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The materials under consideration in the present research are a glass fibre reinforced PU-foam sandwich structure and its constituents. These constituents are: a flexible open cell PU-foam, a rigid closed cell PU-foam and a continuous glass fibre mat. The general goal of this research is to build different tools to analyse and predict the mechanical properties of the constituents and the final sandwich structure. Therefore, this research combines experimental work with numerical modelling techniques.The first part of this dissertation discusses the open cell PU-foam. Although the open cell foam is not the main load carrying material in the sandwich panel, characterizing and modelling it is of great importance in other research areas (e.g. surface functionalization or pressure drop calculations). The cellular structure of this foam is characterized by means of optical microscopy, SEM and CT. Based on the outcome of the experimental observations, the Kelvin cell and Weaire-Phelan structure were selected as RVE for the FE-modelling. Up to now, the use of the latter structure to build a FE-model has not been reported in literature.In correspondence to real foams, the material distribution in the cell edges of the RVE based FE-models is completely governed by a minimization of the surface energy. The influence of the cell size, solid PU material stiffness, relative density and shape anisotropy on the mechanical properties of the open cell foam, is investigated by means of these models. The Weaire-Phelan based FE-model proved to represent and predict the mechanical properties of the open cell foam in a better way than the standard Kelvin cell based FE-model. In order to decrease the large spread on the available data regarding the solid PU stiffness, special attention is given to this parameter.The skins of the investigated sandwich structures consist of a GF/PU-foam composite. Because the skins are formed in situ, they cannot be characterized in advance which hinders a pre-production prediction of the mechanical properties of the sandwich panel. Therefore, X-ray CT-imaging combined with image processing algorithms are used in the current study to determine the skin thickness and fibre orientation distribution function. This allows to calculate the stiffness of the skins based on the rules of mixture and the Mori-Tanaka inclusion model. The resulting data were successfully validated by experimental work.In the final part of this research the knowledge on the stiffness of PU-foam core and GF/PU-foam composite skin is joined into a simple calculation tool to predict the bending stiffness of the sandwich panels. A comparison of the calculated values to experimental stiffness data, measured on industrially produced plated, revealed an accuracy of +/-10%. Moreover, the influence of different parameters like the weight and orientation of the applied fibre reinforcement mats is indicated by this tool and allows to identify directions for future material developments.
669 <043> --- Metallurgy--Dissertaties --- Academische collection --- Theses --- 669 <043> Metallurgy--Dissertaties
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The use of carbon fibre-reinforced composites has been growing exponentially in the past few decades. They offer excellent mechanical properties in combination with a low density, making them an ideal solution for many lightweight applications. However, they often suffer from a lack of toughness. In contrast with carbon fibre composites, self-reinforced composites have an excellent toughness, but a relatively low stiffness and strength. They consist of a polymer fibre in a matrix made from the same polymer. This thesis aims to break through the typical stiffness-toughness dilemma by hybridising carbon fibres with self-reinforced polypropylene (SRPP) and to design a material that is both stiff and tough. The focus lies on optimising the tensile properties and impact resistance of these novel hybrid composites.Before hybridising SRPP, it is vital that the influence of the process parameters on the mechanical properties of SRPP is understood. Hot compaction uses oriented monocomponent polymer tapes, and melts their outer surface to create the matrix. This process has a narrow processing window and is therefore inherently sensitive to the process parameters. It was shown that increasing the temperature or dwell time increased the matrix fraction and molecular relaxation of the oriented polymer tapes. This leads to improved interlayer bonding, which has a small effect on the tensile properties, but a large effect on the impact resistance. The compaction pressure was even more important, as too low of a pressure can strongly reduce the penetration impact resistance. The impact resistance is a key advantage of SRPP, and therefore potential issues with traditional testing techniques were identified. Hybridisation of SRPP with carbon fibres resulted in a novel class of hybrid composites with a unique combination of stiffness, strength, ultimate