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HIGH STRENGTH CARBON NANOFIBERS DERIVED FROM ELECTROSPUN POLYACRYLONITRILE

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HIGH STRENGTH CARBON NANOFIBERS DERIVED FROM ELECTROSPUN POLYACRYLONITRILE ( high-strength-carbon-nanofibers-derived-from-electrospun-pol )

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2.4. Mechanical Experiments with Individual Nanofibers A MEMS nanoscale testing platform, developed to test individual VGCNFs [33], was used to measure the strength and the elastic modulus of individual PAN based CNFs. Individual CNFs were isolated with a sharp tungsten probe and were mounted onto the grips of a surface micromachined loadcell/grip system shown in Figure 2.6(a). A UV curable adhesive was used to attach a CNF to the tip of tungsten probe which was then pulled away to isolate a single CNF. The isolated CNF was mounted on the grips of the loadcell again with the help of UV adhesive. The adhesive grips were very compliant, therefore, a FIB was used to deposit Pt, Figure 2.6(b), at both ends of the CNFs before testing to ensure rigid mounting. During Pt deposition most of the adhesive was etched away and a strong bond was formed between the Pt, the CNF and the polysilicon surface. After CNF mounting, a long thin glass cantilever was attached to the device grip with a two part epoxy. This step avoided preloading of the CNF, which could cause early fracture. The loadcell was gently pushed forward to keep the CNF loose during an overnight epoxy curing. The MEMS platform was actuated by an external piezoelectric device and the loadcell deflection and distance between the grips (i.e. change in CNF length) were recorded independently by a CCD camera at 400× optical magnification as described by Naraghi et al. [41]. Digital Image Correlation (DIC) was applied to the optical images to calculate the loadcell opening and the CNF extension with a displacement resolution of 25 nm [50]. Figure 2.7 shows the three regions on the MEMS platform which were used to apply DIC. The experiments were carried out under mercury light to enhance the speckle pattern used in DIC. The displacement between regions 1 and 2 provided the CNF extension and the displacement between regions 2 and 3 was the loadcell opening, which in turn provided the applied force after use of the calibration factor. The stiffness of relatively compliant loadcells was measured via a traceable method by suspending glass spheres of known weight and recording corresponding loadcell deflections [51]. The force and nanofiber extension data were used to construct stress vs. strain curves for the CNFs. A representative stress-strain curve of a CNF is shown in Figure 16

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