Clasification Society Rulefinder 2020 - Version 9.33 - Fix
Common Structural Rules - Common Structural Rules for Bulk Carriers and Oil Tankers, January 2019 - Part 2 Ship Types - Chapter 2 Oil Tankers - Section 3 Hull Local Scantling - 1 Primary Supporting Members in Cargo Hold Region

1 Primary Supporting Members in Cargo Hold Region

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.
  • Q = fshr P Sshr
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.

shr : 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

shr : 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]

shr : 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:

bdg-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.

bdg-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.

bdg-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.

bdg-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].

bdg-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.

bdg-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 Sshr + c1 D bctr S ρL g
Qex : Design shear force due to green sea pressure, in kN.
  • Qex = 0.65 Pex – dt Sshr

Pin-dt : Design pressure in kN/m2, defined in [1.5.2].

Pex-dt : Design pressure in kN/m2, defined in [1.5.2].

bdg-dt : Effective span, in m, defined in [1.5.2].

shr : 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:
  • fshr = 0.5

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.

st : 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.

st-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:

shr : Effective shear span of the side transverse, in m.
  • shr = ℓst huhl where Qu and Ql are determined based on ℓst.
  • shr = ℓst -cthu where Qu and Ql are determined based on ℓst-ct.

st , 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:

bdg-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.

bdg-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.

bdg-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.

bdg-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 [cuvw (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 [clvw(Pu + Pl) – hl Pl]
  • cw S clvw(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.

vw : Length of the vertical web frame, in m, between the flange of the deck transverse and the inner bottom, see Figure 3.

vw-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:

shr : Effective shear span of the vertical web frame, in m.
  • shr = ℓvwhuhl where Qu and Ql are determined based on ℓvw.
  • shr = ℓvw-cthu where Qu and Ql are determined based on ℓvw-ct.

vw, 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:

bdg-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.

bdg-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.
  • Q = 0.5 P Shsshr

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].

shr : 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:

WctWct – perm

where:

Wct : Applied axial load, in kN.
  • Wct = P bct S

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.

bdg-vw : Effective bending span, in m, defined in [1.5.2].

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.


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