failure strain and impact resistance. Inter- and intralayer hybrids were developed and optimised. For interlayer hybrids, it was revealed how the damage development in tension can be controlled by changing the carbon fibre volume fraction, the carbon fibre and SRPP orientation, and the relative layer thickness. An appropriate choice of these parameters leads to pseudo-ductility, where the carbon fibre layers are able to fracture multiple times. For intralayer hybrids, the importance of intralayer bonding was highlighted. This parameter is crucial as a strong intralayer bonding reduces the ultimate failure strain and impact resistance, but improves the flexural properties. Improving the adhesion between carbon fibre and polypropylene has a similar, but more pronounced effect.The experimental work was supported by extensive modelling studies. A novel and versatile strength model for unidirectional hybrid composites was developed. This model was first elaborated for non-hybrid composites, and its strengths and limitations were identified. An in-depth experimental validation was performed for carbon fibre composites by comparing fibre failure predictions with synchrotron computed tomography data. This led to vital recommendations for future model developments. This model was then extended to hybrid composites and an extensive parametric study was performed. This study focused on the hybrid effect, which is a synergistic effect that increases the failure strain of carbon fibres through hybridisation with a more ductile fibre. The hybrid effect was shown to increase by reducing the carbon fibre volume fraction and by improving the dispersion of both fibre types. The mechanical properties of the ductile fibre were not crucial for the hybrid effect, provided its failure strain is at least twice as high as the carbon fibre failure strain. Using very ductile polypropylene fibres instead of the traditional glass fibres hence does not lead to a larger hybrid effect in carbon fibre hybrid composites. The main advantage of polypropylene fibres is its potential of achieving a larger ultimate failure strain. The predictions of the hybrid effect were also compared to experimental measurements. This validation was the first of its kind to achieve a good agreement, which indicates that the model captures the main phenomena of the hybrid effect.Finally, a road map for optimising hybrid self-reinforced composites was set up by combining the experimental results with the modelling insights. This road map can also be used to optimise other hybrid self-reinforced composites. The presented results revealed the potential benefits of hybrid composites. They should provide a driving force for future work on hybrid composites and for improvements in processing technologies for manufacturing well-dispersed hybrid composites.
669 <043> --- Academische collection --- Metallurgy--Dissertaties --- Theses --- 669 <043> Metallurgy--Dissertaties
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Natural fibres are a realistic and ecological alternative to synthetic fibres as reinforcement for polymer composite materials due to their low cost, environmental friendliness, natural abundance, and mechanical properties. The latter allows the design of composite materials to meet specific mechanical properties. For instance, bamboo exhibits a combination of low density (~1.4 g/cm³) and high stiffness (~43 GPa) and strength (~800 MPa), while coir fibres are not very strong and stiff, but exhibit high strain to failure (approximately 40%).However, their potential as reinforcing agent is reduced when compatibility problems with polymer matrices arise at the interface. The generally hydrophilic nature of natural fibres produces low interfacial interactions with certain important hydrophobic thermoplastic matrices, such as polyethylene and polypropylene, leading to a poor interfacial strength.Mechanical properties of composite materials can be greatly affected by the bond strength at the fibre-matrix interface. When a composite structure is loaded, the load is transferred from the matrix to the fibres mainly through shear stresses at the interface. Load transfer increases with increasing interfacial (shear) stresses, thus improving the composite strength. The adhesion at the interface can be described as a combination of physical adhesion (related to wettability), chemical bonding, and mechanical interlocking. In this study, the wettability and compatibility of the fibre and the matrix is assessed by the analysis of their surface energies. This is done by measuring contact angles, which is a quantitative measure of solid-liquid molecular interactions and thus provides information on the surface energy of solids.This dissertation develops an interdisciplinary and integrated approach that deals with the physical, chemical, and mechanical aspects of natural bamboo fibre composite interfaces. The wetting and mechanical behaviour at the interface of smooth and isotropic synthetic fibres (glass, polyethylene terephthalate) are compared with