hybridisation of composite

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Hybridisation of self-reinforced composites: modeling and verifying a new hybrid concept 1. Introduction A common problem of composites is their brittleness. This is mainly due to the brittle nature of the fibres and the low off-axis strength of impregnated bundels or laminates. A commonly applied solution for this problem is toughnening the matrix, but this solution has its limitations. In the seventies an unexpected alternative popped up. Capiati et al. combined highly-oriented polyethylene (PE) fibres with an un- oriented polyethylene matrix in the search for low density and easy-to-recycle composites. A new class of composite materials was born, namely self-reinforced composites (SRC's). SRC's combine a low density with an exceptional toughness. The most promising SRC up to now is self- reinforced polypropylene (SRPP). This gives an extremely high tougness (notched Izod impact > 4750 J/m at 20°C). On top of that it is one of the few materials which shows a increasing tougness at lower temperatures (7000 J/m at -40°C). The biggest limitation for widespread application of this promising material is the low stiffness (3-5 GPa). In order to exploit the exceptional properties of SRPP, we will hybridise the SRPP to increase the stiffness. In the present case, hybridizing means combining two fibers. On one hand, there's the drawn PP fibre with a stiffness of 10-15 GPa, a strength of 450 MPa and a failure strain of 15-20%. On the other hand we will use different fibres which have a stiffness ranging from 30 tot 230 GPa and a failure strain smaller than 3%. These hybrid SRC's will allow us to break through the toughness-stiffness dilemma (see figure below). 2. The hybrid effect When combining two fibres synergistic effects can appear. This is called the hybrid effect and is simply a deviation from simple rules-of-mixture. For stiffness, we can expect a linear rule-of-mixture to be

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  • Hybridisation of self-reinforced composites: modeling and verifying a new hybrid concept

    1. Introduction

    A common problem of composites is their brittleness. This is mainly due to the brittle nature of the fibres

    and the low off-axis strength of impregnated bundels or laminates. A commonly applied solution for this

    problem is toughnening the matrix, but this solution has its limitations. In the seventies an unexpected

    alternative popped up. Capiati et al. combined highly-oriented polyethylene (PE) fibres with an un-

    oriented polyethylene matrix in the search for low density and easy-to-recycle composites. A new class

    of composite materials was born, namely self-reinforced composites (SRC's).

    SRC's combine a low density with an exceptional toughness. The most promising SRC up to now is self-

    reinforced polypropylene (SRPP). This gives an extremely high tougness (notched Izod impact > 4750

    J/m at 20C). On top of that it is one of the few materials which shows a increasing tougness at lower

    temperatures (7000 J/m at -40C). The biggest limitation for widespread application of this promising

    material is the low stiffness (3-5 GPa). In order to exploit the exceptional properties of SRPP, we will

    hybridise the SRPP to increase the stiffness. In the present case, hybridizing means combining two

    fibers. On one hand, there's the drawn PP fibre with a stiffness of 10-15 GPa, a strength of 450 MPa and

    a failure strain of 15-20%. On the other hand we will use different fibres which have a stiffness ranging

    from 30 tot 230 GPa and a failure strain smaller than 3%. These hybrid SRC's will allow us to break

    through the toughness-stiffness dilemma (see figure below).

    2. The hybrid effect

    When combining two fibres synergistic effects can appear. This is called the hybrid effect and is simply a

    deviation from simple rules-of-mixture. For stiffness, we can expect a linear rule-of-mixture to be

  • appropriate, but for other properties, like strength, toughness and failure strain, this isn't always the case.

    This hybrid effect has been thoroughly examined in the '70's and 80's for carbon-glass and for carbon-

    aramid hybrids. It was explained as a combination of influence of the fracture propagation and process-

    induced shrinkage.

    a) Fracture propagation

    Fracture of unidirectional impregnated composites is a statistical phenomenon. This is because the fibers

    do not possess a unique strength, they follow a certain distribution. Most often, this is a Weibull

    distribution. At a certain stress level, the weakest fiber will break and locally lose its load transfer

    capability. At the fracture location, the matrix is loaded in shear and this ensures the longitudinal fibre

    stress in the broken fiber recovers over a certain length. The load, which was initially carried by the now

    broken fiber, is transferred to the surrounding fibers. Therefore, the surrounding fibers are subjected to

    stress concentrations. The odds that one of the surrounding fibers is loaded to its maximal strength thus

    increases. More and more fibers will break when the composite is increasingly loaded. This finally leads

    to failure of the entire composite.

