:

where:
Q : Design shear force, in kN, taken as:
- Q = 0.21 n1
n2
P

ℓshr : Effective shear span as defined in [1.3.2].
P : Design pressure, in kN/m2, as defined in [1.3.2].
n1 : Coefficient taken as:
n2 : Coefficient taken as:
S : Double bottom floor spacing, in m, as defined in Pt 1 Ch 3 Sec 7 [1.2.2]
1.4.3 Net shear area of side girders
For double bottom side girders where no longitudinal bulkhead is fitted
above, the net shear area, Ashr-n50 in cm2, of the double
bottom side girder in way of the first bay from each transverse bulkhead and wash
bulkhead, where fitted, is not to be less than:

where:
Q : Design shear force, in kN.
n3 : Coefficient taken as:
n4 : Coefficient taken as:
S: Double bottom floor spacing, in m, as defined in Pt 1 Ch 3 Sec 7 [1.2.2]
ℓshr : Effective shear span as defined in [1.3.2].
P : Design pressure, in kN/m2, as defined in [1.3.2].
1.5 Deck transverses
1.5.1 Web depth
The web depth of under deck transverses is not to be less than:
- 0.20 ℓbdg-dt for deck transverses in the wing cargo
tanks of ships with two longitudinal bulkheads.
- 0.13 ℓbdg-dt for deck transverses in the centre cargo
tanks of ships with two longitudinal bulkheads. The web depth of deck transverses in
the centre cargo tank is not to be less than 90% of that of the deck transverses in
the wing cargo tank.
- 0.10 ℓbdg-dt for the deck transverses of ships with a
centreline longitudinal bulkhead.
- The web height required in [1.1.6].
The web depth of above deck transverses is not to be less than:
- 0.10 ℓbdg-dt
- The web height required in [1.1.6].
where:
ℓbdg-dt : Effective bending span, in m, as defined in
[1.5.2].
1.5.2 Net section modulus of deck transverses fitted below the upper
deck
The net section modulus of deck transverses fitted below the upper deck, in
cm3, is not to be less than Zin-n50 and
Zex-n50 as given by the following formulae.
The net section modulus of the deck transverses fitted below the upper deck
in the wing cargo tanks is also not to be less than required for the deck transverses
fitted below the upper deck in the centre tanks.


where:
Min : Design bending moment due to cargo pressure, in kNm,
taken as:
- For deck transverses in wing cargo tanks of ships with two longitudinal
bulkheads, and for deck transverses in cargo tanks of ships with a centreline
longitudinal bulkhead:
- Min = 0.042ϕt
Pin – dt S
+ Mst but is not to be taken as less than
M0.
- For deck transverses in centre cargo tank of ships with two longitudinal
bulkheads:
- Min = 0.042ϕt
Pin – dt S
+ Mvw but is not to be taken as less than
M0.
Mst : Bending moment transferred from the side transverse,
in kNm:
- Mst = cst βst
Pin – st S

- where a cross tie is fitted in a wing cargo tank and
ℓbdg-st-ct is greater than 0.7
ℓbdg-st, then ℓbdg-st in the above
formula may be taken as ℓbdg-st-ct.
Mvw : Bending moment transferred from the vertical web
frame on the longitudinal bulkhead, in kNm:
- Mvw = cvw
βvw
Pin – vw S

- where ℓbdg-vw-ct is greater than 0.7
ℓbdg-vw, then ℓbdg-vw in the above
formula may be taken as ℓbdg-vw-ct. For vertically corrugated
bulkheads, Mvw is to be taken equal to bending moment in upper
end of corrugation over the spacing between deck transverses.
M0 : Minimum bending moment, in kNm.
- M0 = 0.083 Pin – dt S

Mex : Design bending moment due to green sea pressure, in
kNm.
- Mex = 0.067 Pex – dt S

