Icdd Pdf 4 Database 70 ⏩
Icdd Pdf 4 Database 70 ⏩
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Icdd Pdf 4 Database 70
The crystal structure of commercial product was determined by X-ray powder diffraction analysis. X-ray powder diffraction patterns obtained with CuKα radiation show that the synthesized product is composed of three phases in a formula of CuxMo3N2 with lattice parameters of a = 8.9255(2) Å, b = 11.7269(3) Å, and c = 6.8853(2) Å for phase I, and a = 8.9126(6) Å, b = 5.4195(4) Å, and c = 13.546(1) Å for phase II. It is claimed that phase I is goethite more than 75 wt% and may be possibly MgMn2O4, while phase II is an oxy-(H2O) compound. No phase III was found in the X-ray diffraction data set. A summary of crystal structures and lattice parameters of four compounds are listed in Table 1.
Investigation was performed to study of the mechanical behavior of tested alloys at different temperatures. The studied materials are widely used for the cylinder head compartments of two-cycle engines. The hardness of studied materials was checked using the wear test for metallographic specimens. The wear test results are presented in Table 2. The data obtained are illustrated in Fig. 8. We can see that the wear resistance is the greatest in the case of the Ni-based alloy produced by the current method. The wear resistance diminishes in reverse order in the case of the following: a) unmodified aluminum alloys; b) standard aluminum alloys; c) Ni-based alloys produced by the current method; d) standard Ni-based alloys. The differences between the resistance of unmodified alloys and commercial products can be explained by the differences in their chemical composition. As we can see, the Ni-based alloys produced by the current method have higher resistance to wear than the standard products. It has to be taken into account that the commercial alloys have to meet more requirements such as abrasion resistance. The wear behavior of alloys was investigated on the basis of energy dissipation density and its changes over time. The phenomenon investigated was dynamic friction. The results of wear behavior of alloys are presented in Fig. 9 and Table 3.
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