Heat treatment method for improving SLM forming TC4 strength-plasticity matching performance
A heat treatment method and matching performance technology, applied in the direction of energy efficiency improvement, process efficiency improvement, additive manufacturing, etc., can solve the problems of plasticity difference, strength-plasticity matching performance difficult to meet the requirements of industrial engineering applications, and small plasticity improvement.
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Embodiment 1
[0030] The Ti-6Al-4V powder particles with an average particle size of 45 μm and the composition shown in the parameter attached table 1 are used as the raw material for SLM forming. According to the process parameters shown in the parameter attached table 2, the forming size specification is 644mm, and the diameter of the working section is 3mm. Tensile specimen with a gauge length of 15mm, the specific size parameters are attached figure 2 .
[0031] Parameter Schedule 1
[0032]
[0033] Parameter Schedule 2
[0034]
[0035]
[0036] Use the wire cutting process to separate the tensile sample from the substrate, and then uniformly dip-coat a layer with a thickness of 0.2-0.3mm on the surface of the tensile sample, bonded by alumina, silicon oxide, boron carbide refractory and silicate High temperature anti-oxidation coating composed of additives.
[0037] Put the sample coated with high-temperature anti-oxidation coating into a vacuum atmosphere furnace, evacu...
Embodiment 2
[0044] The Ti-6Al-4V powder particles with an average particle size of 45 μm and the composition shown in the parameter attached table 1 are used as the raw material for SLM forming. According to the process parameters shown in the parameter attached table 2, the forming size specification is 644mm, and the diameter of the working section is 3mm. Tensile specimen with a gauge length of 15mm, the specific size parameters are attached figure 2 .
[0045] Parameter Schedule 1
[0046]
[0047] Parameter Schedule 2
[0048]
[0049]Use the wire cutting process to separate the tensile sample from the substrate, and then uniformly dip-coat a layer with a thickness of 0.2-0.3mm on the surface of the tensile sample, bonded by alumina, silicon oxide, boron carbide refractory and silicate High temperature anti-oxidation coating composed of additives.
[0050] Put the sample coated with high-temperature anti-oxidation coating into a vacuum atmosphere furnace, evacuate until the...
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