Pt B, Ch 12, Sec 1<strong>SECTION</strong> 1GENERAL REQUIREMENTS1 General1.1 Application1.1.1 The characteristics of composite materials to be usedin the construction of yachts within scope of Bureau Veritasclassification are to comply with the present Chapter.1.2 General1.2.1 The composite’s characteristics are directly dependingon:• type of resin• type of fibre• type of reinforcement fabric• type of hull’s manufacturing process.All these particulars are taken into account in this Chapter:• to characterize composite materials from a mechanicalpoint of view• to define the Bureau Veritas survey and inspectionrequested for granting the construction marks { or µ andfor classing the yacht.1.2.2 The following steps are to be examined within thescope of the classification of a composite yacht, from astructural point of view:• Raw materials: homologation or equivalent process togrant the construction marks as defined in Ch 12, Sec 2,[6]• Theoretical characterization of laminates as defined in Ch12, Sec 3 (individual layer) and Ch 12, Sec 4 (laminate)• Mechanical sample tests representative of the hull’sstructure to compare with theoretical analysis as definedin Ch 12, Sec 5, [4]• Structure drawings examination, as defined in Ch 1, Sec 3• Preliminary survey of the yard and survey at work asdefined in Ch 12, Sec 5, [2] and Ch 12, Sec 5, [3].1.2.3 The composite materials considered in this presentchapter are basically those made from:• Thermoset resin’s systems• Glass, carbon or para-aramid based reinforcement fabrics• Manufacturing processes as lay-ups (spray and hand) orvacuums (infusion) or pre-pregs.Composite materials made of other resin’s systems, fibres ormanufacturing processes may be accepted provided theirspecifications are submitted to the Society for approval.2 Documents to be submitted2.1 General2.1.1 As a rule, the drawings and documents to be submittedfor examination are listed in Ch 1, Sec 3, Tab 1.2.2 Laminate2.2.1 Following information are to be given on drawings:• arrangement of laminate for the various structural elements:thickness, definition of the successive layers ofreinforcement, mass per square meter in layers of reinforcement,proportion in mass of reinforcement of eachlayer, directions of roving layers and unidirectional reinforcements,decreasing in thicknesses between layers• direction of laminate in relation with ship structure• structure of oil tanks or other liquid tanks which areintegrated to the hull• details of connection between various structural elementsand details of attachments to the hull of reinforcingsupplementary elements• pillars.2.3 Individual layer2.3.1 However, the technical specifications of supplierswith indication of types, trademarks and references of theresins and gel-coats, reinforcements, and core materials areto be supplied.These specifications have to give the following information:• for resins: system (polyester, vinylester or epoxy), density,Young modulus, shear modulus, Poisson coefficient,breaking strength and elongation at break• for reinforcements (unidirectional reinforcements,woven rovings, chopped strand mats): quality (fibre’stype, density with breaking strength of the elementaryfibre, Young modulus and Poisson coefficient, in fibredirection and normal to fibre direction), mass per squaremeter, thickness and eventually weft-warp distribution• for core materials: type and quality, density, tensile,compression and shear strength and elasticity moduli.July 2006 with February 2008 Amendments Bureau Veritas Rules for Yachts 275
Pt B, Ch 12, Sec 2<strong>SECTION</strong> 2RAW MATERIALS1 General1.1 Application2 Resin systems2.1 General1.1.1 The mechanical characteristics of composite materialsdepend on raw materials’ characteristics.1.1.2 The present section gives general ”state of the art”information about raw materials.1.2 Definitions1.2.1 The present chapter describes the main raw materialsused in composite boat building.The raw materials, used in boat building, are of four maintypes: resin systems, reinforcements, core materials, adhesives.1.2.2 Resin systemsAlso named matrix, resin systems are thermoset resins (initialliquid, hard and stiff cross linked material that does notreturn liquid when cured). Resin is used to:• link reinforcements together• protect them from impact, moisture and abrasion• spread loads through reinforcements’ layers.Resin systems dealt with in this Chapter are polyester,vinylester and epoxy systems.1.2.3 ReinforcementsReinforcement fabrics are used to improve mechanicalcharacteristics of composite materials.Reinforcement fabrics