  • Of course, adding a second, ductile fiber will greatly influence this. The stress concentrations will depend

    on the kind of neighbouring fiber. On top of that, less brittle fibers will be present. This is simply because

    the odds of having weak, brittle fibers in the composite decrease when less brittle fibers are present. To

    conclude, the odds that a crack can propagate will most likely decrease when a second, ductile fiber is

    added.

    b) Process-induced shrinkage

    An important difference with the classical hybrid effect lies in the shrinkage. When a stretched polymer

    fiber is heated, it will have the tendency to shrink. The shrinkage is irreversible and can be very large, up

    to 80% for stretched PP. The presence of the brittle fibers will restrain this shrinkage. Therefore the

    polymer fiber will have residual tensile stress. However, this only has a minor influence on the failure of

    the hybrid composite. Much more important is the residual compressive stress in the brittle fibers. This

    compressive stress will counteract the applied tensile stresses and thus increase the apparant tensile

    strain. Because the polymer fibre is taken very close to its melting temperature, the yield stress is very

    low and most of the stresses will relaxes. According to previous experiments, this shrinkage stress is on

    the order of magnitude of 10 MPa.

    Compared to classical hybrids however, the difference in coefficients of thermal expansion (CTE) is a lot

    bigger. Compacted PP tape typically has a CTE of 40-70.10-6 K

    -1. Classical fibres have CTE's which are

    a lot lower:

    -glass: 5.10-6

    K-1

  • -carbon: -0,5 - 0.5.10-6

    K-1

    -aramid: -1 .10-6

    K-1

    Thus the thermal stresses build up in hybrid SRC's is a lot bigger than in classical hybrids. However, it

    can also lead to curved samples or buckled fibers. Therefore, the shrinkage has to be controlled very

    carefully.

    3. Research strategy

    a) Unidirectional composites

    At first, we will investigate unidirectional (UD) composites. These composites can be modelled more

    easily than multidirectional composites. There are basically two different hybridisation routes. The first

    one is intrayarn (shown below).

    The second hybridisation routes is obtained by stacking different non-hybrid layers on top of each other.

    This is shown below.

    The important parameters to be examined are:

    Parameter Invloed

    Degree of dispersion Better dispersion increases the hybrid effect

    Stiffness of hybridisation

    fiber

    Influences the stress concentrations and buckling of

    individual fibres

  • Parameter Invloed

    Volume fraction of

    hybridization fiber Influences the hybrid effect and buckling

    Volumefraction of matrix Thermal conductivity and heat capacity influence

    the amount of molten polymer fiber

    Stiffness of matrix Higher matrix stiffness gives less buckling

    Yield stress of matrix Higher yield stress gives better load transfer and

    increases strength

    Matrix-fiber interphase Stronger interfase increases load-sharing and leads

    to bigger hybrid effect

    b) Multidirectional composites

    Based on intrayarn and interlayer hybrids, it's possible to make multidirectional composites. However,

    there is a third possibility to make hybrids, namely intralayer or co-weaving.

    Most polymer composites contain fibers in at least two different directions. That's why it's useful to set up

    models for multidirectional composites. These models can be split up in to three parts:

    - Damage initiation in transverse layers

    - Damage propagation in transverse layers

    - Breaking of longitudinal layers

    The first two parts will be modelled using previously developed models of the CMG. For the last part, we

    can use the results from our unidirectional model.

  • 4. Conclusion

    Hybrid SRC's have a huge potential, but a lot of its features are currently unknown. This research will

    help us understand the fundamentals of its behaviour and help us optimise their properties. In the end,

    we will be able to develop better hybrid SRC's in a rational, scientific way. On top of that, the developed

    models are generic and also applicable on classical hybrids.

    3. Review of Literature: .

    Acharya and Samantarai (2012) investigated the tribo potential of biomass

    based carbon black filler in epoxy composite. They observed that incorporation of

    Rice Husk Char in to epoxy significantly reduce abrasive wear loss.

