Tension
Figure 5 illustrates the stress strain curve of four different materials that are proposed as alternative implant materials: kevlar, hybrid, carbon fibre, and flax.
It’s clear that all fiber materials have an increasing behavior in their tensile strength when increasing the volume fraction. However, in flax fibers, both 8 and 16 vol. % have displayed convergence in performance.
It can be deduced that KF exhibits the highest tensile strength, indicating its superior ability to resist tearing under tensile stress. Moreover, during the test, the failure of the KF composite was catastrophic and sudden.
The hybrid material follows CF in terms of tensile strength and exhibits almost a similar performance under strain; unlike KF, there was a tearing sound in the hybrid composite that could be detected, which made the failure point more anticipated. This is due to the presence of CF within the composite. CF, while less in tensile strength than KF and the hybrid material, outperforms flax, which trails behind the other three materials with the lowest tensile strength. For further understanding, Fig. 6 illustrates the effect of volume fraction on ultimate tensile stress for KF, hyprid, CF, and flax at a strain rate of 10 mm/min.
Figure 6 illustrates the relationship between volume fractions of reinforcement fibers and ultimate tensile stress. As the volume fraction increases from 0–24%, all materials exhibit an increase in stress, indicating that they become durable. Among them, KF stands out with the highest stress values across all volume fractions, reaching 283.5 Mpa at 24 vol. %, leaving a big gap between other proposed composites, making it the most robust of the four materials.
Flexural Test Mode 1
Figure 7 presents a comprehensive analysis of the relationship between deflection and flexural stress for different composite materials at varying volume fractions, 8, 16, and 24%. The materials under study include pure, flax, CF, KF, and hybrid.
It’s crucial to understand that in flexural stress, the upper section undergoes compression (above the neutral axis), while the lower section is subjected to tension (below the neutral axis). In the context of the first mode of the bending test, the fibers oriented in the transverse direction play a more significant role in responding to the bending load. As a result, when analyzing the curves in Fig. 7, they display a zig-zag pattern, indicative of the ongoing rupture of fibers along the transverse direction.
Figure 8 depicts the influence of the volume fraction of fiber reinforcement on flexural strength. As the volume fraction rises from 8 to 24%, all composites demonstrate a significant increase in flexural force, indicating a positive relationship between the volume fraction and the flexural stress of the proposed composites. KF appears to consistently display the greatest flexural force across all volume fractions (8, 16, and 24%), making it the most resilient to flexural bending.
Flax, CF, and hybrid fibers exhibit increasing performance, with hybrid typically surpassing flax and CF. In terms of flexural elastic modulus, a similar trend as above is observed, as it escalates with the introduction of reinforcement fibers, starting with flax, then CF, then hybrid, culminating at the apex, which is KF fibers achieving 53 MPa at a 24% volume fraction.
Flexural Testing Mode 2
At first glance of Fig. 9, two significant insights can be drawn. First, the performance of the fiber within the epoxy matrix reflects the pattern seen in the initial bending mode. Second, there is a substantial increase in flexural forces across different volume fractions. This rise is in line with expectations, originating from the 90⁰ rotation of the implant, leading to an increased area moment of inertia. As a result, the composite suggested for the implant demonstrates improved resistance to flexural forces. However, this comes at the cost of reduced ductility, which has significantly decreased by about 50% compared to the first mode.
In Fig. 10, at volume fractions of 8 and 16%, the performance of KF and hybrid fibers was relatively similar. However, a notable peak emerged for KF at a volume fraction of 24%, reaching a value of 90.4 MPa.
To understand and examine the fracture mechanism of the proposed compositions, a microscope was used to image the fracture surface at the microscale, Fig. 11, for each of the fiber types used.
Figure. 11 illustrates the fracture zone of each proposed fibers. In Fig. 11(a), flax appears as bundles made of smaller fibers intertwined together, forming a large cohesive bundle, in contrast to carbon fiber CF, hybrid, and KF, that consists of small fibers woven together. Flax fibers stand out due to their larger size compared to other fibers, resulting in a distinct behaviour upon detachment from the epoxy matrix. As these fibers separate, they carry substantial segments of epoxy, appeared in the red coloration. This is in stark contrast to the behaviour observed with other fibers, where small epoxy particles on the surface, highlighted in blue, as depicted in Fig. 11(b), (c) and (d).
Upon examining the fracture shape of the fibers themselves, indicated by the green colour, a crucial observation emerges regarding the fundamental difference in fracture mechanisms between CF and KF. Previous conclusions drawn from tensile and bending tests, whether in the first or second mode, have consistently demonstrated KF superior strength compared to CF. This assertion finds further support in the images captured. In Fig. 11, (b), (c), and (d), it becomes apparent that during tension tests, KF undergo slight elongation, see Table 4, until reaching the fracture point. Upon complete separation, these fibers undergo a spring-back effect, resulting in a characteristic arching shape at the fracture area. On the other hand, the CF has straight fiber breakage, showing a brittle fracture characteristic, see Table 3.
The assessment of the performance of composites reinforced with KF fibers via mechanical testing uncovers a potentially beneficial substitute for traditional metal implants. This substitute tackles a key issue related to stress shielding, a phenomenon triggered by the excessive rigidity intrinsic to metal implants. The composites, distinguished by their diminished rigidity, bypass this problem without sacrificing the necessary mechanical strength vital for the implant’s effective operation during the bone recovery process. As a result, the integration of KF into the composites presents itself as a promising approach, providing a balanced trade-off between rigidity and mechanical strength, thereby improving the overall effectiveness of orthopaedic implants.