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    I. Phases of composite materials types and functions

    ALENA SIKOVTECHNICAL UNIVERSITY OF KOICECIVIL ENGINEERING FACULTYDEPARTMENT OF MATERIAL ENGINEERING

    LLP ERASMUS - IP 2012, PRAGUE

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    Definition of the composite material

    A multiphasematerial formed from a

    combination of materials which differ incomposition or form, remain bonded together,

    and retain their identities and properties.

    Composites maintain an interface betweencomponents and act in concert to provide

    improved specific or synergistic

    characteristicsnot obtainable by any of the original components

    acting alone

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    Synergistic effect

    QK = Q(A) + Q(B) + Q(C) + Q(A) . Q(B) . Q(C)sum effect synergistic effect

    where: QK; Q(A); Q(B); Q(C) quality of composite / components A, B, C contain of components

    Synergistic effect is one of the objectivecharacteristics differentiating the compositematerials from the other ones

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    Phases of a composite material

    Phaseis:

    a region ofmatter thatpossesses uniform

    intensivepropertiesthroughout itsvolume

    a homogeneousarea of compositematerial

    Discontinuous phase (stiffer andstronger) - filler/reinforcement,

    Continuous phase (less stiff andweaker) - binder/matrix

    Interphase between matrix andreinforcement

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    surrounds and supports otherconstituents by keepingtheirrelative positions and holding themtogether,

    protectsboth the reinforcementand whole the composite fromenvironment effects/deterioration;

    transfersthe loading toreinforcement

    protectsthe filler from abrasion (witheach other)

    enhancessome of the properties ofthe resulting material (that filler aloneis not able to impart). Theseproperties are such as: transverse strength of a lamina impact resistance

    providesbetter finish to final product

    imparts special properties,such as electrical andmechanical, to improve thematrix properties,

    provides some stiffeningandstrenghteningof the material,

    provides control of cracksriseand development

    MatrixMatrix FillerFiller

    Roles of phases

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    Systems of composite materials based

    on ratio of individual phases

    matrix

    1st limiting system

    Vc = Vm

    matrixfiller

    Composite of I. type

    Vc = Vm + VfFiller is dispersed

    Vfcan increase at the cost of Vm

    up to maximal possible fillig of volume

    2 nd limiting system

    Vc = Vm + VfClosest packing of volume by filler

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    Composite of II. type

    Vc= V

    f+ V

    m+ V

    v

    Changing the ratio of phases ispossible only by reduction of matrixand incorporation of voids instead

    Discrete voids

    Composite of III. type

    Vc = Vf+ Vm + Vv

    Volume of voids increases, voids startto be continuous

    3 rd limiting system

    Vc = Vv + Vf

    Without matrix

    Composite is incoherent, loose

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    Parameters influencing resulting properties of

    a composite material

    Volume (or weight) fraction of phases Shape, geometry, and distribution of the phases Orientation of filler/reinforcement in system

    (isothropy/anisothropy) Individual properties of phases, compatibility of

    components Bonding strength/ITZ (interfacial transition zone)

    properties on the interface between the dispersed phaseand matrix

    Interaction of composite and ambient environment Age of composite components Production technology

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    Filler/reinforcement

    Forms: Particles Flakes Fibers

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    Filler/reinforcement - Orientation Isotropic

    Having uniform properties in

    all directions. The measuredproperties of an isotropicmaterial are independent ofthe axis of testing.

    AnisotropicNot isotropic; having

    mechanical and/or physicalproperties which vary withdirection relative to naturalreference axes inherent inthe material

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    Classification of composite materialsbased on the form and orientation of

    filler/reinforcement

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    Filler/reinforcement - Particles

    They usually reinforce a composite equally in all

    directions. Particle fillers are usually of very small dimension(0,01 0,1 m) and they occupy app. 15% ofcomposite volume they are dispersed without mutualconnection

    Typical particles in the terms of constructioncomposite materials are of bigger dimensions(granularity), such as sand and gravel

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    Usual materials of particle fillers Natural rocks: granit, feldspar, silica, limestone,

    gypsum, kaoline ... Glass microspheres, milled glass

    Metal particles Ceramic particles

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    Filler/reinforcement - Fibers

    Natural Fibres:

    Animal fibres: Silk, Wool, Spider silk, Sinew, Camelhair Vegetable fibres: Cotton, Jute, Bamboo, Sisal, Maze,

    Hemp, Sugarcane, Banana, Ramie, Kapok, Coir,

    Abaca, Kenaf, Flax, Raffia palmProcessed Fibres: Mineral fibres: Asbestos, Basalt, Glass Metal fibers: steel Polymer fibers: PE, PP, PVA ...