    Ndazi et al. (2007) studied chemical and physical modifications of rice husk

    for use as composites panels. They found that chemical modification of rice husks by

    NaOH improves the adhesion properties of rice husk in composites due to removal of

    surface impurities such as silica and carboxylic compounds, which blocks reactive

    chemical groups.

    Studies are also available on aluminium reinforced by silicon carbide

    from rice husk. The reports based on these studies says that the reinforced aluminium

    not only has a good combination of room temperature specific strength and modulus

    and excellent thermal stability, but it also can be processed by normal metal working

    technique. Such materials are increasingly considered for aerospace applications

    where high stiffness and strength to weight ratios are additional advantages.

    The applications of Rice Husk Ash (RHA) as a filler in plastics is

    relatively limited mainly due to polypropylene (PP). As reported for a PP composites

    30, with an increase in the RHA loading, its flexural modulus and density increases,

    where as its tensile strength, breaking elongation and impact strength decreases, yet

    RHA still can replace some commercial fillers.

    Navinchand et al. (1987) reported the studies on polyester filled with RHA.

    They have mentioned in their study reports that both the tensile and impact strength of

    the resulting composites were decreased with the increase in filler loading. they have

  • also reported that in addition to being used in rubbers or plastics, RHA can also be

    used as a filler in rubber/plastic blends.

    Rozman H. D. et al. (2000) had made their studies on the effect of chemical

    modification of rice husk. They found and reported that with chemical modification in

    the rice husk, the reinforcing effect can be increased to an acceptable limit.

    Silvia Luciana Favaro et al. (2010) studied the chemical, morphological and

    mechanical analysis of rice husk/post-consumer polyethylene (PE) composites. PE and

    rice husk were chemically modified to improve their compatibility in composite

    preparation. They found improved fibre surface adhesion with matrix and improved

    mechanical performance compared to pure polymer matrix, on the other hand no

    benefit is observed in the tensile strength over the pure PE.

    Garcia et al. (2007) used a combination of waste tire rubber and rice husk with

    different size particles as raw materials in their research for obtaining new materials by

    sintering technique so that environmental problems could be reduced.

    Ayswarya et al. (2012) studied the use of RHA for property modification on

    high density polyethylene (HDPE). They found and reported that RHA is a valuable

    reinforcing material for HDPE and the environmental pollution arising due to RHA

    can also be eliminated.

    Rout and Satpathy (2012) studied mechanical and tribo-performance of rice-

    husk filled glass-epoxy hybrid composites. They found that hardness, tensile modulus

    and impact energy of these new class hybrid composites are enhanced with the rice

    husk as filler additive whereas a steady decline of tensile and flexural properties are

    also observed.

    Bohlooli et al. (2012) analytically investigated the compressive strength of

    geopolymers with seeded fly ash and rice husk bark ash by fuzzy logic modelling.

    They found that fuzzy logic can be an alternative approach for evaluating the effect of

    seeded mixture of fly ash and rice husk bark ash on compressive strength values of

    geopolymer specimens.

  • Kwon et al. (2013) investigated the flexural properties and dimensional

    stability of the sandwich-structured composites comprising the rice husk particles in

    the core layer and randomly aligned the wood strands in the face layers. They found

    that 1040% of the strands into the face layers of the RH particleboards improved the

    flexural modulus and strength.

    Ahmad et al. (2012)were performed their research on using of rice husk

    powder as reinforcing filler in blends of natural rubber(NR) and high density

    polyethylene. They observed that the incorporation of radiated Rice Husk into

    NR/HDPE blends improved the mechanical properties tensile stress and modulus and

    impact strength and hardness.

    Mahboobeh Azadi et al. (2011) investigated the influence of the RHA

    on different mechanical properties of the cured coatings (wear, hardness, and

    elongation). The presence of RHA in epoxy paints can enhance wear resistance,

    scratch resistance, and elongation. It seems that this type of filler in epoxy paints

    increases paint plasticity. The addition of white ash is better in improving the wear

    resistance due to the presence of more silica. Adding 20 wt% black ash to the pure

    epoxy paint lowers its friction coefficient with respect to the white RHA. Finally,

    using this type of filler, which is cheap and abundant in nature, can modify some

    mechanical properties of epoxy paints and also reduce air pollution from burning rice

    husks. Thus, a green product can be produced in the paint industry.

