Method and device for preparing large-size bulk amorphous composite materials
An amorphous composite material, large-scale technology, applied in the field of fiber/amorphous composite materials, can solve the problems of size, interface reaction limitation, etc., to achieve the effect of reducing interface reaction, short contact time, and controlling mechanical properties
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Embodiment 1
[0024] Example 1. Several pieces of VIT1 amorphous flakes with different thicknesses were prepared by the copper mold suction casting method. Take out three of them, such as figure 2 The I, II, III non-wafers shown, the overlapping height of the three non-wafers is 4.7mm, and they are sequentially polished with 400~1000# sandpaper, and cleaned in acetone and alcohol using ultrasonic waves, and placed in the mold after overlapping. superior. The initial pressure of the indenter at both ends of the Gleeble is 150MPa (the pressure is 294kgf), and the surface of the amorphous sheet is blown with high-purity argon for protection, and heated. The heating rate is 20K / min, and the heating upper limit is 410°C. During the test, the pressure was always maintained at 150MPa. The compression plastic deformation is very fast, and the holding time is very short. After the plastic deformation, the temperature is increased within a few degrees, and then unloaded, and the sample is taken ou...
Embodiment 2
[0026] In the experiment, the polished and cleaned VIT1 bulk amorphous and tungsten composite wires were wrapped in layers and orderly. The directions are perpendicular to each other. figure 1 The upper and lower heating furnaces are first heated to a certain temperature, and then put the package into the figure 1 In the backing plate mold, heating is carried out at a heating rate of 40K / min, and then heat preservation and pressure are applied. The relationship between heating temperature and heating time is as follows Figure 4 As shown in (a), the relationship between heating time and displacement is as follows Figure 4 As shown in (b), the relationship between loading load and heating time is as follows Figure 4 (c) shows. In the test, the final compressive stress is 100MPa. The morphology of the prepared composite material is as follows Figure 4 shown.
Embodiment 3
[0028] Others are the same as in Example 2. In the test, five layers of 0.2mm amorphous flakes sandwich four layers of tungsten composite double wires (a 0.2mm×0.4mm cross-sectional shape of the amorphous composite double wires is selected), and the final compressive stress is 50MPa. The morphology of the as-prepared composites is as follows: Figure 5 shown.
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