Section 5 Single bottom structure and appendages
Clasification Society 2024 - Version 9.40
Clasifications Register Rules and Regulations - Rules and Regulations for the Classification of Special Service Craft, July 2022 - Part 8 Hull Construction in Composite - Chapter 3 Scantling Determination for Mono-Hull Craft - Section 5 Single bottom structure and appendages

Section 5 Single bottom structure and appendages

5.1 General

5.1.1 The requirements of this Section provide for single bottom construction of mono-hull craft in association with either transverse or longitudinal framing.

5.1.2 All girders are to extend as far forward and aft as practicable and care is to be taken to avoid any abrupt discontinuity particularly in way of skegs. Where girders are cut at bulkheads, their longitudinal strength is to be maintained.

5.1.3 Particular attention is to be taken to ensure that the continuity of structural strength in way of the intersection of transverse floors and longitudinal girders is maintained. The face reinforcement of such stiffening members is to be effectively continuous.

5.1.4 The single bottom structure in way of the keel, skeg and girders is to be sufficient to withstand the forces imposed by dry-docking the craft.

5.1.5 The breadth and thickness of plate keels are to comply with the requirements detailed in Pt 8, Ch 3, 3.2 Keel plate. See also Pt 8, Ch 3, 3.9 Skeg 3.9.1.

5.2 Centreline girder

5.2.1 In craft with single bottoms, a centreline girder is, in general, to be fitted in association with transverse frames, transverses supporting longitudinals or where the breadth of floors at the upper edge is greater than 1,5 m.

5.2.2 Centreline girders may be in the form of intercostal or continuous top hat or plate webs. Where the girder is intercostal, additional bracketing and local reinforcement as given in Pt 8, Ch 3, 3.14 Local reinforcement are to be provided to maintain the continuity of structural strength. The face reinforcement in all cases is to be continuous.

5.2.3 The web depth of the centre girder in general is to be equal to the depth of the floors at the centreline as specified in Pt 8, Ch 3, 5.4 Floors, general.

5.2.4 The web thickness, t w, for a centre girder of `top-hat' type section is to be not less than that required by Pt 8, Ch 3, 1.17 Stiffener proportions or as determined as follows, whichever is the greater:

in no case is t w to be taken less than 5,0 mm

where k A and L R are as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

5.2.5 The web thickness for a centre girder of single plate laminate construction is to be two times the thickness as required by Pt 8, Ch 3, 5.2 Centreline girder 5.2.4.

5.2.6 The face area of the centre girder, A f, is to be not less than:

where k A and L R are as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

5.2.7 The face area of the centre girder outside 0,5L about midships may be reduced to 80 per cent of the value given in Pt 8, Ch 3, 5.2 Centreline girder 5.2.6.

5.2.8 The face thickness, t f, is to be not less than the web thickness of the centre girder.

5.2.9 Additionally, the requirements of Pt 8, Ch 3, 4.5 Bottom longitudinal primary stiffeners for bottom longitudinal primary stiffeners are to be complied with.

5.3 Side girders

5.3.1 Where the floor breadth at the upper edge exceeds 6,0 m, side girders are to be fitted at each side of the centre girder such that the spacing between the side and centre girders or between the side girders themselves is not greater than 3 m. Side girders, where fitted, are to extend as far forward and aft as practicable and are, in general, to terminate in way of bulkheads, deep floors or other primary transverse structure.

5.3.2 In the engine room, additional side girders are generally to be fitted in way of the main machinery.

5.3.3 The face area of side girders, A f, is not to be taken as less than:

where k A and L R are as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

5.3.4 The face thickness, t f, is not, in general, to be less than the web thickness of the side girder.

5.3.5 The web thickness, t w, for side girders of `top-hat' type section is to be not less than as required by Pt 8, Ch 3, 1.17 Stiffener proportions or as determined as follows, whichever is the greater:

where k A and L R are as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1

in no case is t w to be taken less than 5,0 mm.

5.3.6 The web thickness for side girders of single plate laminate construction is to be two times the thickness as required by Pt 8, Ch 3, 5.3 Side girders 5.3.5.

5.3.7 In addition, the requirements of Pt 8, Ch 3, 4.5 Bottom longitudinal primary stiffeners for bottom longitudinal primary stiffeners are to be complied with.

5.3.8 Watertight side girders, or side girders forming boundaries of tank spaces, are also to comply with the requirements for watertight bulkheads or deep tanks as detailed in Pt 8, Ch 3, 7.3 Watertight bulkheads and Pt 8, Ch 3, 7.4 Deep tanks respectively.

5.4 Floors, general

5.4.1 In transversely framed craft, floors are generally to be fitted at every frame and underneath each bulkhead.

5.4.2 In longitudinally framed craft, floors are to be fitted at every transverse web frame and bulkhead and generally at a spacing not exceeding 2 m. Additional transverse floors or webs are, in general, to be fitted at half web-frame spacing in way of engine seatings and thrust bearings, pillars, skegs, ballast/bilge keels and the bottom of the craft in the forefoot region.

5.4.3 The overall depth of transverse floors at the centreline, d f, is not to be taken as less than:

when B < 10 m d f =40 (B + 0,85D) mm
when B ≥ 10 m d f = 40 (1,5B + 0,85D) - 200 mm

where B is as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

5.4.4 The web thickness, t w, for transverse floors of `top-hat' type section is to be not less than that required by Pt 8, Ch 3, 1.17 Stiffener proportions or as determined as follows, whichever is the greater:

where
d f = is as defined in Pt 8, Ch 3, 5.4 Floors, general 5.4.3

k A and s are defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

In no case is t w to be taken less than 5,0 mm.