Pin-dt : Design cargo pressure given in Table 1 for the
design load set being considered, calculated at midpoint of effective bending span,
ℓbdg-dt of the deck transverse located at mid tank, in
kN/m2.
Pin-st : Corresponding design cargo pressure in wing cargo
tank given in Table 1 for the design load set being considered, calculated at the
mid-point of effective bending span, ℓbdg-st of the side transverse
located at mid-tank, in kN/m2.
Pin-vw : Corresponding design cargo pressure in the centre
cargo tank of ships with two longitudinal bulkheads given in Table 1 for the design load
set being considered, calculated at mid-point of effective bending span,
ℓbdg-vw of the vertical web frame on the longitudinal bulkhead
located at midtank, in kN/m2.
Pex-dt : Design green sea pressure given in Table 1 for
the design load set being considered, calculated at mid-point of effective bending span,
ℓbdg-dt of the deck transverse located at mid tank, in
kN/m2.
φt : Coefficient taken as:
but not taken less than 0.6.
ytoe : Distance from the end of effective bending span,
ℓbdg-dt to the toe of the end bracket of the deck transverse,
in m.
βst : Coefficient taken as:
but not taken less than 0.10 or greater than 0.65.
βvw : Coefficient taken as:
but not taken less than 0.10 or greater than 0.50.
ℓbdg-dt : Effective bending span of the deck transverse, in
m, see Pt 1, Ch 3, Sec 7, [1.1.6] and Figure 3, but is not to be taken as less than 60%
of the breadth of the tank at the location being considered.
ℓbdg-st : Effective bending span of the side transverse,
in m, between the deck transverse and the bilge hopper, see Pt 1, Ch 3, Sec 7, [1.1.6]
and Figure 3.
ℓbdg-st-ct : Effective bending span of the side
transverse, in m, between the deck transverse and the mid depth of the cross tie, where
fitted in wing cargo tank, see Pt 1, Ch 3, Sec 7, [1.1.6].
ℓbdg-vw : Effective bending span of the vertical web frame
on the longitudinal bulkhead, in m, between the deck transverse and the bottom
structure, see Pt 1, Ch 3, Sec 7, [1.1.6] and Figure 3.
ℓbdg-vw-ct : Effective bending span of the vertical web
frame on longitudinal bulkhead, in m, between the deck transverse and the mid depth of
the cross tie, see Pt 1, Ch 3, Sec 7, [1.1.6].
Idt-n50 : Net moment of inertia of the deck transverse at
mid-span with an effective breadth of attached plating specified in Pt 1, Ch 3, Sec 7,
[1.3.2], in cm4.
Ist-n50 : Net moment of inertia of the side transverse at
mid-span with an effective breadth of attached plating specified in Pt 1, Ch 3, Sec 7,
[1.3.2], in cm4.
Ivw-n50 : Net moment of inertia of the longitudinal bulkhead vertical
web frame at mid-span with an effective breadth of attached plating specified in Pt 1,
Ch 3, Sec 7, [1.3.2], in cm4.
cst : Coefficient given in Table 3.
cvw : Coefficient given in Table 3.
Table 3 : Values of cst
and cvw for deck transverses
Structural
configuration
|
cst
|
cvw
|
Ships with
centreline longitudinal bulkhead
|
0.056
|
-
|
Ships with two longitudinal
bulkheads
|
Cross tie in centre cargo tank
|
Mvw based on
ℓbdg-vw-ct
|
-
|
0.044
|
Mst based on ℓbdg-st
or Mvw based on ℓbdg-vw
|
0.044
|
0.016
|
Cross ties in wing cargo tanks
|
Mst based on
ℓbdg-st-ct or Mvw based on
ℓbdg-vw-ct
|
0.044
|
0.044
|
Mst based on ℓbdg-st
or Mvw based on ℓbdg-vw
|
0.041
|
0.015
|
1.5.3 Net shear area of deck transverses fitted below the upper
deck
The net shear area of deck transverses fitted below the upper deck, in
cm2, is not to be less than Ashr-in-n50 and
Ashr-ex-n50 as given by:
where:
Qin : Design shear force due to cargo pressure, in kN.
- Qin = 0.65 Pin – dt
S ℓshr + c1
D
bctr
S ρL
g
Qex : Design shear force due to green sea pressure, in
kN.
- Qex = 0.65 Pex – dt S
ℓshr
Pin-dt : Design pressure in kN/m2, defined in
[1.5.2].
Pex-dt : Design pressure in kN/m2, defined in
[1.5.2].
ℓbdg-dt : Effective span, in m, defined in [1.5.2].
ℓshr : Effective shear span, of the deck transverse, in
m, see Pt 1, Ch 3, Sec 7, [1.1.7].
c1 : Coefficient taken as:
- c1 = 0.04 in way of wing cargo tanks of ships with
two longitudinal bulkheads.
- c1 = 0.00 in way of centre tank of ships with two
longitudinal bulkheads.
- c1 = 0.00 for ships with a centreline longitudinal
bulkhead.
bctr : Breadth of the centre tank, in m.
Figure 3 : Definition of spans of deck, side transverses, vertical web
frames on longitudinal bulkheads and horizontal stringers on transverse bulkheads
1.5.4 Deck transverses fitted above the upper deck
When deck transverses are fitted above the upper deck, the net section
modulus and shear area of deck transverses are not to be less than
Zn50 and Ashr-n50, in cm3 and
cm2 respectively, as given by the following formulae. The required
section modulus and shear area are to be maintained over the full length of span.


