Section 2 Hull strengthening requirements
Clasification Society 2024 - Version 9.40
Clasifications Register Rules and Regulations - Rules and Regulations for the Classification of Naval Ships, January 2023 - Volume 3 Additional Class Notations - Part 1 Ship Type Capability - Chapter 1 Ice Navigation - First-Year Ice Conditions - Section 2 Hull strengthening requirements

Section 2 Hull strengthening requirements

2.1 Application

2.1.1 Where the notation 'Ice Class 1AS, 1A, 1B, or 1C' as specified in Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15 is desired, the ship is to comply with the requirements of this Section, in addition to those for sea-going service, so far as they are applicable.

2.1.2 The vertical extent of the ice strengthening is related to the ice light and ice load waterlines, which are defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions . The maximum and minimum Ice Class draughts at both the fore and aft ends will be stated on the Class Certificate.

2.1.3 The ballast capacity of the ship is to be sufficient to give adequate propeller immersion in all ice navigating conditions without trimming the ship in such a manner that the actual waterline at the bow is below the ice light waterline.

2.1.4 Fresh-water and sea-water ballast tanks, the tops of which are situated above the minimum operating condition waterline and adjacent to the shell, and which are intended to be used in ice and cold navigation conditions, are to be provided with means to prevent freezing. It is to be demonstrated that such means protect against the following:

  1. Hull structural damage caused by tank contents being pumped from beneath a layer of ice, thereby drawing a vacuum into the tank.

  2. Hull structural damage caused by ice expansion.

  3. Tank internal piping and other components being damaged by ice expansion or blockage by ice.

  4. Tank internal piping and other components being mechanically damaged by falling pieces of ice.

Heating coils are considered effective means for tanks entirely above the waterline. Heating coils, continuous circulation, air bubbling or alarms and instrumentation are considered effective means for tanks partially below the waterline. Alternatively, submission of documentary evidence of service experience, testing, calculations or a combination thereof may be used to demonstrate that the above hazards have been mitigated.

2.1.5 The requirements of this Section are formulated for both transverse and longitudinal framing systems but it is recommended that, whenever practicable, transverse framing is selected.

2.1.6 The requirements of this Section assume that when approaching ice infested waters the ship’s speed will be reduced appropriately. The vertical extent of ice strengthening for ships intended to operate at speeds exceeding 15 knots in areas containing isolated ice floes will be specially considered.

2.1.7 An icebreaking ship is to have a hull form at the fore end adapted to break ice effectively. It is recommended that bulbous bows are not fitted to Ice Class 1AS ships.

2.1.8 The stern of an icebreaking ship is to have a form such that broken ice is effectively displaced.

2.1.9 Where it is desired to make provision for short tow operations, the bow area is to be suitably reinforced. Similarly, ice breakers may require local reinforcement in way of the stern fork.

2.2 Definitions

2.2.1 The Ice Deep Waterline corresponds to the Deep Draught Waterline. Where specially requested, an Ice Deep Waterline may be specified which differs from the foregoing, but corresponds to the deepest condition in which the ship is expected to navigate in ice. See Vol 1, Pt 3, Ch 1, 5.3 Margins for margins.

2.2.2 The Ice Light Waterline is that corresponding to the lightest condition in which the ship is expected to navigate in ice. However, it is recommended that the minimum draught at the fore end is not to be less than:

where

h = the nominal ice thickness, in metres, associated with the desired Ice Class, see Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15.
Δ = displacement as defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions 2.2.11.

2.2.3 The Ice Deep Waterline and the Ice Light Waterline are to be indicated on the plans.

2.2.4 The Main Ice Belt Zone extends vertically above and below the waterline defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions 2.2.1 and Vol 3, Pt 1, Ch 1, 2.2 Definitions 2.2.2 by the distances shown in Table 1.2.1 Vertical extent of main ice belt zone. For ships fitted with a bulbous bow, the vertical extent of the Main Belt Zone will be suitably increased.

