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delivering extra-large diameter drill bits for the oil industry is a difficult task. in the early development phase of the drilling application, a number of design parameters, such as the drill bit quality, have to be designed. the mechanical properties and drill bit mechanics of the developed drill bits have to be determined for the prediction of damage. in this study, we developed a numerical model for prediction of the damage caused by the extra-large diameter drill bits. we used the finite element method to model the drilled hole geometry and damage evolution. the results of the finite element analysis have been verified using experimental data.
both ultrasonic and x-ray imaging methods were used to investigate the microstructural changes in the front and back sides of the specimens after impact. from the ultrasonic and x-ray images of the front and back sides of the specimens, it was determined that the damage occurred at the interfaces, which was confirmed using the hardness test. the microstructural changes were observed using a scanning electron microscope. the results suggest that cracking in the outer surface layers was due to the tensile stresses developed in the outer layers.
the experimental results of the impact test for plain and hybrid composites are presented. the load-deflection data are used to determine the mechanical properties of the plain and hybrid composites. the mechanical properties of plain and hybrid composites can be used to identify differences between materials and to assess the effectiveness of design approaches. the impact tests are conducted to determine the failure modes and mechanisms of plain and hybrid composites. two damage mechanisms were identified for plain woven composites: damage at the interface and damage at the outer surface. the failure modes and mechanisms of hybrid composites were similar to those of plain composites. the mechanical properties of plain and hybrid composites were found to differ significantly. these differences could be explained by the fiber orientation and the damage mechanisms.
prior to the test, moisture was removed from the veneer specimens by heating them in vacuum oven for 15 min. the moisture content of the specimens before the test was approximately 5 percent. the specimens were heated again at 160°c for 10 min at 20 mm/min speed. the heating was necessary to keep specimens hydrated before impact.
the impacts were performed at 4 and 6 km/h impact velocities. the impacts were performed until the shock absorbers of the transducers reached their mechanical limits. the test conditions for all the impact tests were optimized based on the output specifications of the vsi system in terms of the first wave arrival, the maximum wave amplitude, and the worst-case interval. these output data were recorded for each specimen.
optimum impactor dimensions were selected using the following criteria: length at the bottom of the impactor and 10 mm above the notch, width at the impact notch, 10 mm above the notch, and height at the notch, 6 mm above the notch. impactor displacement was 8 mm for all tests. using these dimensions, the displacement was varied from 0.5 mm to 10.5 mm to obtain the required impact velocity. based on the dimensions determined, maximum vertical forces at the bottom of the impactor were measured using a load cell with a resolution of 0.05 kg/cm 2. the values were recorded using vsi system.
a total of four samplings were performed at each velocity to obtain measurements of the critical energy release rate. the samplings were evenly spaced and performed at the same time, therefore, any relative movements of the specimens were minimized during the impact. the initial and final micrometer readings were recorded and used to compute the displacement of the platform and the maximum force at the impactor bottom. the first micrometer reading was taken at the beginning of the test and the final one at the end of the test. the readings at the end of the test were used to compute the specimen deformation and displacement using vsi system.
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