Method for preparing nb-based multi-element powder fusion alloy coating on titanium metal surface
A technology of element powder and alloy coating, which is applied in the field of surface modification of titanium metal and the preparation of Nb-based multi-element powder fusion alloy coating on the surface of titanium metal, which can solve the problems of low hardness and poor wear resistance, and achieve small changes in hardness , High corrosion resistance, high coating hardness
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Embodiment 1
[0024] Such as Figure 1-3 shown.
[0025] Put 62.2 grams of Nb powder, 26.5 grams of Sn powder, 10 grams of Zr powder, and 1.3 grams of Ti powder in a ball mill, mix them evenly, take them out and dry them, and press them into tablets (thickness is about 0.5 mm) on a press. Place the pressed tablet on the cleaned titanium surface, using NEL-2400T cross-flow CO 2 The laser is used for laser cladding, and the process parameters are: laser power 1.9KW, scanning speed 200mm / min, spot diameter 2mm.
[0026] The coating structure obtained in this embodiment is dense and the interface is tightly bonded ( figure 1 ), the coating and the substrate have obvious and gradient element diffusion ( figure 2 ). The hardness of the coating along the cross-section changes little, and the average hardness HV850 is 142% higher than that of the substrate HV350 ( image 3 ).
Embodiment 2
[0028] This embodiment is similar to the embodiment, except that the laser used is a YLS-6000 fiber laser, and the laser process parameters are: laser power 1.9 KW, scanning speed 300 mm / min, spot diameter 2 mm.
[0029] The coating structure obtained in this embodiment is uniform and dense, without obvious cracks and holes ( Figure 4 ).
Embodiment 3
[0031] This embodiment is similar to the embodiment, except that the laser used is a YLS-6000 fiber laser, and the laser process parameters are: laser power 1.8KW, scanning speed 300 mm / min, spot diameter 2mm.
[0032] The coating structure obtained in this embodiment is uniform and dense, without obvious cracks and holes ( Figure 5 ).
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Abstract
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