Figure 1.2.1 Regions and zones (First year ice conditions)

Table 1.2.1 Vertical extent of main ice belt zone

Class Above Ice
Load Waterline (mm)
Below Ice
Light Waterline (mm)
1AS
1A
1B
1C
600
500
400
400
750
600
500
500

2.2.5 The Forward Region extends from the stem to aft of the forward borderline of the flat side of the hull by a distance equal to the greater of 0,04L R or 5 m for ice classes 1AS and 1A, or the greater of 0,02L R or 2 m for ice classes 1B and 1C. Where no clear forward borderline of the flat side of the hull is discernible, the aft boundary of the forward region is to be taken 0,4L R aft of the forward perpendicular.

2.2.6  Forefoot Region 1 is the area below the main ice belt zone extending from the stem, or the fore end of the bulb where a bulbous bow is fitted, to a position five frame spaces aft of the point of intersection between the level keel line and the raked stem.

2.2.7  Forefoot Region 2 is the area below the main ice belt extending from the aft boundary of Forefoot Region 1 to the aft boundary of the forward region and encompasses both side and bottom shell plating.

2.2.8 The Shoulder Region is a part of the main ice belt zone in the forward region and extends from the aft boundary of the forward region to forward of the forward borderline of the flat side of the hull by a distance of 0,04L R for ice classes 1AS and 1A or 0,02L R for ice classes 1B and 1C. Where no clear forward borderline of the flat side of the hull is discernible, the forward boundary of the shoulder region is to be taken 0,32L R aft of the forward perpendicular for ice classes 1AS and 1A or 0,36L R aft of the forward perpendicular for ice classes 1B and 1C. The extent of the shoulder region forward of its aft boundary is not to be taken as less than 10 m for ice classes 1AS and 1A or 4 m for ice classes 1B and 1C.

2.2.9 The Midship Region extends from the aft boundary of the forward region to aft of the aft borderline of the flat side of the hull by a distance equal to the greater of 0,04L R or 5 m for ice classes 1AS and 1A or the greater of 0,02L R or 2 m for ice classes 1B and 1C. Where no clear aft borderline of the flat side of the hull is discernible, the aft boundary of the midship region is to be taken 0,2L R forward of the aft perpendicular.

2.2.10 The Aft Region extends from the aft boundary of the midship region to the stern.

2.2.11  Displacement ∆ is the displacement, in tonnes, at the Ice Deep Waterline when floating in water having a relative density of 1,0.

2.2.12  Shaft power, P 0 , is the maximum propulsion shaft power, in kW, for which the machinery is to be classed.

2.3 Powering of ice strengthened ships

2.3.1 The total shaft power installed in ice strengthened ships is to be not less than P required by Vol 3, Pt 1, Ch 1, 3 Machinery and engineering systems for the desired Ice Class notation.

2.3.2 Ice strengthened ships which are to be considered to have an independent icebreaking capability are to be able to develop sufficient thrust to permit continuous mode icebreaking at a speed of at least five knots in ice having a thickness equal to the nominal value specified in Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15 for the desired Ice Class and a snow cover of at least 0,3 m.

2.3.3 The requirements of Vol 3, Pt 1, Ch 1, 2.4 Shell plating are formulated on the assumption that the shaft power necessary to provide an independent icebreaking capability as described in Vol 3, Pt 1, Ch 1, 2.3 Powering of ice strengthened ships 2.3.2 can be determined by the equation:

P 1 = 0,736C 1 C 2 C 3 C 4 [240B h (1 + h + 0,035v2) +70S c )]
where
B = breadth as defined in Vol 1, Pt 3, Ch 1, 5 Definitions
C 1 = , but is not to be taken as less than 1,0
C 2 = 0,9 if the ship is fitted with a controllable pitch propeller, otherwise 1,0
C 3 = 0,9 if the rake of the stem is 45º or less, otherwise 1,0. The product C 2 C 3 is not to be taken as less than 0,85
C 4 = 1,1 if the ship is fitted with a bulbous bow, otherwise 1,0
h = ice thickness as defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions 2.2.2
S c = depth of snow cover
v = ship speed, in knots, when breaking ice of thickness h