    S. Mahzan et al. uses natural fibre for studying sound absorption properties.

    This study investigates the use of rice-husk waste as the potential element for sound

    absorption material of rice-husk reinforced composite. The study of rice husk waste

    material for sound absorption purposes has been reported. The optimum percentage of

    rice husk was obtained at 25%. The pattern obtained for rice husk was similar to

    membrane absorber curves which are predominant at the lower frequencies.

    Furthermore the peaks value was obtained at 250Hz. Comparison between virgin

    Polyurethane (PU) and the optimum percentage of rice husk (25%) indicated that

    value of mixture is higher than virgin PU at low frequency whereas for high frequency

    the virgin PU is higher. The comparison between other natural materials also has been

    done for recycled rubber and wood shavings. The result demonstrates that rice husk is

    superior to both materials for range 0-500Hz. Since, rice husk is available in large

  • amount, the potential for commercialization, especially for low frequency sound

    absorbent material is possible.

    Reis et al. (2011) studied experimentally the effect of cork and rice husk ash

    micro particles fillers on the mechanical properties (flexural resistance, fracture

    toughness, impact absorbed energy, elastic and viscous moduli) of polyester based

    hand moulded composite was. Filled materials exhibit fragile behaviour and flexure

    strength much lower than polyester matrix, and decreasing significantly when the filler

    content increases from 1 to 5%. The resistance loss is more pronounced for cork

    powder than for rice husk ash filler. Fracture toughness is also much lower for the

    filled composites than for the polymer matrix. Using cork powder the fracture

    toughness decreases significantly with filler content, while for rice husk ash filler a

    slight increase was observed. Both fillers improve absorbed impact energy, peaking

    about 2.5% on filler content. Better improvements were obtained using rice husk ash

    powder, reaching about 30%. Both fillers increase glass transition temperature and the

    maximum use temperature and also the elastic modulus compared with observed for

    the polyester, reaching the modulus a peak for 2.5% of filler content.

    Yussuf et al. (2010) investigated and compared the performances of polylactic

    acid (PLA)/kenaf (PLA-K) and PLA/rice husk (PLA-RH) composites in terms of

    biodegradability, mechanical and thermal properties. It was found that flexural

    modulus of pure PLA was increased drastically when filled with both kenaf and rice

    husk fibres; however, the flexural and impact strengths declined. For composites, it

    was found that kenaf composite shows better mechanical properties compare to rice

    husk composite. The thermal stability of the virgin PLA was decreased by addition of

    kenaf and rice husk; and the composite with rice husk fibre showed higher thermal

    degradation than kenaf composite. From the results of biodegradability, it was found

    that addition of natural fibres slightly improves biodegradability of PLA and kenaf has

    more significant effect on the biodegradation rate, which exhibits better performances

    than rice husk.

    Stefani et al. (2005) proposed the use of rice husk as filler for increasing the

    value of recycled tire rubber. They observed that the addition of rice husk produces a

    decrease in apparent activation energy for low conversions (up to 0.6). For higher

    conversions this decrease was not so clearly observed.

  • Sisir Mantry et al. (2011) fabricated a jute-epoxy composites with

    reinforcement of SiC derived from rice husk. They reported that incorporation of

    fillers modifies the tensile, flexural and inter-laminar shear strength of the jute epoxy

    composites. They also investigated that the presence of particulate fillers (silicon

    carbide) in these composites improves their erosion wear resistance.

    4. Noteworthy Contribution in the Field of Proposed Work:

    D. Siva Prasad et al. (2012) investigated that incorporation of rice husk

    particles in aluminium matrix can lead to produce low cost aluminium composites

    with improved hardness and strength. These composites can find a wide applications

    in automotive components like pistons, cylinder liners and connecting rods. Theses

    composites can also find applications where light weight materials are required with

    good stiffness and strength.

    Acharya et al. (2012) observed incorporation of Rice Husk Char in to epoxy

    significantly reduce abrasive wear loss. Nadazi et al. found that chemical modification

    of Rice Husks by NaOH improves the adhesive properties of Rice Husk. Rout and

    Satpathy studied mechanical and tribo-performance of Rice Husk filled glass-epoxy

    hybrid composites.