where:
P : Design pressure given in Table 1 for the design load set being
considered, calculated at midpoint of effective bending span, ℓbdg of
the deck transverse located at mid tank, in kN/m2.
fbdg : Coefficient taken as:
- fbdg = 12 for design load set OT-1, OT-2 and OT-3
as defined in Table 1.
- fbdg = 15 for design load set SEA-1 as defined
in Table 1.
fshr : Coefficient taken as:
lbdg : Effective bending span of the deck transverse
fitted above upper deck, in m, measured from inner hull welded to deck to longitudinal
bulkhead, or upper stool plating where upper stool is fitted
lshr : Effective shear span of the deck transverse fitted
above upper deck, in m, measured from inner hull welded to deck to longitudinal
bulkhead, or upper stool plating where upper stool is fitted
As an alternative, the required section modulus and shear area may be
obtained by finite element method in accordance with Pt 1, Ch 7 and with in
consideration of loading patterns A1, A2 or B1, B2 as defined in Pt 1, Ch 4, Sec 8,
[3.2.9] with draught equal to Tsc and cargo density of 1.025
t/m3.
1.5.5 Deck transverse adjacent to transverse bulkhead
The scantling of deck transverse adjacent to the transverse bulkhead is to
comply with the requirements of [1.5.2] to [1.5.4] for design green sea pressure
only.
1.6 Side transverses
1.6.1 Net shear area
The net shear area, Ashr-n50, in cm2, of side
transverses is not to be less than:
where:
Q : Design shear force as follows, in kN:
- Q = Qu for upper part of the side
transverse.
- Q = Ql for lower part of the side
transverse.
Qu : Shear force, in kN, taken as:

- where a cross tie is fitted in a wing cargo tank and
ℓst-ct is greater than 0.7 ℓst, then
ℓst in the above formula is taken as
ℓst-ct.
Ql : Shear force, in kN, taken as the greater of the
following:


- 1.2Qu
- where a cross tie is fitted in a wing cargo tank and
ℓst-ct is greater than 0.7 ℓst, then
ℓst in the above formula is taken as
ℓst-ct.
Pu : Design pressure given in Table 1 for the design load set being
considered, in kN/m2, calculated at mid length of tank and at mid height of
hu.
Pl : Design pressure given in Table 1 for the design load
set being considered, calculated at mid height hl located at mid
length of tank, in kN/m2.
ℓst : Length of the side transverse, in m, taken as
follows:
- Where deck transverses are fitted below deck, ℓst is
the length between the flange of the deck transverse and the inner bottom, see
Figure 3.
- Where deck transverses are fitted above deck, ℓst is
the length between the elevation of the deck at side and the inner bottom.
ℓst-ct : Length of the side transverse, in m, taken as
follows:
- Where deck transverses are fitted below deck, ℓst-ct
is the length between the flange of the deck transverse and mid depth of cross tie,
where fitted in wing cargo tank.
- Where deck transverses are fitted above deck, ℓst-ct
is the length between the elevation of the deck at side and mid depth of the cross
tie, where fitted in wing cargo tank.
hu : Effective length of upper bracket of the side transverse, in m,
taken as follows:
- Where deck transverses are fitted below deck, hu is as
shown in Figure 3.
- Where deck transverses are fitted above deck:
- When an inner hull longitudinal bulkhead is arranged with a top
wing structure as follows, hu is taken as the distance between the deck at
side and the lower end of slope plate of the top wing structure:
- The breadth at top of the wing structure is greater than
1.5 times the breadth of the double side and.
- The angle along a line between the point at base of the
slope plate at its intersection with the inner hull longitudinal
bulkhead and the point at the intersection of top wing structure and
deck is 30 deg or more to vertical.
- In the other cases: hu is taken as 0.
hl : Height of bilge hopper, in m, as shown in Figure 3.
cu : Coefficient defined in Table 4.
cl : Coefficient defined in Table 4.
Table 4 : Values of
cu and cl for side transverses
Structural configuration
|
Cu
|
Cl
|
Number of side stringers
|
Less than three
|
Equal to or greater than three
|
Less than three
|
Equal to or greater than three
|
Ships with a centreline longitudinal
bulkhead
|
0.12
|
0.09
|
0.29
|
0.21
|
Ships with two longitudinal bulkheads
|
Cross tie in centre cargo tank
|
Cross ties in wing cargo tanks
|
Qu or Ql based on
ℓst-ct
|
Qu or Ql based on
ℓst
|
0.08
|
0.20
|
1.6.2 Shear area over the length of the side transverse
The shear area over the length of the side transverse is to comply with the following.
When materials of different yield stress are employed, appropriate adjustments are to be
made to account for differences in material yield stress.
- a) The required shear area for the upper part is to be maintained over the
upper 0.2 ℓshr.
- b) The required shear area for the lower part is to be maintained over the
lower 0.2 ℓshr.
- c) Where Qu and Ql are determined based on
ℓst-ct, the required shear area for the lower part is
also to be maintained below the cross tie.
- d) For ships without cross ties in the wing cargo tanks, the required shear
area between the upper and lower parts is to be reduced linearly towards 50% of
the required shear area for the lower part at midspan.
- e) For ships with cross ties in the wing cargo tanks, the required shear area
along the span is to be tapered linearly between the upper and lower parts.
where:
ℓ
shr : Effective shear span of the side transverse, in m.
- ℓshr = ℓst – hu –
hl where Qu and Ql
are determined based on ℓst.
- ℓshr = ℓst -ct– hu where
Qu and Ql are determined based on
ℓst-ct.
ℓst , ℓst -ct,hu,
hl, Qu, Ql: Parameters
defined in [1.6.1].
1.7 Vertical web frames on longitudinal bulkhead
1.7.1 Web depth
The web depth of the vertical web frame on the longitudinal bulkhead is not to be less
than:
- 0.14 ℓbdg-vw for ships with a centreline longitudinal
bulkhead.
- 0.09 ℓbdg-vw for ships with two longitudinal bulkheads.
- The web height required in [1.1.6].
where:
ℓbdg-vw : Effective bending span, in m, defined in [1.7.2].
1.7.2 Net section modulus
The net section modulus, Zn50 in cm3, of the vertical web
frame is not to be less than:

where:
M : Design bending moment, in kNm, as follows:
- M = cu P S
for upper part of the web frame.
-
M = cl P S
for lower part of the web frame.
- where a cross tie is fitted and ℓbdg-vw-ct is greater than
0.7 ℓbdg-vw, then ℓbdg-vw in the above
formula is to be taken as ℓbdg-vw-ct.
P : Design pressure given in Table 1 for the design load set being considered,
calculated at mid-point of the effective bending span, ℓbdg-vw of the
vertical web frame located at mid tank, in kN/m2.
ℓbdg-vw : Effective bending span of the vertical web frame on the
longitudinal bulkhead, between the deck transverse and the bottom structure, in m, see
Figure 3.
ℓbdg-vw-ct : Effective bending span of the vertical web frame on
longitudinal bulkhead, between the deck transverse and mid-depth of the cross tie on
ships with two longitudinal bulkheads, in m.
cu : Coefficient defined in Table 5.
cl : Coefficient defined in Table 5.
Table 5 : Values of
cu and cl for vertical web frame on
longitudinal bulkheads
Structural configuration
|
cu
|
cl
|
Ships with a centreline longitudinal
bulkhead
|
0.057
|
0.071
|
Ships with two longitudinal bulkheads
|
Cross tie in centre cargo tank
|
M based on ℓbdg-vw-ct
|
0.057
|
0.071
|
M based on ℓbdg-vw
|
0.012
|
0.028
|
Cross ties in wing cargo tanks
|
M based on ℓbdg-vw-ct
|
0.057
|
0.071
|
M based on ℓbdg-vw
|
0.016
|
0.032
|
1.7.3 Section modulus over the length of the vertical web frame
The section modulus over the length of the vertical web frame on the longitudinal
bulkhead is to comply with the following. When materials of different yield stress are
employed, appropriate adjustments are to be made to account for differences in material
yield stress.
- a) The required section modulus for the upper part is to be maintained over the
upper 0.2 ℓbdg-vw or 0.2 ℓbdg-vw-ct as
applicable.
- b) The required section modulus for the lower part is to be maintained over the
lower 0.2 ℓbdg-vw or 0.2 ℓbdg-vw-ct as
applicable.
- c) Where the required section modulus is determined based on
ℓbdg-vw-ct, the required section modulus for the lower
part is also to be maintained below the cross tie.
- d) The required section modulus between the upper and lower parts is to be
reduced linearly to 70% of the required section modulus for the lower part at
mid-span.
ℓbdg-vw, ℓbdg-vw-ct : Effective bending
span, in m, defined in [1.7.2].
1.7.4 Net shear area
The net shear area, Ashr-n50 in cm2, of the vertical web
frame is not to be less than:

where:
Q : Design shear force as follows, in kN:
- Q = Qu for upper part of the web
frame.
-
Q = Ql for lower part of the web frame.
Qu : Shear force, in kN, taken as:
- Qu= S [cu ℓvw
(Pu + Pl) – hu
Pu]
- where a cross tie is fitted in a centre or wing cargo tank and
ℓvw-ct is greater than 0.7 ℓvw, then
ℓvw in the above formula is to be taken as
ℓvw-ct.
Ql : Shear force, in kN, taken as the greater of the following:
- S [cl ℓvw(Pu +
Pl) – hl Pl]
- cw
S
cl ℓvw(Pu +
Pl)
- 1.2 Qu
where a cross tie is fitted in a centre or wing cargo tank and ℓvw-ct
is greater than 0.7 ℓvw, then ℓvw in the above
formula is to be taken as ℓvw-ct.
Pu : Design pressure given in Table 1 for the design load
set being considered, calculated at mid-height of upper bracket of the vertical web
frame, hu located at mid tank, in kN/m2.
Pl : Design pressure given in Table 1 for the design load
set being considered, calculated at mid-height of lower bracket of the vertical web
frame, hl located at mid tank, in kN/m2.
ℓvw : Length of the vertical web frame, in m, between the flange of the
deck transverse and the inner bottom, see Figure 3.
ℓvw-ct : Length of the vertical web frame, in m, between the flange of
the deck transverse and mid-depth of the cross tie, where fitted.
hu : Effective length of upper bracket of the vertical web frame, in m,
as shown in Figure 3.
hl : Effective length of lower bracket of the vertical web frame, in m,
as shown in Figure 3.
cu : Coefficient defined in Table 6.
cl : Coefficient defined in Table 6.
cw : Coefficient taken as:
- cw = 0.57 for ships with a centreline longitudinal bulkhead,
- cw = 0.50 for ships with two longitudinal bulkheads.
Table 6 : Values of
cu and cl for vertical web frame on
longitudinal bulkhead
Structural configuration
|
cu
|
cl
|
Ships with a centreline longitudinal
bulkhead
|
0.17
|
0.28
|
Ships with two longitudinal bulkheads
|
Qu or Ql based on
ℓvw-ct
|
Qu or Ql based on
ℓvw
|
0.075
|
0.18
|
1.7.5 Shear area over the length of the vertical web frame
The shear area over the length of the vertical web frame on the longitudinal bulkhead is
to comply with the following. When materials of different yield stress are employed,
appropriate adjustments are to be made to account for differences in material yield
stress.
- a) The required shear area for the upper part is to be maintained over the
upper 0.2 ℓshr.
- b) The required shear area for the lower part is to be maintained over the
lower 0.2 ℓshr.
- c) Where Qu and Ql are determined based on
ℓvw-ct, the required shear area for the lower part is
also to be maintained below the cross tie.
- d) For ships without cross ties in the wing or centre cargo tanks, the required
shear area between the upper and lower parts is to be reduced linearly towards
50% of the required shear area for the lower part at mid-span.
- e) For ships with cross ties in the wing or centre cargo tanks, the required
shear area along the span is to be tapered linearly between the upper and lower
parts.
where:
ℓ
shr : Effective shear span of the vertical web frame, in m.
- ℓshr = ℓvw –
hu – hl where Qu and
Ql are determined based on
ℓvw.
- ℓshr = ℓvw-ct –
hu where Qu
and Ql are determined based on
ℓvw-ct.
ℓvw, ℓvw-ct, hu,
hl, Qu, Ql : Parameters
defined in [1.7.4].
1.8 Horizontal stringers on transverse bulkheads
1.8.1 Web depth
The web depth of horizontal stringers on transverse bulkhead is not to be less than:
- 0.28 ℓbdg-hs for horizontal stringers in wing cargo tanks of ships
with two longitudinal bulkheads.
- 0.20 ℓbdg-hs for horizontal stringers in centre tanks of ships
with two longitudinal bulkheads, but the web depth of horizontal stringers in centre
tank is not to be less than required depth for a horizontal stringer in wing cargo
tanks.
- 0.20 ℓbdg-hs for horizontal stringers of ships with a
centreline longitudinal bulkhead.
- The web height required in [1.1.6].
where:
ℓbdg-hs : Effective bending span, in m, defined in [1.8.2].
1.8.2 Net section modulus
The net section modulus, Zn50 in cm3, of the
horizontal stringer over the end 0.2 ℓbdg-hs is not to be less
than:

where:
M : Design bending moment, in kNm.
P : Design pressure given in Table 1 for the design load set being considered,
calculated at mid-point of effective bending span, ℓbdg-hs and at
mid-point of the spacing, S of the horizontal stringer, in kN/m2.
ℓbdg-hs : Effective bending span of the horizontal stringer, in m, but
is not to be taken as less than 50% of the breadth of the tank at the location being
considered, see Figure 3.
c : Coefficient taken as:
- c = 0.073 for horizontal stringers in cargo tanks of ships with a centreline
bulkhead.
- c = 0.083 for horizontal stringers in wing cargo tanks of ships with two
longitudinal bulkheads.
- c = 0.063 for horizontal stringers in the centre tank of ships with two
longitudinal bulkheads.
1.8.3 Section modulus over the length of horizontal stringers
The required section modulus at mid effective bending span is to be taken as 70% of that
required at the ends, intermediate values are to be obtained by linear interpolation.
When materials of different yield stress are employed, appropriate adjustments are to be
made to account for differences in material yield stress.
1.8.4 Net shear area
The net shear area, Ashr-n50 in cm2, of the horizontal
stringer over the end 0.2 ℓshr is not to be less than:

Q : Design shear force, in kN.
P : Design pressure given in Table 1 for the design load set being considered,
calculated at mid-point of effective bending span, ℓbdg-hs and at
mid-point of the spacing, S of the horizontal stringer, in kN/m2.
Shs : Spacing, in m, defined in [1.8.2].
ℓshr : Effective shear span of the horizontal stringer, in m.
1.8.5 Shear area at mid effective shear span
The required shear area at mid effective shear span is to be taken as 50% of that
required in the ends, intermediate values are to be obtained by linear interpolation.
When materials of different yield stress are employed, appropriate adjustments are to be
made to account for differences in material yield stress.
1.9 Cross ties
1.9.1 Maximum applied design axial load
The maximum applied design axial load on cross ties, Wct is to be less
than or equal to the permissible load, Wct-perm as given by:
Wct ≤ Wct – perm
where:
Wct : Applied axial load, in kN.
Wct-perm : Permissible load, in kN.
- Wct – perm = 0.12 Act – n50 ηall
σcr
P : Maximum design pressure for all the applicable design load sets being
considered given in Table 1, calculated at centre of the area supported by the cross tie
located at mid tank, in kN/m2.
bct : Span, in m, taken as:
- Cross tie fitted in centre cargo tank: bct = 0.5
ℓbdg-vw
- Cross ties fitted in wing cargo tanks:
- bct = 0.5 ℓbdg-vw for design cargo
pressure from the centre cargo tank.
- bct = 0.5 ℓbdg-st for design sea
pressure.
ℓbdg-vw : Effective bending span, in m, defined in [1.5.2].
ℓ bdg-st : Effective bending span, in m, defined in [1.5.2].
ηall : Allowable buckling utilisation factor as defined in Pt 1, Ch 8,
Sec 1, [3.3].
σcr : Critical buckling stress in compression of the cross tie, in
N/mm2, as calculated using the net sectional properties in accordance
with Pt 1, Ch 8, Sec 5, [3.1.1].
Act-n50 : Net cross sectional area of the cross tie, in
cm2.
1.9.2 Welded connections
Special attention is to be paid to the adequacy of the welded connections for the
transmission of the forces, and also to the stiffening arrangements, in order to provide
effective means for transmission of the compressive forces into the webs.
Particular attention is to be paid to the welding at the toes of all end brackets of the
cross ties.
1.9.3 Horizontal stiffeners
Horizontal stiffeners are to be located in line with, and attached to, the longitudinals
at the ends of the cross ties.