5.4.5 The web thickness for transverse floors of single plate laminate construction is to be two times the thickness as required by Pt 8, Ch 3, 5.4 Floors, general 5.4.4.

5.4.6 If side frames are attached to the floors by brackets, the depth of floor may be reduced by 15 per cent and the floor thickness determined using the reduced depth. The brackets are to have the same thickness as the floors, and their arm lengths clear of the frame are to be the same as the reduced floor depth given above.

5.4.7 The face area of floors, A f, is not to be taken as less than:

where k A and L R are as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1.

5.4.8 The thickness of the face reinforcement, t f, is to be not less than the web thickness.

5.4.9 In addition, the requirements of Pt 8, Ch 3, 4.8 Bottom transverse web frames for bottom transverse web frames are to be complied with.

5.4.10 Floors are generally to be continuous from side to side.

5.4.11 The tops of floors, in general, may be level from side to side. However, in craft having considerable rise of floor the depth of the floor plate may require to be increased to maintain the required mechanical properties of the section.

5.4.12 The floors in the aft peak are to extend over and provide efficient support to the sterntube where applicable.

5.4.13 Watertight floors, or floors forming boundaries of tank spaces, are also to comply with the requirements for watertight bulkheads or deep tanks as detailed in Pt 8, Ch 3, 7.3 Watertight bulkheads or Pt 8, Ch 3, 7.4 Deep tanks respectively.

5.5 Floors in machinery spaces

5.5.1 Floors within machinery spaces are to comply with the requirements of Pt 8, Ch 3, 5.4 Floors, general.

5.5.2 The depth and mechanical properties of floors between engine or gearbox girders is to be not less than that required to maintain continuity of structural integrity or 50 per cent of the depth given in Pt 8, Ch 3, 5.4 Floors, general 5.4.3. The web thickness and face reinforcement weight of such reduced height floors are to be increased appropriately in order to maintain the continuity of structural strength.

5.6 Machinery seating

5.6.1 The general requirements for machinery seating are given in Pt 3, Ch 2, 6.9 Machinery seatings.

5.6.2 Main and auxiliary engines are to be effectively secured to the hull structure by seatings of adequate scantlings to resist the gravitational thrust, torque and vibration forces which may be imposed upon them.

5.6.3 The longitudinal girders forming the engine seating are to extend as far forward and aft as is practicable and are to be adequately supported by transverse floors or brackets.

5.6.4 Where stiffening is of plate construction, engine holding-down bolts are to be arranged as near as practicable to floors and longitudinal girders. When this cannot be achieved, bracket floors are to be fitted.

5.6.5 Machinery seatings are to be attached by means of primary bonding angles in accordance with Pt 8, Ch 3, 1.19 Boundary bonding.

5.7 Drainage arrangements

5.7.1 Suitable arrangements are to be made to provide free passage of air from all parts of the tanks to the air pipes, see also Pt 9, Ch 1, 5 Securing of machinery.

5.7.2 Sufficient limber holes are to be positioned in the internal bottom structure to allow for the drainage of water from all parts of the bilge to the pump suctions.

5.7.3 Particular attention is to be given to the positioning of limbers to ensure adequate drainage and to avoid stress concentrations. See LR's Guidance Notes for Calculation Procedures for Composite Construction.

5.7.4 Openings in the webs of stiffening sections, baffle plates, etc. are, in general, to be formed by moulded-in preforms under top hat type stiffening. Edges of openings in plate laminates are to be suitably sealed in accordance with Pt 8, Ch 3, 1.30 Openings in the webs of stiffening members.

5.8 Rudder horns

5.8.1 The scantlings of the rudder horn will be specially considered and in the case of high aspect ratio or novel designs direct calculations will be required to be submitted in accordance with Pt 3, Ch 1, 2 Direct calculations.

5.9 Sternframes

5.9.1 Where it is proposed to mould a composite sternframe, the scantlings and arrangements will be specially considered on the basis of direct calculations and loadings submitted by the Builders and designers.

5.10 Skeg construction

5.10.1 Skegs are to be effectively integrated into the adjacent structure and their design is to be such as to facilitate this, see also Pt 8, Ch 3, 3.9 Skeg.

5.10.2 The scantlings of skegs and the internal diaphragms at bulkheads and web frames are to be sufficient to withstand any docking forces to which they may be subjected.

5.11 Forefoot and stem

5.11.1 For craft of composite sandwich construction the forefoot region is to be so designed that in the event of local impact (see also Pt 8, Ch 3, 2.8 Impact considerations) with floating debris, the resultant damage will be limited. This may be achieved by:

  1. Arranging the individual plies of the laminate such that any delamination will be directed to the outer surface of the laminate, see Figure 3.5.1 Arrangement of laminate in way of forefoot and stem.

  2. The addition of a sacrificial `nose', see Figure 3.5.2 `Sacrificial nose'.

  3. By the addition of suitable sheathing, in accordance with Pt 8, Ch 3, 2.9 Sheathing.

  4. For vessels where the operating high speed waterline results in the exposure of the forefoot region, the laminate sequence in the keel area will be specially considered.

Figure 3.5.1 Arrangement of laminate in way of forefoot and stem

5.12 Transom knee

5.12.1 Centre and side girders are to be bracketed to the transom framing members by means of substantial knees. The face flat area of the girders may be gradually reduced to that of the transom stiffening member in accordance with Figure 3.5.3 Transom knee.

Figure 3.5.2 `Sacrificial nose'

Figure 3.5.3 Transom knee

5.12.2 Hard spots are to be avoided in way of the end connection, and care taken to ensure that the stiffening member to which the transom knee is bracketed can satisfactorily carry the transmitted bending moment.


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