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Although helical electrodes have been proven to improve the EDM (electrical discharge machining) speed of small holes, there are few studies on the morphological characteristics of the machined small holes and the influence of electrode structures. In this paper, the influence of the helical electrode structure on the machining effect is studied by the method of orthogonal experiment, and the internal mechanism of the influence of the helical electrode on the machining is explained by the method of CFD (computational fluid dynamics) simulation. The results show that the larger depth and width of the helical groove and the helix angle of 60° are beneficial to increase the machining speed and reduce the relative loss rate, and at the same time, avoid serious defects in the small hole morphology. These conclusions provide a valuable reference for future researchers to choose the reasonable structure of the helical electrode, which is of great significance. [ABSTRACT FROM AUTHOR]

Wire electric discharge machining (WEDM) and electrical discharge machining (EDM) promise to be effective and economical methods for the machining of metal matrix composites and conducting ceramic blanks. However, the machining process of Ni-AlO functionally graded materials (FGMs) is extremely difficult because the insulating ceramic layer cannot be machined directly by EDM. In this paper, the pure AlO layer has been machined by self-induced EDM, using the conductive layers of Ni-AlO FGMs to trigger the discharges in the insulating ceramic layer. Machining experiments have been performed to investigate the effects of discharge capacitance, pulse off-time, and charging resistance on the process performance of the pure AlO layer using RC-type pulse generator. From the experimental results, the discharge waveform of pure AlO layer includes long pulse discharge waveform, in addition to conventional normal discharge of conductive layers. The shape of long pulse discharge waveform can be changed by pulse off-time. The appropriate pulse off-time not only improves the stability of EDM but also increases the material removal rate (MRR). Moreover, it was observed that the MRR increases with increasing discharge capacitance and decreasing charging resistance. The surface roughness increases with increasing discharge capacitance. Finally, a small hole with a depth-diameter ratio of 5, little tapper is machined based on the experimental analysis. [ABSTRACT FROM AUTHOR]

C f -ZrB 2 -SiC is a new composite material with excellent properties for making the next-generation aerospace component. This material is extremely difficult to removal by mechanical machining, and there is a lack of research on feasible secondary processing methods of this composite at present. Micro-EDM is not limited by material hardness, so it is very suitable for machining this material. In this paper, the Material removal mechanisms and processing characteristics of C f -ZrB 2 -SiC by micro-EDM is analyzed. The removal mechanism of composite materials is explored though the discharge crater morphology, and the single-discharge experiments of each phase materials with different medium and different energies are also carried out as a reference. Electrical discharge milling experiments of C f -ZrB 2 -SiC are performed to explore the medium on processing index, and found that the best surface quality and maximum processing efficiency can be realized in kerosene. An experiment with four factors (pulse width, voltage, peak current, capacitance) and three indexes (surface roughness, MRR, TWR) is designed to analyze the C f -ZrB 2 -SiC process characteristics of micro-EDM and the response surface diagram and second-order regression equation are obtained. Milling the C f -ZrB 2 -SiC by electrical discharge according to the optimal combination of surface roughness parameters deduced above, the as-machined surface is analyzed including the surface morphology by SEM, element content by EDS and the surface phase by XRD. The feasibility and advantages of micro-EDM on machining C f -ZrB 2 -SiC are prove. [ABSTRACT FROM AUTHOR]