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    Advanced fibres: fibres possessing high specific

    strength [/]) Glass Carbon

    Organic: aramid, kevlar Ceramic: borone, silicone

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    Filler/reinforcement - Fibers

    Performance properties of fibers

    High tensile strength

    Specific modulus of elasticity Stability in actual matrix Shape

    Surface treatment End treatment/shape Lenght and diameter aspect ratio (large aspect ratios

    result in stronger composites, but they are more difficultto process)

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    Filler/reinforcement - Fibers

    Forms of Fibrous CompositesSingle-layered composites: continious (Layer, Lamina, Ply - any of the term is used)

    unidirectional bi-directional

    discontinuous

    random orientation preferred orientation

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    Multi-layered composites:

    Laminates

    Hybrides

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    Filler/reinforcement - Fibers

    Kinds of fibersSteel

    The usual way of application is as short fibers torandom reinforcement of concrete they are made of cold drawn steel wire with low

    content of carbon various shapes and endings (hooked, undulated or

    flat) are produced in order to obtain correct anchoragein concrete

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    Polypropylene

    They are produced in two types: as fibrillated ones(bundles of several fibers) cut from a sheet; or

    monofilaments cut from a yarn

    Monofilaments Fibrillated fibers

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    Glass

    manufactured frommolten glass, fromwhich glassmonofilaments aredrawn and thengathered to strands.The strands are usedfor preparation ofdifferent glass fiber

    products (yarns,rovings, wovenfabrics, mats)

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    Carbon

    They are commonly produced by the pyrolysis ofhydrocarbon precursors in a non-reactive atmosphere carbon fibers offer high strength, high stiffness, low

    density, and low thermal expansion not achievable withany other structural fibers.

    In addition, carbon fibers have high thermal and electricalconductivity which make them suitable for specialized

    applications where thermal energy and electrical currentneed to be specifically controlled

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    Carbon fibers allow to produce a composites withexcellent strength and stiffness and reduced weight

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    The role of fibres in cementitious materials is

    that they generally have two positive effects:

    reduction of shrinkage strainsin early age of

    concrete, when high risk of shrinkage cracks formationcomes fibers with lower modulus of elasticityaresufficient

    carrying the stressescaused by external loads fibers with higher modulus of elasticityarerequired

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    Filler/reinforcement - Fibers

    Properties of selected types

    TypeDiameter

    [mm]

    Density

    [g/cm3]

    Tensilestrength

    [GPa]

    Modulus

    of

    elasticity

    [GPa]

    Ultimateelongation

    [%]

    Steel 0,1 - 1,0 7,8 0,3 - 2,0 200 0,5 - 3,5

    Polypropylene 0,02 - 0,4 0,9 0,3 - 0,5 5 15 - 25

    Glass 0,05 - 0,15 2,5 1,0 - 3,0 70 - 80 1,5 - 4,5

    Carbon 0,008 - 0,01 1,9 1,0 - 3,0 230 - 400 0,5 - 1,0

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    Matrix

    The primary consideration in the selection of a matrix isits basic mechanical properties. For high-performancecomposites, the most desirable mechanical propertiesof a matrix are:

    High modulus of elasticity, which influences the

    compressive strength of the composite High tensile strength, which controls the intraply

    cracking in a composite laminate

    High fracture toughness, which controls plydelamination and crack growth

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    Matrix Usual materials

    Plastics

    Metals Ceramics

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    Matrix Usual materials - Plastics

    Thermoplastics:

    polypropylene, polyvinyl chloride (PVC), nylon,

    polyurethane, poly-ether-ether ketone (PEEK), polyphenylene sulfide (PPS),

    polysulpone

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    Matrix Usual materials - Plastics

    Thermoplastics are increasingly used over thermosetsbecuase of the following reasons:

    Processing is faster than thermoset composites sinceno curing reaction is required. Thermoplasticcomposites require only heating, shaping and cooling.

