Section 3 Shell envelope laminate
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 3 Shell envelope laminate

Section 3 Shell envelope laminate

3.1 General

3.1.1 The requirements in respect of the general plating elements of the shell envelope, excluding the deck, are contained within this Section.

3.2 Keel plate

3.2.1 The width, b K, and thickness, t K, of plate keels are not to be taken as less than:

where
k t =
L R = Rule length, in metres, as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1
σf = ultimate flexural strength of the keel plate material, in N/mm2, see Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.6

3.2.2 In no case is the thickness of the keel to be less than that of the adjacent bottom shell plating.

3.2.3 The width and thickness of plate keels are to be maintained throughout the length of the craft from the transom to a point not less than 25 per cent of the freeboard measured at the forward perpendicular (FP), above the deepest load waterline on the stem. Thereafter the keel thickness may be reduced to that required by Pt 8, Ch 3, 3.3 Stem plate for the stem. Laminate tapers are to be in accordance with Pt 8, Ch 2, 3.9 Laminate detail.

3.2.4 Where the bottom shell is of sandwich construction the keel is, in general, to be formed by locally returning to single skin construction for a width as required by Pt 8, Ch 3, 3.2 Keel plate 3.2.1. The Rule thickness of keel is to comprise both the inner and outer skins of the adjacent bottom shell sandwich plus additional reinforcement as required. The distribution of reinforcement in way of the plate keel and sandwich bottom structure is to be in accordance with Figure 3.3.1 Single skin/sandwich skin intersection detail.

Figure 3.3.1 Single skin/sandwich skin intersection detail

3.2.5 For large or novel craft, or yachts with externally attached ballast keels, or where it is proposed to incorporate keels of the `bar' type the scantlings of the keel will be specially considered.

3.3 Stem plate

3.3.1 The thickness of the plate stem, t s, is not to be taken as less than that given by the following expression:

where
k t = as defined in Pt 8, Ch 3, 3.2 Keel plate 3.2.1
L R = Rule length, in metres, as defined in Pt 8, Ch 3, 1.5 Symbols and definitions 1.5.1
σf = ultimate flexural strength of the stem plate material, in N/mm2, see Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.6.

3.3.2 In no case is the thickness of the plate stem to be taken as less than the thickness of the adjacent side shell plating.

3.3.3 The width of the plate stem is to be not less than the width of keel as required by Pt 8, Ch 3, 3.2 Keel plate 3.2.1.

3.3.4 Plate stems are to be supported by horizontal diaphragms and, where the stem radius is large, a centreline stiffener or web may be required.

3.3.5 Where the side shell is of sandwich construction the stem is to be formed by locally returning to single skin construction for a width as required by Pt 8, Ch 3, 3.2 Keel plate 3.2.1. The Rule thickness of stem is to comprise both the inner and outer skins of the adjacent side shell sandwich plus additional reinforcement as required. The distribution of reinforcement in way of the plate stem and sandwich bottom structure is to be in accordance with Figure 3.3.1 Single skin/sandwich skin intersection detail.

3.3.6 For large or novel craft, the scantlings of the stem will be specially considered, see also Pt 8, Ch 3, 5.11 Forefoot and stem.

3.4 Bottom

3.4.1 The bending moment assumed to be carried by the bottom shell plating is to be not less than that determined from Pt 8, Ch 3, 1.9 Plate and sandwich laminates 1.9.1, using the design pressure from Pt 5, Ch 3, 3.1 Hull structures or Pt 5, Ch 4, 3.1 Hull structures for high speed or displacement type craft as appropriate. This bending moment is to be applied to laminates of both single skin and sandwich construction in the determination of the panel scantling required by Pt 8, Ch 3, 3.4 Bottom 3.4.2 and Pt 8, Ch 3, 3.4 Bottom 3.4.4 respectively.

3.4.2 An estimate of the thickness of bottom single skin plating is to be determined from Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.1. The tensile and compressive stresses are to be determined for each ply of reinforcement in the proposed laminate using Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.3 and Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.4, see also LR's Guidance Notes for Calculation Procedures for Composite Construction. The allowable tensile and compressive stress limits indicated in Table 7.3.1 Limiting stress criteria for local loading are to be complied with.

3.4.3 In no case is the minimum thickness of single skin plating to be taken as less than 5,5 mm.

3.4.4 An estimate of the stiffness E thickness of single skin plating for outer and inner skins of the bottom sandwich panel and the thickness of core material is to be determined from Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.2 and Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.9 respectively. The tensile and compressive stresses are to be determined for each ply of reinforcement in the proposed laminate using Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.7 and Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.8. The allowable tensile and compressive stress limits indicated in Table 7.3.1 Limiting stress criteria for local loading are to be complied with.