    D. Siva Prasad and A Rama Krishna (2012) studied the effect of T6 heat

    treatment on the damping behaviour of aluminium Rice Husk Ash composites. It was

    observed that composites exhibit high damping capacities than unreinforced alloy and

    increases with increase in weight % and the storage modulus increases with the

    addition of RHA particles but decreases with increase in weight %.

    5. Proposed Methodology During the Tenure of Research Work:

    Fabricating a specimen of a new structure of matrix (resin/epoxy) based low

    cost hybrid composite reinforced with the fibres (or whiskers or particles)

    obtained from agricultural wastes.

    Performing different tests on the composite specimen for different

    weight/volume proportions of matrix and reinforcement to study the

  • mechanical, thermal and tribological performances under different parameters

    (viz. types of loading, temperature, environmental factors, etc.) in varying

    conditions.

    Developing a Finite Element Model (FEM) for the composite under different

    parameters and comparing the results obtained with the experiments.

    Analysing the results obtained from the above approaches and their validation.

    Performing parametric study using optimization techniques, such as Taguchi

    Method, to suggest which weight/volume percentage contribute most to give

    significant optimized results.

    6. Expected Outcome of the Proposed Work:

    The mechanical properties of the proposed composite structure depend upon

    the type of reinforcement of one or more types of fibres (or whiskers or particles) and

    the type of matrix (resin/epoxy) used, the relative percentages of each, and the method

    of manufacture. Thus, the expected outcomes will be based on:

    The measurement of reinforcement-matrix ratio, since this property is chosen by

    the application requirements.

    Determination of the relative amounts of reinforcing material(s) and the matrix as

    an important measure of the quality and proper processing.

    Determination of Void content and density, as these can has detrimental effect on

    the mechanical properties of the composite.

    Determination of transition temperature (Tg) of the matrix material, as it is one of

    the most important properties of a cured matrix. This parameter is both a measure

    of the completeness of the curing process and an indication of the maximum

    service temperature of the composite. It is the temperature at which a significant

    change to the elastic modulus will be observed.

    Determination of Elastic Modulus of the composite at the transition temperature.

    Determination of thermal conductivity of the composite to define the specific

    applications of the composite as insulator, conductor or super-conductor.

    Measurement of the operating temperature range of the composite because it is

    probably the most important parameter considered in choosing the chemical

    nature of the matrix.

  • Measurement of Moisture content as it tends to plasticize or soften the matrix. As

    with temperature effects, the composite properties can be measured after exposure

    to water for varying times and at varying temperatures.

    Measuring the effects of variable amplitude loading on remaining life of the

    composite and fatigue under complex stress states as these have received a

    limited attention in the research.

    Prediction of operational life of structures can be made of the said materials is

    feasible and can be based on measurements of fatigue strength and stiffness

    degradation. Thus these properties are to be determined. Also stiffness

    degradation can be correlated to the damage accumulated in the material.

    Structural response of the composite due to cyclic loads can be studied.

    7. References:

    Acharya, S. K. and Samantarai, S. P. (2012). Investigation in to Tribo Potential of

    Biomass Based Carbon Black Filler in Epoxy Composite. International

    Journal of Scientific and Engineering Research , 3 (6), 1-4.

    Ahmad, I., Ee Lane, C., Dahlam, H. M. and Abdulla, I. (2012). Electron - beam -

    irradiated rice husk powder as reinforcing filler in natural rubber / high-density

    polyethylene (NR/HDPE) composites. Composite: Part B , 43, 3069-3075.

    Ayswarya, E., Vidya Francis, K., Renju, V. and Thachil, E. T. (2012). Rice husk ash -

    A valuable reinforcement for high density polythelene. Materials and Design ,

    41, 1-7.

    Azadi, M. and Ebrahim Bahrololoom, M. (n.d.). Enhancing the mechanical properties

    of an epoxy coating with rice husk ash, a green product.

    Bohlooli, H., Nazari, A., Khalaj, G., Kaykha, M. M. and Riahi, S. (2012).