    Better properties: high toughness (delamination resistance) and

    damage tolerance, low moisture absorption chemical resistance

    They have low toxity Cost is high

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    Matrix Usual materials - Plastics

    Thermosets:

    polyesters epoxies polyimides

    other resins

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    Matrix Usual materials - Plastics

    Properties of selected typesEpoxy Polyester Phenolic Polyamid

    Modulus of elasticity

    Em (MPa)4 500 4 000 3 000

    4 000 -

    19000Shear modulus of

    elasticity Gm

    (MPa)

    1 600 1 400 1 100 1 100

    Tensile strengthpm (MPa)

    130 80 70 70

    Density

    (kg.m-3)1 200 1 200 1 300 1 400

    Maximaltemperature

    Tmax (oC)

    90 -200 60 - 100 120 - 200 250 - 300

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    Matrix Usual materials - Metals

    Aluminum Titanium Copper

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    Matrix Usual materials - Ceramics

    Carbon Silicon carbide Silicon nitride

    Lime, gypsum, cement

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    Phase boundary - interfacial transition zone

    Thin region in which the intensive properties change

    discontinuously. Usually the properties of boundaryare worseas those of separate phases. At all kinds of composites there is a critical area, with

    the highest probability of cracks and failure all ofcomposite. It is the weakest area of compositematerial

    Good bonding(adhesion) between matrix phase and

    dispersed phase provides better transfer of load

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    Character of ITZ is influenced and can beoptimized by:

    physical properties of particles/fibers (specificsurface area, surface coarseness, porosity, ),

    chemical processes - reaction between matrix andfiller

    technological processes: mixing, compacting,forming, curing of composite

    I t f i l t iti

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    Interfacial transition zone

    Ways of modificationIn cementitious CM1.Through aggregate quality: optimal grading (means grading with

    minimal void ratio. It can be reached usingaggregates of various grain size)

    surface area - minimal shape - regular surface - coarse

    2. Through matrix quality:

    porosity, cracks and hydratation productscontrol due to minimal water/cement ratioand additive fine-grain materials(granulated blast furnace slag, fly ash,microsilica)

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    Role of mineral fine-grain materials:

    improvement in packing, that is, action as a filler withmuch more smaller particles than cement particles

    better adhesion of matrix

    aggregate

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    In polymer CM:

    aggregate must be of good quality, free of dust andother debris, and dry.

    failure of these criteria can reduce the bond strengthbetween the polymer binder and the aggregate. bonding can be improved by some special chemical

    admixtures

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    LITERATURE: LEE, S. M. Preface to the Dictionary of Composite Materials Technology.

    http://composite.about.com/od/referencematerials/l/blpreface.htm MORVA, T. Composite Building Materials. http://ezinearticles.com/?Composite-Building-

    Materials&id=353965 CAMPBELL, F.C. Structural Composite Materials. Chap. 1: Introduction to Composite Materials.

    2010. http://www.asminternational.org/content/ASM/StoreFiles/05287G_Sample_Chapter.pdf http://www.ewp.rpi.edu/hartford/~taurim/EP/Report%20Material/Resources/frc_chap_2.pdf ISHAI, O. Engineering Mechanics of Composite Materials.

    http://www.globalspec.com/reference/60655/203279/chapter-1-introduction BARE, R. Composite materials. In Czech. SNTL. Praha 1988.

    AGARWAL, B., BROUTMAN, L. Fiber composites. In Czech. SNTL. Praha 1987 KOPELIOVICH, D. Structure of Composites.

    http://www.substech.com/dokuwiki/doku.php?id=structure_of_composites&DokuWiki=9cf99564549611b3ac3e32e5e472e368

    LA, V.: Mechanika kompozitnch materil, 2006. In:http://www.kme.zcu.cz/download/predmety/mkm/1-uvod.ppt

    SCRIVENER, K. at al. he Interfacial Transition Zone (ITZ) Between Cement Paste and Aggregate inConcrete. In Chemistry and Materials Science. Interface Science. Vol. 12, N. 4, 411-421, DOI:10.1023/B:INTS.0000042339.92990.4c

    TREFIL, V. Influence of microsilica and nanosilica on the hardened concrete properties. In Czech.http://www.stavebnitechnologie.cz/view.php?cisloclanku=2002032802

    What are composites?http://www.composites.ugent.be/home_made_composites/what_are_composites.html

    MOHITE, PM: Composite Materials. In: http://home.iitk.ac.in/~mohite/Composite_introduction.pdf