may be constructed with interlacedyarns or without interlacing, named respectively woven rovingsand stitched rovings.Reinforcement fabrics dealt in this chapter are made of continuousyarns, manufactured with glass, carbon or para-aramidfibres.1.2.4 Core materialsCore materials are used in composite sandwich structures toimprove global moment of inertia of the whole laminate.Sandwich structures are made of two reinforced faces alsonamed skins, separated by and jointed to a core.Core materials dealt with in this chapter are syntheticfoams, natural cores and honeycombs.1.2.5 AdhesivesAdhesive materials are generally considered as resin systems,and are used to bond together different compositestructures or to bond skins to core in sandwich structures.2.1.1 Manufacturing and curing processAs a general rule, thermoset resin systems used in shipbuildingare obtained from a synthetic resin, also namedpolymer, made of long unsaturated chains of molecules.The process, which allows to modify the arrangement ofmolecular chains from free independent chains to a threedimensional linked chains network, is called polymerisationor curing process.This chemical reaction is observed where resin goes from itsliquid state to its solid state. This reaction is accompaniedby a heat discharge and is irreversible for thermoset resins.The three dimensional network is obtained by different curingprocesses, according to the type of synthetic resin:• for polyester and vinylester: by mixing synthetic resin withan unsaturated monomer (e.g. styrene) which creates thechemical links. In this case, the chemical reaction needs acatalyst to start the polymerisation process• for epoxy: by adding a hardener which promotes thepolymerisation process. In this case, macromolecularchains are directly linked to each other.These two different chemical processes have an importanteffect on mechanical characteristics of the final resin systemand particularly on the volumetric shrinkage during thepolymerisation (source of stress concentration in the finalcomposite between resin and fibre).2.1.2 Glass Transition Temperature (Tg)Glass Transition Temperature (Tg): the state of polymerisationmay be appraised by measuring the Tg. This is theapproximate temperature at which number of chemicallinks between molecular chains is significant to changemechanical properties of a cured resin.The more polymerized is the resin, which means the greateris the number of chemical links between macromolecularchains, higher is the value of Tg.Where Tg is measured, it is necessary to indicate the referenceof the test method, taking into account that the measuredvalue of Tg may vary from one method to another.For epoxy resin systems in particular, Tg may be increasedafter the resin polymerisation by a post cure with an additionalrise of temperature.276 Bureau Veritas Rules for Yachts July 2006 with February 2008 Amendments
- Page 1 and 2: A-PDF Merger DEMO : Purchase from w
- Page 3 and 4: Pt A, Ch 1, Sec 3SECTION 3SURVEYS1
- Page 5 and 6: Pt A, Ch 1, Sec 5SECTION 5INTERVENT
- Page 7 and 8: Pt A, Ch 2, Sec 1SECTION 1DEFINITIO
- Page 9 and 10: Pt A, Ch 2, Sec 2Table 3 : Charter
- Page 11 and 12: Pt B, Ch 1, Sec 1SECTION 1APPLICATI
- Page 13 and 14: Pt B, Ch 1, Sec 2SECTION 2SYMBOLS A
- Page 15 and 16: Pt B, Ch 1, Sec 4SECTION 4CALCULATI
- Page 17 and 18: Pt B, Ch 10, Sec 5SECTION 5INDEPEND
- Page 19: Pt B, Ch 11, Sec 1SECTION 1GENERAL
- Page 23 and 24: Pt B, Ch 12, Sec 2The chemical netw
- Page 25 and 26: Pt B, Ch 12, Sec 2This Carbon may u
- Page 27 and 28: Pt B, Ch 12, Sec 23.4 Homologation
- Page 29 and 30: Pt B, Ch 12, Sec 2Table 4 : BalsaVo
- Page 31 and 32: Pt B, Ch 12, Sec 2Table 6 : Meta-ar
- Page 33 and 34: Pt B, Ch 12, Sec 3SECTION 3INDIVIDU
- Page 35 and 36: Pt B, Ch 12, Sec 3Table 1 : Resin /
- Page 37 and 38: Pt B, Ch 12, Sec 3Table 4 : Element
- Page 39 and 40: Pt B, Ch 3, Sec 1c) Lightweight che
- Page 41 and 42: Pt B, Ch 3, Sec 2Figure 1 : Severe
- Page 43 and 44: Pt B, Ch 3, Sec 2where:F : Wind for
- Page 45 and 46: Pt B, Ch 3, App 2APPENDIX 2TRIM AND
- Page 47 and 48: Pt B, Ch 4, Sec 2SECTION 2DESIGN LO
- Page 49 and 50: Pt B, Ch 6, Sec 3SECTION 3SPECIFIC
- Page 51 and 52: Pt B, Ch 6, Sec 3Figure 2 : Rig loa
- Page 53 and 54: Pt B, Ch 7, Sec 1SECTION 1 HYDRODYN
- Page 55 and 56: Pt B, Ch 7, Sec 1Figure 4 : Load ar
- Page 57 and 58: Pt B, Ch 7, Sec 1• for monohull -
- Page 59 and 60: Pt B, Ch 7, Sec 2SECTION 2BOTTOM SL
- Page 61 and 62: Pt B, Ch 9, Sec 1SECTION 1GENERAL1
- Page 63 and 64: Pt C, Ch 1, Sec 1Table 1 : Inclinat
- Page 65: Pt C, Ch 1, Sec 13.4 Safety devices