    Experimental investigations and fuzzy logic modeling of compressive strength

    of geopolymers with seeded fly ash and rice husk bark ash. Composite: Part B

    , 43, 1293-1301.

    Chand, N., Dan, T. K., Verma, S. and Rohtagi, P. K. (1987). Rice husk filled - polyster

    resin composites. J. Master Sci. Lett. , 6.

    Chawla, K. K. Composite Materials: Science and Technology. Springer.

    Garcia, D., Lopez, J., Balart, R., Ruseckaite, R. A. and Stefani, P. M. (2007).

    Composites based on sintering rice husk - waste tire rubber mixtures. Materials

    and Design , 28, 2234-2238.

  • Kaw, A. K. (2006). Mechanics of Composite Materials. Taylor and Francis.

    Kwon, J. H., Ayrilimis, N. and Hyung Han, T. (2013). Enhancement of flexural

    properties and dimensional stability of rice husk particleboard using wood

    strands in face layers. Composite: Part B , 44, 728-732.

    Luciana Favaro, S., Savioli Lopes, M. and Radovanovic, E. (2010). Chemical,

    morphological and mechanical analysis of rice husk / post - consumer

    polyethylene composites. Composites: Part A , 41, 154-160.

    Mantry, S., Satpathy, A., Jha, A. K., Singh, S. K. and Patnaik, A. (2011). Preparation,

    characterization and erosion response of jute - epoxy composites reinforced

    with SiC derived from rice husk. Int. J. Plast Technol. , 15, 69-76.

    Nadazi, B. S., Karlsson, S., Tesha, J. V. and Nyahumwa, C. W. (2007). Chemical and

    physical modifications of rice husks for use as composite panels. Composite:

    Part A , 38, 925-935.

    Reis, P., Ferreira, J. and Silva, P. (2011). Mechanical Behaviour of Composites Filled

    by Agro-waste Materials. Fibers and Polymers , 12 (02), 240-246.

    Rout, A. K. and Satpathy, A. (2012). Study on mechanical and tribo performance of

    rice-husk filled glass-epoxy hybrid composites. Materials and Design , 41,

    131-141.

    Rozman, H. D., Lee, M. H., Kumar, R. N., Abusaman, A. and Ishak, Z. A. (2000). The

    effect of chemical modification of rice husk with glycidyl methacrylate on the

    mechanical and physical properties of rice husk - polystyrene compsites. J.

    Wood Chem Technol , 20.

    Siva Prasad, D. and Ramakrishna, A. (2012). Effect of T6 heat treatment on damping

    characteristics of Al/RHA composites. Bulletin of Matrial Science. 35, pp. 989-

    995. Bangalore: Indian Academy of Science.

    Stefani, P. M., Garcia, D., Lopez, J. and Jimenez, A. (2005). Thermogravimetric

    Analysis of Composite Obtained From Sinterining Of Rice - Husk Scrap Tire

    Mixture. Journal of Thermal Science and Calorimetry , 81, 315-320.

    Totry, E., Molina-Aldaregua, J. M., Gonzalez, C. and Lorca, J. L. (2010). Effect of

    fibre, matrix and interface properties on the in-plane shear deformation of

    carbon-fibre reinforced composites. Composites Science and Technology , 70,

    970-980.

    Wessel, J. K. (2004). Handbook of Advanced Materials. Wiley Interscience.

    Xu, Y., Wu, Q., Lei, Y., Yao, F. and Zhang, Q. (2008). Natural Fiber Reinforced

    Poly(vinyl chloride) Composites: Effect of Fiber Type and Impact Modifier. J

    Pollym Environ , 16, 250-257.

  • Yussuf, A. A., Massoumi, I. and Hassan, A. (2010). Comparison of Polylactic Acid /

    Kenaf and Poylactic Acid / Rice Husk Composites: The Influence of the

    Natural Fibers on the Mechanical, Therma and Biodegradibility Properties.

    Journal of Polymer Environment , 18, 422-429.

    8. List of Publications by Candidate: NIL

    (AJAY KUMAR VERMA)

    Signature of the Candidate

    (Dr. S. K. Dhagat) (Dr. M. L. Verma)

    Signature of the Supervisor Signature of the Co-Supervisor