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INFLUENCE OF THE BINDING SYSTEM ON THE COMPACTION BEHAVIOUR OF NCF - PDF document

18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS INFLUENCE OF THE BINDING SYSTEM ON THE COMPACTION BEHAVIOUR OF NCF CARBON FIBRE REINFORCEMENTS S. Aranda 1 *, F. Klunker 1 , G. Ziegmann 1 1 Institute of Polymer Materials and Plastics


  1. 18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS INFLUENCE OF THE BINDING SYSTEM ON THE COMPACTION BEHAVIOUR OF NCF CARBON FIBRE REINFORCEMENTS S. Aranda 1 *, F. Klunker 1 , G. Ziegmann 1 1 Institute of Polymer Materials and Plastics Engineering, Clausthal University of Technology, Clausthal-Zellerfeld, Germany * Corresponding author (santiago.aranda@tu-clausthal.de) Keywords : liquid composite moulding, preforming, binder, non-crimp fabrics, compaction 1 Summary automatable steps like storage and transfer to the The compaction behaviour of textile reinforcements mould [1]. In order to achieve this net-shape- must be considered for the design and optimisation preform, thermoset or thermoplastic binders of closed mould manufacturing processes. The (tackifiers) are applied between layers. Being solid at room temperature, they melt at their deformation of the reinforcement during preforming and processing has a direct impact on the production corresponding activation temperature, allowing the parameters as well as the final product textile plies to bond together after the preforming characteristics. The presence of powder binder and cycle. fleece between layers as tackifier has an influence An important requirement is that the preform must on the compaction response of the material. In this properly fit to the mould cavity in RTM-processes: work, compaction-relaxation-release tests were on the one hand if the preform is too thin, it will not performed for three non-crimp fabric lay-ups be possible to assure a predictable flow front combined with two different binding systems. The progress. On the other hand, if the preform is too experiments were carried out at preforming thick, additional pressure must be applied to close temperature (120°C). The compaction behaviour the tooling before impregnation. Problems depending on the material and compaction associated to the spring-back effect derived from temperature are analysed in this paper. relaxation of the fibres must be also taken into account, such as potential difficulties during the 2 Introduction operations previous to impregnation. These The transversal compaction behaviour of fibre challenges can be addressed with a systematic and reinforcements has to be considered in the design of process-oriented study of the compaction response of the fibre reinforcement. [2] and [3] reported a the manufacturing process chain, from preforming to after-infusion. higher fibre volume content as well as a lower spring-back effect when the preforming was The preforming phase is critical for the achievement performed at higher temperature and using binders. of high production ratios, which are necessary to Together with the concentration, size and type, the spread the use of carbon fibre reinforced plastics in location of the binder will determine the minimum new applications like automotive industry for thickness achievable under compression and the example. During the preforming operations the magnitude of the spring-back effect. As reported by fibrous reinforcement gets close to the actual [3], an easier compression and a better controlled component geometry and is prepared for a spring back are achieved when the binder is located convenient impregnation. Preforming requires in the interlayer (outside the tows) than within the accurate specification of the fibre orientations tows. Their work also pointed out that a higher besides the fibre volume content (FVC) which is concentration of binder in the interlayer would essential to achieve the targeted mechanical slightly increase the spring-back control, but properties. Furthermore, the handling of the preform decrease the degree of compaction. in the steps before the impregnation must be assured as well. Indeed, the preform must be sufficiently Transversal compaction must also be considered stable to conserve its integrity and geometry during during the impregnation stage, since the flow and the

  2. compaction behaviour are strongly coupled. The sorts of reinforcements. They fitted their dependence of the reinforcement permeability on the experimental data to a model where the fibre is fibre volume content has been already widely modelled as a bulking arc contacting at two single reported [4]. Recent works suggest that the points at the beginning of the compaction, increasing compaction velocity has an influence on the the contact region gradually as the compaction transversal permeability K z [5]. The evolution of the pressure increases. Fibre volume content is linearly transversal compaction behaviour becomes quite related with applied pressure at the beginning of the complex during the infusion because of the compaction but presents a nonlinear relation for difference between dry and wet compaction [8] and higher values of pressure. Some other models have the expected lubrication caused by the resin. been proposed to describe the compression behaviour of fibrous reinforcement like the The power law (Eq. 1) is the most commonly used exponential fit of Kang [13]. expression to model the dependence between fibre volume content and compacting pressure [6], [7] . None of the above mentioned models take into account effects like the permanent deformation σ = a ⋅ k V Eq. 1 remaining after compression, hysteresis or the f effects of cyclic loading [14]. Comas-Cardona et al. Where σ represents the transversal stress, V f is the [15] proposed a non-linear elastic-plastic model fibre volume fraction and a and k are material which considers finite strains for loading and parameters. Adjusting a and k , the dry and wet unloading of glass fibre woven fabrics. behaviour can be described. Although this model fits Bickerton and Kelly [16][17] modelled both the well to experimental data, it presents a singularity compression and relaxation phases by means of the when the applied compaction pressure is still zero, same viscoelastic model. They showed the effect of as it implies that the fibre volume content is zero and the compression rate on maximum stress required to thus, the thickness of the laminate is infinite. It reach the desired compaction degree and the makes the implementation of these models in relaxation effect at a held deformation. In [18] a new simulation a difficult task. A more realistic model formulation considering stored and frictional was presented by the authors [9] which considers the dissipated energy are presented. fact, tat even uncompressed fibres have a finite thickness and a initial fibre volume content V 0 (see More recently Bayldon [19] presented an Eq. 2). interpolation model based on Gutowski´s approach that describes the compaction stages in typical σ = ⋅ − k a V V Eq. 2 ( ) 0 f flexible bag processes considering partial unloading and reloading cycles. A lot of effort has been paid to the study and modelling of the compaction behaviour for a variety Nevertheless, much attention has not been yet paid of materials. Van Wyk [10] studied the properties of in the literature to study the influence of the wool and derived the power equation for the temperature on the compaction behaviour which is compaction of a 3D network of randomly oriented mostly related to the behaviour of binders. In [20] fibres. The physical model assumes that the fibres the influence of a preheating treatment on the behave like bending beams that transmit loads compaction of a non-crimp fabric with a through contact points. The compaction pressure thermoplastic fleece was presented. This work is the increases with the 3 rd power of the fibre volume continuation of this investigation line, exploring the content. One disadvantage of this early approach is influence on the preforming and liquid composite that it is not able to handle with aligned fibres. moulding processes. Gutowski et al. [11] studied the consolidation of pre- impregnated reinforcements and proposed different 3 Materials and Experimental Method versions of a compaction model for aligned and In the present work, the compaction behaviour of undulated fibres, where fibres are initially bent and three different non-crimp carbon fibre stacking straightened under pressure. In [12] Batch and co- sequences at preforming temperature is studied. It workers measured compaction pressures of different

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