2.3.4 The ice strengthening requirements of Vol 3, Pt 1, Ch 1, 2.4 Shell plating include a power-displacement correction factor, γ, which is to be determined as follows:

  1. Forward region

    γ = 0,653 + 3,217 x 10-5
    or γ = 0,876 + 9,908 × 10-6
    or γ = 1,0 whichever is the least

    where P 0 and Δ are as defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions .

    For ships assigned ice classes 1AS and 1A, in which the installed shaft power P 0 exceeds the shaft power P 1 determined in accordance with Vol 3, Pt 1, Ch 1, 2.3 Powering of ice strengthened ships 2.3.3 when the ship speed is taken as five knots, the ice thickness, h, as defined in Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15 and the snow cover S c is taken as 0,3 m, γ for the forward region is to be multiplied by the following factor:

    1. for shell plating


      1 + 0,1

    2. for framing, stringers and web frames

      1 + 0,05

      but γ need not be taken greater than 1,1.

  2. Midship and aft regions

    γ = 0,653 + 9,908 × 10-6
    or = 0,79, whichever is the lesser.

2.4 Shell plating

2.4.1 In way of the main ice belt zone, the thickness of the shell plating is not to be less than:

t = As αp β γ + c mm
where
c = corrosion-abrasion increment to be taken as 2 mm for first-year ice classes, see also Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.3
s = distance to the adjacent main or intermediate frame, in mm
A = 0,40 in association with transverse framing
= 0,41 in association with longitudinal framing
αp = longitudinal distribution factor, dependent on Ice Class and longitudinal position, as given in Table 1.2.2 Longitudinal distribution factor-shell plating
β = vertical distribution factor, to be taken as 1,0 for all first-year ice classes
γ = power-displacement factor determined in accordance with Vol 3, Pt 1, Ch 1, 2.3 Powering of ice strengthened ships 2.3.4
σo = specified minimum yield stress of the steel, in N/mm2. For mild steel the value 235 N/mm2 is to be used.

Table 1.2.2 Longitudinal distribution factor-shell plating

Ice Class αp
Forward Midship Aft
1AS
1A
1B
1C
1,00
0,98
0,93
0,86
0,95
0,86
0,71
0,53
0,85
0,73
0,57
0,38

2.4.2 Where operation in first-year ice is an emergency feature as recognised by Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15 with a * annotated to the Ice Class notation, consideration will be given to the use of fully plastic design criteria for the shell plating.

2.4.3 If a recognised abrasion resistant coating is to be applied in way of the main ice belt and is to be maintained in good condition during service, the thickness determined in accordance with Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1 may be reduced by 1 mm. See the Rules for the Manufacture, Testing and Certification of Materials, July 2022, Ch 15, 2.13 Ice coatings.

2.4.4 For ice classes 1AS and 1A, where the hull form includes a pronounced shoulder, the value of the corrosion-abrasion increment in the shoulder region will be specially considered.

2.4.5 For ice classes 1AS and 1A, the thickness of shell plating is to be as follows:

  1. In Forefoot Region 1 – not less than that determined in accordance with Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1 for the main ice belt zone in the forward region.

  2. In Forefoot Region 2 – 2 mm greater than that required by Vol 1, Pt 6, Ch 3 Scantling Determination or Vol 1, Pt 7 Enhanced Structural Assessment (Provisional) for ships with TLA notation.

  3. For the forward 0,2L R, the region 2 m above the main ice belt zone in ships having an open water speed equal to and exceeding 17,5 knots (9 m/sec) – not less than that required in the ice belt in the Midship Region.