3.4.5 The amount of reinforcement in laminates which form the skins of a sandwich laminate is to comply with the requirements of Pt 8, Ch 3, 2.5 Minimum skin reinforcement in sandwich laminates 2.5.1, see Pt 8, Ch 3, 2.3 Sandwich skin laminate 2.3.1.

3.4.6 For all craft types, the minimum bottom shell thickness as required by Pt 8, Ch 3, 3.4 Bottom 3.4.3 and Pt 8, Ch 3, 3.4 Bottom 3.4.5 is to extend to the chine line or 150 mm above the static load waterline, whichever is the greater.

3.4.7 Additionally, for high speed craft, the minimum thickness requirements for the bottom shell between the bilge tangential points or chines and the chine line or 150 mm above the static load waterline, whichever is the greater, is not to be less than determined for the side shell using the side shell impact pressure or the bottom shell hydrostatic or pitching pressures associated with a displacement or semi-displacement type craft whichever is the greater, see Figure 3.3.2 Extent of bottom shell.

Figure 3.3.2 Extent of bottom shell

3.4.8 Special consideration may be given to laminate thicknesses lesser than those required by Pt 8, Ch 3, 3.4 Bottom 3.4.2 and Pt 8, Ch 3, 3.4 Bottom 3.4.4, provided that all of the structural strength requirements of the Rules are complied with, a satisfactory water barrier is provided, see Pt 8, Ch 3, 2.3 Sandwich skin laminate 2.3.1, and the equivalent impact resistance is demonstrated as required by Pt 8, Ch 3, 2.8 Impact considerations 2.8.2.

3.5 Side

3.5.1 The bending moment assumed to be carried by the side shell plating is to be not less than that determined from Pt 8, Ch 3, 1.9 Plate and sandwich laminates 1.9.1, using the design pressure from Pt 5, Ch 3, 3.1 Hull structures or Pt 5, Ch 4, 3.1 Hull structures for non-displacement or displacement craft as appropriate. This bending moment is to be applied to laminates of both single skin and sandwich construction in the determination of the panel scantling required by Pt 8, Ch 3, 3.5 Side 3.5.2 and Pt 8, Ch 3, 3.5 Side 3.5.4 respectively.

3.5.2 An estimate of the thickness of side single skin plating is to be determined from Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.1. The tensile and compressive stresses are to be determined for each ply of reinforcement in the proposed laminate using Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.3 and Pt 8, Ch 3, 1.13 Determination of properties and stresses for single skin plate laminates 1.13.4. The allowable tensile and compressive stress limits indicated in Table 7.3.1 Limiting stress criteria for local loading are to be complied with.

3.5.3 In no case is the minimum thickness of single skin plating to be taken as less than 5 mm.

3.5.4 An estimate of the stiffness E , thickness of single skin plating for outer and inner skins of the side sandwich panel and the thickness of core material is to be determined from Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.2 and Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.9 respectively. The tensile and compressive stresses are to be determined for each ply of reinforcement in the proposed laminate using Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.7 and Pt 8, Ch 3, 1.14 Mechanical properties sandwich laminates 1.14.8. The allowable tensile and compressive stress limits indicated in Table 7.3.1 Limiting stress criteria for local loading are to be complied with.

3.5.5 The amount of reinforcement in laminates that form the skins of a sandwich laminate is to comply with the requirements of Pt 8, Ch 3, 2.5 Minimum skin reinforcement in sandwich laminates 2.5.1.

3.5.6 Special consideration may be given to laminate thicknesses lesser than that required by Pt 8, Ch 3, 3.5 Side 3.5.3 and Pt 8, Ch 3, 3.5 Side 3.5.5, provided that all of the structural strength requirements of the Rules are complied with, a satisfactory water barrier is provided, see Pt 8, Ch 3, 2.3 Sandwich skin laminate 2.3.1, and the equivalent impact resistance is demonstrated as required by Pt 8, Ch 3, 2.8 Impact considerations 2.8.2.

3.6 Sheerstrake

3.6.1 The sheerstrake, is in general, to be taken as the side shell, locally reinforced in way of deck/hull connection and fender attachment. The amount of local reinforcement will be dependent upon the arrangement of structure and the proposed service, but is not to be less than that required by Pt 8, Ch 3, 3.14 Local reinforcement.

3.6.2 The fendering arrangements for all craft types are the responsibility of the designers/Builders and are outside the scope of classification.

