Section
1 Materials of construction
1.1 General
1.1.1 These Rules
relate, in general, to the construction of steel ships, although consideration
will be given to the use of other materials, when permitted by the
Regulations of National and/or International Authorities for the type
of ship.
1.1.3 Where steel castings or forgings are used for sternframes, rudder frames,
rudder stocks, propeller shaft brackets and other major structural items, they are to
comply with LR’s Rules for the Manufacture, Testing and Certification of Materials, July 2022, Pt 3, Ch 4 Longitudinal Strength or Pt 3, Ch 5 Fore End and Aft End Structure, as appropriate.
1.1.4 Where aluminium alloy is used for superstructures, deckhouses, hatch covers
or other structural components, equivalent scantlings are to be derived in accordance
with Pt 3, Ch 2, 1.4 Aluminium.
1.2 Grades of steel
1.2.1 The ships covered by these Rules are generally to be constructed of Grade
‘A’ or 'AH' steel. In highly stressed areas, however, grades of steel with higher levels
of notch toughness (Grades ‘B’, ‘D’, 'DH', ‘E’ or 'EH') may be required, dependent on
the thickness of the material and the stress pattern associated with its location.
1.3 Steel
1.3.1 Steel having a specified minimum yield stress of 235 N/mm2 is
regarded as mild steel. Steel having a higher specified minimum yield stress is
regarded as higher tensile steel.
1.3.2 For the determination of the hull girder section modulus, where higher
tensile steel is used, a higher tensile steel factor, kL, is given
in Table 2.1.1 Values of
KL.
Table 2.1.1 Values of
KL
Specified
minimum yield stress in N/mm2
|
kL
|
235
|
1,0
|
265
|
0,92
|
315
|
0,78
|
355
|
0,72
|
Note 1. Intermediate
values by linear interpolation.
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1.3.3 The local scantling requirements of higher tensile steel plating, longitudinals,
stiffeners and girders may be based on a k factor determined as
follows:
or 0,66 whichever is the greater.
where
σo
|
= |
specific minimum yield stress in N/mm2
|
1.4 Aluminium
1.4.1 The use of aluminium alloy is permitted for superstructures, deckhouses,
hatch covers, helicopter platforms or other local components on board ships.
1.4.2 Except where otherwise stated in Pt 3, Ch 8, 3 Aluminium erections, equivalent
scantlings are to be derived as follows:
- Plating thickness,

- Section modulus of stiffeners

- where
c
|
= |
0,95 for high corrosion resistant alloy |
= |
1,00 for other alloys |
ka |
= |
|
ta |
= |
thickness of aluminium plating |
ts |
= |
thickness of mild steel plating |
Za |
= |
section modulus of aluminium stiffener |
Zs |
= |
section modulus of mild steel stiffener |
σa |
= |
0,2 per cent proof stress or 70 per cent of the
ultimate strength of the material, whichever is the lesser. |
1.4.3 In general, for welded structures, the maximum value of sa to be used in the
scantlings derivation is that of the aluminium in the welded condition. However,
consideration will be given to using unwelded values depending upon the weld line
location and other heat affected zones, in relation to the maximum applied stress on
the member (e.g. extruded sections).
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