2.4.6 Changes in plating thicknesses in the longitudinal direction are to take place gradually. Side scuttles are not to be situated in the ice belt.

2.4.7 If the weather deck in any part of the ship is situated below the upper limit of the ice belt, as may be the case of a raised-quarter decker, the bulwark is to be reinforced to a standard required for the shell plating in the main ice belt.

2.5 Transverse framing

2.5.1 The increased requirements for transversely framed structures are normally met by the addition of intermediate frames.

2.5.2 Ships with shock enhanced notation transverse intermediate frames are not to be fitted. The ice strengthening requirements are to be met by the use of reduced main frame spacing.

2.5.3 The section modulus of transverse main and intermediate frames (including a width of attached plating equal to s), is to be determined in accordance with the following formula:

Z = Cs αt β γ2 (3 2h 2) K cm3
where
d = distance, in metres, measured along the frame from the lower span point to the ice deep waterline or from the upper span point to the ice light waterline, whichever is the lesser. In no case is this distance to be taken greater than
h = nominal ice thickness, in metres, for the Ice Class as defined in Vol 1, Pt 1, Ch 2, 3.10 Other notations 3.10.15

s, β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1

C = 12,5
K = but is not to be taken greater than 1,0 nor less than 0,3. If the lower span point is above the ice load waterline or the upper span point is below the ice light waterline, then k is to be taken as 0,3
αt = longitudinal distribution factor, dependent on Ice Class and longitudinal position, as given in Table 1.2.3 Longitudinal distribution factor - transverse framing
= span, in metres, measured along a chord at the side between the span points. For definitions of span points, see Vol 1, Pt 6, Ch 2, 2 Structural design. Where adjacent main and intermediate frames have different end connections, resulting in different spans, a mean value is to be used.

Table 1.2.3 Longitudinal distribution factor - transverse framing

Ice Class αt
Forward Midship Aft
1AS
1A
1B
1C
1,00
0,89
0,78
0,66
0,87
0,68
0,49
0,31
0,66
0,49
0,33
0,16

2.5.4 The inertia of transverse main and intermediate frames including a width of attached plating equal to s is to be determined in accordance with the following formula:

= 4Z cm4
where

2.5.5 The cross-sectional shear resisting area of transverse main and intermediate frames is to be determined in accordance with the following formula:

A = Cs αt β γ2 K s cm2

where s, β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1

C = 3,75
K s = 0,5 if the upper span point is below the bottom edge of the main ice belt zone or the lower span point is above the upper edge of the main ice belt zone
= 1,0 for all other cases

2.5.6 Except as allowed by Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.7, main and intermediate frames having scantlings as required by Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.2 are to be continued and bracketed to the first primary longitudinal member outside of the minimum extent of ice framing given in Table 1.2.4 Minimum extent of ice framing or to the top of floors in ships having a single bottom. In the latter case intermediate frames will require to be bracketed, or otherwise efficiently attached to a gusset plate which is to be fitted at the level of top of floors. The free edge of the horizontal gusset should be suitably supported. In this context a primary longitudinal member is defined as either a deck, inner bottom, margin plate, deep tank top or ice stringer complying with the requirements of Vol 3, Pt 1, Ch 1, 2.8 Primary longitudinal members supporting transverse ice framing.

Table 1.2.4 Minimum extent of ice framing

Ice Class Region Minimum extent of ice framing
Above Ice Deep Waterline (mm) Below Ice Light Waterline (mm)
1AS Forward
(stem to 0,3L R)
1200 To double bottom or top of floors or 1600 mm, whichever is the greater
Forward (abaft 0,3L R) and Midship 1200 1600
Aft 1200 1200
1A,
1B,
1C
Forward
(stem to 0,3L R)
1000 1600
Forward (abaft 0,3L R) and Midship 1000 1300
Aft 1000 1000

2.5.7 If a primary longitudinal member is fitted within 0,25 m inside a boundary of the minimum extent of ice framing, intermediate frames may be terminated at that member.

