Large-size metallic glass composite material with tensile ductility and preparation method thereof
A technology of metallic glass and composite materials, which is applied in the field of metal matrix composite materials, can solve problems such as the application of plastic materials, and achieve the effects of eliminating shrinkage, simple and controllable process, and uniform structure
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[0017] The present invention has tensile plastic large-scale metallic glass composite material, and its alloy composition expression is: Zr a Ti b m c Cu d Ni e be f , where M is one of Nb, V or Hf, a, b, c, d, e, f represent atomic percentages, and the ranges are 10≤a≤70, 10≤b≤70, 4≤c≤20, 2≤d≤20, 0≤e≤15, 5≤f≤22.5, a+b+c+d+e+f=100. The preparation method of the above-mentioned metallic glass composite material comprises the following steps:
[0018] The first step: select the alloy elements Zr, Ti, M, Cu, Ni, Be with a purity greater than 99.5%, according to Zr a Ti b m c Cu d Ni e be f Proportioning is carried out, and the master alloy is melted in a pure argon atmosphere electric arc furnace with titanium oxygen absorption, so that the alloy composition is homogenized, and the master alloy profile is sucked and cast.
[0019] Step 2: Put the master alloy profile into the crucible, heat it to 1300°C-1350°C, keep it warm for 10-20 minutes, and perform overheating t...
Embodiment 1
[0039] (1) Selection of raw materials
[0040] The purity of each metal component that the present invention prepares master alloy ingot for selection is as table 1, and alloy composition is (Zr 4 TiNb) 80 (Cu 5 Ni 4 ) 10 be 10 i.e. Zr 60 Ti 14.5 Nb 5.5 Cu 5.6 Ni 4.4 be 10 (atomic percent).
[0041] Table 1 prepares the purity (%) of the metal component selected from the master alloy ingot
[0042]
[0043] (2) Preparation of master alloy ingot
[0044] Under the conditions of Ti inhalation and high-purity argon protection, master alloy buckle ingots are melted in a non-consumable arc melting furnace. The specific procedures are as follows:
[0045] a. After mechanically grinding the surface of the metal raw material to remove the oxide skin on the surface, prepare the material according to the designed composition ratio; put the prepared material into the water-cooled copper crucible in the melting furnace according to the weight of about 80g per ingot, cover ...
Embodiment 2
[0056] Embodiment 2 adopts the method identical with embodiment 1, and alloy composition is (Zr 4 Ti 4 Nb) 81 Cu 6.5 be 12.5 i.e. Zr 36 Ti 36 Nb 9 Cu 6.5 be 12.5 (atomic percent). The prepared composite sample with a diameter of 30 mm has uniform structure and no defects, and the tensile plastic strain reaches 9%.
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