3.6.3 Where the pressure or impact loadings that a particular type of craft will experience in service are considered by the Builder, or subsequent Owner, to be not covered by, or be greater than, those indicated in Pt 5 Design and Load Criteria of the Rules, details of the loadings together with the calculations of how these will be satisfactorily distributed into the craft's structure, are to be submitted for consideration with the relevant contruction plans.

3.6.4 The arrangements indicated in Pt 8, Ch 3, 3.6 Sheerstrake 3.6.5, Pt 8, Ch 3, 3.6 Sheerstrake 3.6.6, Pt 8, Ch 3, 4.19 Fenders and reinforcement in way 4.19.5 and Pt 8, Ch 3, 4.19 Fenders and reinforcement in way 4.19.6 for pilot and fishing craft are for the guidance of the Builder and subsequent Owners/operators of the craft. Where the intended service for either of these types of craft, or other types of craft which may be subject to loadings resulting from contact with other craft, jetties or similar loading or boarding facilities, is such that the loadings are greater than those that can be satisfactorily distributed into the craft's structure by the arrangements indicated, the strengthening arrangements are to be increased accordingly.

3.6.5 For pilot craft and other general workboats which may be subject to repeated impact loadings from contact with other craft, etc. the sheerstrake laminate and stiffening arrangements in way are to be increased locally. An increase in laminate weight of not less than 50 per cent of the side shell laminate weight is to be fitted, extending in general from the bow aft over a distance of 0,33L R or 500 mm aft of the point at which the craft reaches its greatest breadth, whichever is the greater, and around the quarters. The additional weight is to extend forward of the quarter and over the transom for a distance of 0,075L R or 1,0 m, whichever is the greater. This reinforcement is in general to extend from the deck edge to below the first longitudinal stiffener, or a vertical distance equivalent to 1/3 the freeboard height, whichever is the greater. The additional laminate weight is then to be tapered out to the side shell laminate weight in accordance with the Rules, see Pt 8, Ch 3, 3.14 Local reinforcement 3.14.2. For increase in stiffening arrangements, see Pt 8, Ch 3, 4.19 Fenders and reinforcement in way. Where the side shell is of sandwich construction then in way of the sheerstrake the two skins of the sandwich are to combine and form a single skin. The weight of this single skin is to be the Rule single skin reinforced in accordance with the above or 1,5 times the total sandwich skin laminate weight whichever is the greater. The arrangement and distribution of this additional laminate between the skins in way of the taper is to be in accordance with Pt 8, Ch 3, 3.2 Keel plate 3.2.4. Where fendering can be considered to act as a chine/spray rail the extent of bottom shell laminate is, in general, to be to above the lower fender.

3.6.6  Fishing craft are, in general, to have their shell laminate as required to satisfy the Rule loadings, increased by 20 per cent. Additionally the side shell is not to be taken as less than the bottom shell weight, and where there are gallows, gantries, nets, or lines etc. the laminate in way is to be further increased locally and/or suitably protected by sheathing in timber, steel or other means. Where the hull is of sandwich construction in way of the sheerstrake the laminate is to combine to form a single skin as indicated in Pt 8, Ch 3, 3.6 Sheerstrake 3.6.2.

3.6.7 Individual consideration will be given to lesser scantlings than those required by Pt 8, Ch 3, 3.6 Sheerstrake 3.6.3 for fishing craft used for pleasure, light duties, etc. Details of the service are to be submitted for appraisal.

3.7 Transom boundary reinforcement

3.7.1 Additional reinforcement is to be moulded into the transom boundary.

3.7.2 For single skin construction, the total weight of reinforcement is to be not less than twice the weight of the adjacent side shell plate laminate, but need not be greater than Rule keel weight as required by Pt 8, Ch 3, 3.2 Keel plate.

3.8 Chine reinforcement

3.8.1 Additional reinforcement is to be moulded into the chine line knuckle boundary, chines and other areas where there is a change of section.

3.8.2 The chine line knuckle is to be reinforced as required by Pt 8, Ch 3, 3.7 Transom boundary reinforcement for the transom boundary.

3.8.3 Chine details are to be such that the continuity of structural strength across the panel is maintained. Details of all chines are to submitted for consideration, see also LR's Guidance Notes for Structural Details.

3.9 Skeg

3.9.1 The thickness of the skeg plating is, in general, to be not less than the thickness of the keel at bottom or 1,5 times the thickness of the bottom shell on the sides, whichever is the greater, see also Pt 8, Ch 3, 5.10 Skeg construction.