2.5.8 If a primary longitudinal member is fitted within 1 m inside a boundary of the minimum extent of ice framing, the intermediate frames may be terminated at that boundary, provided that their ends are attached to the adjacent main frames by a horizontal intercostal member having the same scantlings as the intermediate frames.

2.5.9 If primary longitudinal members are not fitted, or are located more than 1 m inside a boundary of the minimum extent of ice framing, then the intermediate frames may be either:

  1. extended to a primary longitudinal member or equivalent as defined by Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.6.

  2. terminated at the boundary of minimum extent of ice framing and attached by a horizontal intercostal member, having the same scantlings as the intermediate frames, to the adjacent main frames. The scantlings of the main frames are to be based on the spacing and span of the main frames. The inertia of the intermediate frames is to be not less than 75 per cent of the main frames.

2.5.10 Except where provided for in Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.7 and Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.9, the ends of intermediate frames are to be bracketed or otherwise efficiently attached to a primary longitudinal member or are to be attached to adjacent brackets, floors or main frames by a longitudinal flat bar. see also Vol 3, Pt 1, Ch 1, 2.7 Framing - General requirements 2.7.5.

2.5.11 In twin screw ships, three intermediate frames forward of, and three aft of, the propeller blade tips are to extend to the double bottom.

2.6 Longitudinal framing

2.6.1 The section modulus of longitudinal frames (including a width of attached plating equal to s), is to be determined in accordance with the following formula:

Z = Cs αl β γ2 2 cm3
where
h = ice thickness as defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions 2.2.2
= is as defined in Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.3
s = spacing, in mm, of longitudinal frames but need not be taken as greater than 1000h
C = 16,6
αl = longitudinal distribution factor, dependent on Ice Class and longitudinal position, as given in Table 1.2.5 Longitudinal distribution factor-longitudinal framing

β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

Table 1.2.5 Longitudinal distribution factor-longitudinal framing

Ice Class α1
Forward Midship Aft
1AS
1A
1B
1C
1,00
0,90
0,80
0,68
0,95
0,74
0,51
0,32
0,71
0,53
0,34
0,16

2.6.2 The inertia of longitudinal frames, including a width of attached plating equal to s, is to be determined in accordance with the following formula:

= Cs αl β γ2 2,3 cm4

where

C = 270

Other symbols are as defined in Vol 3, Pt 1, Ch 1, 2.6 Longitudinal framing 2.6.1.

2.6.3 The cross-sectional shear resisting area of longitudinal frames is to be determined in accordance with the following formula:

A = Fs αl β γ2 cm2

where

F = 2,5

Other symbols are as defined in Vol 3, Pt 1, Ch 1, 2.6 Longitudinal framing 2.6.1.

2.6.4 Where longitudinal framing is adopted, frames satisfying the requirements of Vol 3, Pt 1, Ch 1, 2.6 Longitudinal framing 2.6.1 to Vol 3, Pt 1, Ch 1, 2.6 Longitudinal framing 2.6.3 are to be fitted within the minimum vertical extent of ice framing in Table 1.2.4 Minimum extent of ice framing.

2.7 Framing - General requirements

2.7.1 The web thickness of ice frames is not, in general, to be less than half that of the attached shell plating with a minimum of 9 mm.

2.7.2 Where a frame intersects a boundary between two of the hull regions defined in Vol 3, Pt 1, Ch 1, 2.2 Definitions , the scantling requirements applicable will be those for the forward region if the forward midship boundary is intersected or for the midship region if the aft midship boundary is intersected.

2.7.3 Main and intermediate frames within the minimum extent of ice framing given in Table 1.2.4 Minimum extent of ice framing are to be efficiently supported to prevent tripping, e.g. as shown in Figure 1.2.2 Framing support. The distance between anti-tripping supports is not to exceed 1500 mm. The extent of anti-tripping supports is to be as given in Table 1.2.6 Extent of anti-tripping supports.