that of a rough and anisotropic natural fibre (bamboo). Atomic force microscopy (AFM), X-ray Photoelectron Spectroscopy (XPS), Time-of-Flight Secondary Ion Mass Spectrometry (ToF-SIMS), and optical profilometry techniques were used to study the fibres topography and chemistry. A new approach, based on an autoclave treatment, to reduce the noise in performing contact angle measurements on rough natural fibre surfaces is presented. The results indicate that the high concentration of lignin on the surface of bamboo fibres is responsible for their surface wetting properties.The wetting dynamics of various test liquids on bamboo fibres is analysed by applying the molecular-kinetic theory of wetting. The surface free energy components are calculated according to the acidbase theory. These values are then used to calculate the theoretical work of adhesion, spreading coefficient, wetting tension, and interfacial energy for analysing the fibre-matrix compatibility. Additionally, a novel way to measure equilibrium contact angles by using sound excitation is proposed. This way it is possible to better take into account both polar and dispersive surface energy components. The findings suggest that the contact angle obtained by forcing relaxation through acoustic vibration is a reliable method to study the wetting behaviour of natural fibres.Moreover, understanding of the stress state in the composite after processing and during mechanical testing is required for a correct analysis of adhesion properties. The mechanical strength of the interfaces was assessed by single fibre pull-out tests, and transverse 3-point bending tests. The fibre matrix interfacial bond strength was characterized by the critical local value of interfacial shear stress. Since during crack initiation in the pull-out test, the crack surfaces move directly apart, it is possible to correctly relate the theoretical work of adhesion with the normal stress at the debond point. This radial normal stress at the interface at the moment of crack initiation is also used in this study as a parameter for correlating thermodynamic work of adhesion and practical adhesion.
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Metallurgy
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669 Metallurgy
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Possessing excellent stiffness and strength, carbon fiber reinforced polymers (CFRPs), however, have a limited toughness. The first damage in CFRPs usually occurs in transverse plies where stiff carbon fibers are microscopic stress concentrators in the matrix. The toughness of CFRPs can be enhanced by adding carbon nanotubes (CNTs) – nano-reinforcements of a high aspect ratio and exceptional stiffness – into the polymer. CNTs are believed to redistribute matrix stresses by lowering the matrix stress concentration scale from micro-level – around carbon fibers – to nano-level – around CNT tips – thereby hindering damage onset.The aim of this work was to understand the effect of CNTs on the stress distribution in CFRPs using a numerical approach. A novel finite element model was developed that represents thousands of individual CNTs with a “true-to-life” morphology in a composite with microscopic fibers in a single simulation. A numerically efficient “embedded elements” method was verified against analytical and numerical solutions. The developed model captured the matrix stresses between individual CNTs, thereby allowing the microscopic matrix stresses within the CNT-rich matrix regions to be captured as well.The discovered heterogeneity of the matrix stress fields in nano-engineered fiber reinforced composites with CNTs (nFRCs) was found to be strongly affected by the length, position, orientation, waviness and concentration of the CNTs. CNT agglomerates were shown to behave as stiff microscopic particles and to exacerbate the existent stress concentrations. CNTs introduced at fiber surfaces by fiber grafting or sizing/coating with CNTs were found to increase stresses in resin-rich zones between the fibers. CNTs grown on fibers were also shown to effectively suppress stress concentrations in the matrix close to the fiber surface.The conventional CNT configurations in FRCs were shown to be suboptimal for the purpose of suppressing microscopic stress concentrations: this was at the cost of stress magnification in other matrix regions. To address this issue, a novel concept of intelligent hierarchical nFRCs was proposed and modeled. Combining precise localization and orientation of CNTs, a complete elimination of microscopic inter-fiber stress concentrations was achieved by aligned CNT “bridges” constructed interdependently with the fiber positions in FRC.The modeling results presented in this thesis are the first step towards practical realizations of such hierarchical structures. Designed to suppress micro-scale stress concentrations in the material, the intelligent CNT networks are, hence, designed to postpone the damage onset in the fiber composites.
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