3.10 Shell openings

3.10.1 Openings are to have smooth edges and well rounded corners. Exposed edges in way of cut-outs in single skin/plate laminate are, in general, to be suitably sealed over laminating with not less than 2 x 450 g/m2 CSM (or equivalent) reinforcements. Alternative arrangements demonstrating the equivalent protection to the ingress of moisture into the laminate will be individually considered in association provided on the relevant plans.

3.10.2 The exposed edges of all openings cut in sandwich panels are to be suitably sealed. In general a high density foam core (or equivalent material) is to be used around the perimeter of such openings. Exposed edges in way of cut-outs in sandwich panels are to be overlaminated with a weight of laminate not less than that required for the outer skin of the sandwich panel.

3.10.3 Where other than an epoxy resin system is used the first layer of reinforcement, as required by Pt 8, Ch 3, 3.10 Shell openings 3.10.1 and Pt 8, Ch 3, 3.10 Shell openings 3.10.2, is, in general, to be CSM with a weight not exceeding 300 g/m2.

3.10.4 Sea inlet boxes are to have well rounded corners and, so far as possible are to be kept clear of the bilge radius. Arrangements are to be made to maintain the continuity of structural strength in way of the openings.

3.11 Appendages

3.11.1 The scantlings of appendages will be subject to special consideration on the basis of the Rules and the design loadings anticipated, but are in no case to be taken as less than that of the surrounding structure.

3.12 Fin and tuck

3.12.1 Additional reinforcement is to be moulded into the fin and tuck areas of yachts which have either internal fixed ballast or external attached ballast keels, see also Pt 16 Control and Electrical Engineering.

3.12.2 For single skin construction the total weight of reinforcement is not to be less than 1,50 times the weight of the adjacent bottom shell plate laminate, but need not be greater than the Rule keel weight as required by Pt 8, Ch 3, 3.2 Keel plate.

3.13 Transom

3.13.1 The thickness of the stern or transom is to be not less than that required by Pt 8, Ch 3, 3.4 Bottom and Pt 8, Ch 3, 3.5 Side as appropriate. Where water jet or sterndrive units are fitted, the scantlings of the plating in way of the nozzles and connections will be specially considered.

3.14 Local reinforcement

3.14.1 The hull and deck are to be locally increased in thickness in way of fittings for rudder tubes, propeller brackets, passenger routes, vehicle lanes, etc. The amount of increase is to be not less than 50 per cent of the adjacent plate laminate. Details of such reinforcement are to be submitted.

3.14.2 Local reinforcement is in general to extend under the adjacent supporting structure and then be tapered gradually to the base laminate thickness over a distance of not less than 20 times the difference in thickness, see Figure 3.3.3 Arrangement of local reinforcement.

Figure 3.3.3 Arrangement of local reinforcement

3.14.3 The amount of material laid ‘wet on wet’ is to be limited to avoid excessive heat generation.

3.15 Hull laminate arrangement

3.15.1 The hulls of all craft with a service speed of 25 knots or greater are to be moulded, such that following local impact, damage progressive stripping of surface reinforcements will not occur. This may be achieved by arranging all hull reinforcements as shown in Figure 3.3.4 Arrangement of hull reinforcement.

Figure 3.3.4 Arrangement of hull reinforcement

3.15.2 Details of the laminate sequence and direction of orientation are to be indicated in the laminate schedule as required by Pt 8, Ch 2, 3.3 Laminating 3.3.7.

3.15.3 It is recommended that woven reinforcements be laid transversely to minimise the susceptibility to progressive stripping of hull laminates following local impact.

3.15.4 Special consideration is to be given to hull laminates where high glass content is proposed and where orthophthalic resins are used.

3.16 Novel features

3.16.1 Where the Rules do not specifically define the requirements for novel features then the scantlings and arrangements are to be determined by direct calculations. Such calculations are to be carried out on the basis of the Rules, recognised standards and good practice, and are to be submitted for appraisal.


Copyright 2022 Clasifications Register Group Limited, International Maritime Organization, International Labour Organization or Maritime and Coastguard Agency. All rights reserved. Clasifications Register Group Limited, its affiliates and subsidiaries and their respective officers, employees or agents are, individually and collectively, referred to in this clause as 'Clasifications Register'. Clasifications Register assumes no responsibility and shall not be liable to any person for any loss, damage or expense caused by reliance on the information or advice in this document or howsoever provided, unless that person has signed a contract with the relevant Clasifications Register entity for the provision of this information or advice and in that case any responsibility or liability is exclusively on the terms and conditions set out in that contract.