Figure 1.2.2 Framing support

Table 1.2.6 Extent of anti-tripping supports

Ice Class Extent of anti-tripping supports
1AS
1A
1B
1C
All regions
Forward and midship region
Forward region
Forward region

2.7.4 Ice frames are to be attached to the shell plating by double continuous welding and are not to be scalloped except at shell plating seams or butts. However, in the case of the aft region for Ice Class 1A, 1B and 1C and the midship region for Ice Class 1B and 1C, consideration will be given to the use of intermittent welding provided the requirements of Vol 1, Pt 6, Ch 6, 5.9 Intermittent and single sided fillet welding are complied with.

2.7.5 Frames are to be effectively attached to supporting structure by brackets. In general, longitudinals are to be connected to both sides of cut-outs in the webs of transverse structure.

2.7.6 The effective weld area attaching ice frames to primary members is not to be less than the shear area for the frames as required by Vol 3, Pt 1, Ch 1, 2.5 Transverse framing 2.5.2 or Vol 3, Pt 1, Ch 1, 2.6 Longitudinal framing 2.6.3, as appropriate.

2.7.7 Where a bulkhead or deck is fitted instead of an ice strengthened frame, the thickness of the bulkhead or deck adjacent to the shell is normally to be that of the frame for a width sufficient to give an area equal to the frame.

2.8 Primary longitudinal members supporting transverse ice framing

2.8.1 The section modulus of ice stringers or of decks adjacent to hatchways, including a width of attached plating determined in accordance with Vol 1, Pt 6, Ch 2, 2.3 Section properties and taken about an axis parallel to the plating, is to be determined in accordance with the following formula:

Z = C αo β γ2 2 cm3
where
= span, in metres, of the ice stringer or deck adjacent to a hatchway determined in accordance with Vol 1, Pt 6, Ch 2, 2 Structural design.
C = 11 300
αo = longitudinal distribution factor, dependent on Ice class and longitudinal position, as given in Table 1.2.7 Longitudinal distribution factor-primary longitudinal members

β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

Table 1.2.7 Longitudinal distribution factor-primary longitudinal members

Ice Class αo
Forward Midship Aft
1AS
1A
1B
1C
1,00
0,87
0,78
0,68
0,98
0,75
0,64
0,53
0,89
0,64
0,51
0,37

2.8.2 The cross-sectional shear resisting area of ice stringers or of decks adjacent to hatchways is to be determined in accordance with the following formula:

A = C αo β γ2 cm2

where

C = 1240

Other symbols are as defined in Vol 3, Pt 1, Ch 1, 2.8 Primary longitudinal members supporting transverse ice framing 2.8.1.

2.8.3 Where the span of a deck adjacent to a hatchway exceeds 10 times the width of the deck strip the scantlings of the deck section may require special consideration to ensure adequate stiffness.

2.8.4 The webs of primary longitudinal members supporting transverse ice frames are to be stiffened and connected to the main or intermediate frames so that the distance, r, between such stiffening is not to be greater than given according to the following formula:

r = mm

where

t = thickness, in mm, of the primary longitudinal member adjacent to the shell plating

Other symbols are as defined in Vol 3, Pt 1, Ch 1, 2.8 Primary longitudinal members supporting transverse ice framing 2.8.1.

2.8.5 The minimum thickness of the web plating of longitudinal primary members is to comply with the requirements of Vol 1, Pt 6, Ch 6, 6 Construction details.

2.9 Web frames

2.9.1 The section modulus of web frames supporting ice stringers or longitudinal ice frames including a width of attached plating determined in accordance with Vol 1, Pt 6, Ch 2, 2 Structural design and taken about an axis parallel to the plating is to be determined in accordance with the following formula:

Z = Cs αo β γ2 cm3

where

= span, in metres, of the web frames determined in accordance with Vol 1, Pt 6, Ch 2, 2 Structural design
s = spacing of web frames, in metres
C = 20 600
αo = longitudinal distribution factor as given in Table 1.2.7 Longitudinal distribution factor-primary longitudinal members

β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

2.9.2 The cross-sectional shear resisting area of web frames supporting ice stringers or longitudinal ice frames is to be determined in accordance with the following formula:

A = C αo β γ2 s cm2

where

C = 1240

αo and s are as defined in Vol 3, Pt 1, Ch 1, 2.9 Web frames 2.9.1

β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

2.9.3 Ice stringers are to be bracketed or otherwise efficiently attached to the web frames or transverse bulkheads.

2.9.4 The thickness of the web is generally not to be less than one per cent of the web depth.

2.10 Stem

2.10.1 The stem is to be made of rolled, cast or forged steel or of shaped steel plates. A sharp edged stem, as shown in Figure 1.2.3 A sharp edged stem improves the manoeuvrability of the ship in ice.

Figure 1.2.3 A sharp edged stem

2.10.2 The section modulus of the stem in the fore and aft direction is not to be less than determined in accordance with the following formula:

Z = cm3

where

αo = longitudinal distribution factor for the forward region as given in Table 1.2.3 Longitudinal distribution factor - transverse framing

β and γ are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

2.10.3 The dimensions of a welded stem constructed as shown in Figure 1.2.3 A sharp edged stem are to be determined in accordance with the following formula:

t = 31 mm

where

t = thickness of the side plates, in mm.

2.10.4 The plate thickness, t, of a shaped plate stem or a bulbous bow is to be determined in accordance with the following formula:

t = As αp β γ + 2 mm

where

s = the distance, in mm, between horizontal webs diaphragm plates having a thickness of at least 0,5t mm
A = 0,50

αp, β, γ and σo are as defined in Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

2.10.5  The reinforced stem is to extend from the keel plate to 750 mm above the ice load waterline and is to be internally strengthened by floors, brackets or webs having a thickness of at least 0,5t and spaced not more than 600 mm apart.

2.10.6 In bulbous bow constructions the extent of plating having the thickness, t, as specified in Vol 3, Pt 1, Ch 1, 2.10 Stem 2.10.4, below the ice light waterline should be such as to cover that part of the bulb forward of the vertical line originating at the intersection of the ice light waterline and the stem contour at the centreline. A suitably tapered transition piece should be arranged between the reinforced stem plating and keel. However, in no case should the reinforced stem plating extend vertically below the Ice Light Waterline for less than 750 mm. The adjacent strake to the reinforced shaped stem plating of the bulb should be in accordance with the requirements of Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1.

2.10.7 Where in the ice belt region the radius of the stem or bulb front plating is large, one or more vertical stiffeners are to be fitted in order to meet the section modulus requirement of Vol 3, Pt 1, Ch 1, 2.10 Stem 2.10.2. In addition, vertical ring stiffening will be required for the bulb.

2.10.8 The dimensions of the stem may be tapered to the requirements of Vol 1, Pt 6, Ch 3, 5.2 Plate keel at the upper deck. The connections of the shell plating to the stem are to be flush.

2.10.9 For towing purposes, a mooring pipe with an opening not less than 250 mm by 300 mm having inner surfaces at least 150 mm wide with a rounding radius of not less than 100 mm is to be fitted in the bow bulwark on the centreline. A bitt, or other convenient means of securing the line, is to be dimensioned to withstand the breaking strength of the ship’s towline.

2.11 Stern

2.11.1 Where the screwshaft diameter exceeds the Rule diameter, the propeller post is to be correspondingly strengthened. see Vol 1, Pt 3, Ch 3, 2 Rudders.

2.11.2 A transom stern is not normally to extend below the ice load waterline. Where this cannot be avoided, the transom is to be kept as narrow as possible and the scantlings of plating and stiffeners are to be as required for the midship region.

2.12 Bossings and shaft struts

2.12.1 Shaftings and sterntubes of ships with two or more propellers are generally to be enclosed within plated bossings. If detached supporting struts are necessary, their design, strengthening and attachment to the hull will be specially considered.

2.13 Rudder and steering arrangements

2.13.1 Rudder posts, rudder horns, solepieces, rudder stocks and pintles are to be dimensioned in accordance with Vol 1, Pt 3, Ch 3, 2 Rudders and Vol 1, Pt 3, Ch 3, 2.9 Rudder strength calculation as appropriate. Rudder scantlings are to be determined in accordance with Vol 1, Pt 3, Ch 3, 2 Rudders using the basic stock diameter, δs. The speed used in the calculations is to be the service speed or that given in Table 1.2.8 Minimum speeds, whichever is the greater. When used in association with the speed given in Table 1.2.8 Minimum speeds, the hull form factor and rudder profile coefficients are to be taken as 1,0.

Table 1.2.8 Minimum speeds

Ice Class Minimum speed, in knots
1AS
1A
1B
1C
20
18
16
14

2.13.2 For double plate rudders, the minimum thickness of plating and horizontal and vertical webs in the main ice belt zone is to be determined as for shell plating in the aft region in accordance with Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1. For the horizontal and vertical webs the corrosion-abrasion increment, c, need not be added.

2.13.3 For ice classes 1AS and 1A, the rudder head and the upper edge of the rudder are to be protected against ice pressure by an ice knife, or equivalent.

2.13.4 Due regard is to be paid to the method of securing the rudder in the centreline position when backing into ice. Where possible, rudder stoppers working on the blade or rudder head are to be fitted.

2.13.5 Where an ice class notation is included in the class of a ship, the nozzle construction requirements as defined in Vol 1, Pt 3, Ch 3, 5 Fixed and steering nozzles, bow and stern thrust units, ducted propellers are to be upgraded to include abrasion allowance as follows:

Ice Class Thickness increment
1AS
1A
1B
1C
5 mm
4 mm
3 mm
2 mm

However, the thickness of the shroud plating is not to be less than the shell plating for the aft region as obtained from Vol 3, Pt 1, Ch 1, 2.4 Shell plating 2.4.1 taking frame spacing s in the formula as 500 mm.

2.13.6 The scantlings of the stock, pintles, gudgeon and solepiece associated with the nozzle are to be increased on the basis given in Vol 3, Pt 1, Ch 1, 2.13 Rudder and steering arrangements 2.13.1. However, the diameter of the nozzle stock is to be not less than that calculated in the astern condition taking the astern speed as half the speed given in Table 1.2.8 Minimum speeds or the actual astern speed, whichever is the greater.

2.13.7 Nozzles with articulated flaps will be subject to special consideration.

2.14 Direct calculations

2.14.1 If, as an alternative to the requirements of Vol 3, Pt 1, Ch 1, 2.8 Primary longitudinal members supporting transverse ice framing and Vol 3, Pt 1, Ch 1, 2.9 Web frames, the scantlings of primary longitudinal members and web frames are determined by direct calculation, as permitted by Vol 1, Pt 3, Ch 1, 2 Direct calculations, then:

  1. the applied ice load may be taken as 775αo β γ2 kN per metre of ship length evenly distributed over a depth equal to the nominal ice thickness, h, for the Ice Class;

  2. the scantlings are to be suitable for the centre of the load depth to be located at any height between the ice load waterline and the ice light waterline;

  3. the scantlings determined in association with Vol 3, Pt 1, Ch 1, 2.14 Direct calculations 2.14.1 and Vol 3, Pt 1, Ch 1, 2.14 Direct calculations 2.14.1.(b) are to be sufficient to ensure that the von Mises-Hencky combined stress does not exceed 90 per cent of the yield stress of the steel.


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