Method for brazed connection of C/C composite material through high-entropy alloy
A technology of composite materials and high-entropy alloys, applied in welding equipment, metal processing equipment, manufacturing tools, etc., can solve problems such as difficult wetting, poor high-temperature mechanical properties of joints, and large residual stress, so as to reduce residual stress and relieve residual stress. effects of stress, good wetting
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Embodiment 1
[0029] Using AlCoCrFeNi 2.1 The method for high-entropy alloy brazing C / C composite material, the steps are as follows:
[0030] 1) Use 800#, 2000# SiC sandpaper to grind the surface of the C / C composite material to be brazed step by step, and place it on a polishing machine, polish it with a diamond suspension with a particle size of 1 μm until there is no trace, and then place it Ultrasonic cleaning in acetone, and finally drying to complete the surface treatment;
[0031] 2) According to AlCoCrFeNi 2.1 The atomic ratio of each metal raw material in the high-entropy alloy, the metal raw material powders are mixed together according to the ratio to form a powder raw material; the powder raw material is suspended and smelted at a temperature of 1350 ° C, and the powder raw material is smelted into a solder alloy ingot , and then repeated smelting 4 times to make a solder alloy ingot with uniform composition;
[0032] 3) Cut the solder alloy ingot obtained in step 2) into 0....
Embodiment 2
[0037] Using AlCoCrFeNi 2.1 The method of high-entropy alloy brazing C / C composite materials, the operation steps are repeated in Example 1, the only difference is that "in step 5), the brazing temperature is replaced from 1350°C to 1380°C", other conditions and examples 1 is the same, and the final preparation uses AlCoCrFeNi 2.1 Joints of C / C composites brazed with high-entropy alloys.
Embodiment 3
[0039] Using AlCoCrFeNi 2.1 The method of high-entropy alloy brazing C / C composite materials, the operation steps are repeated in Example 1, the only difference is that "in step 5), the brazing temperature is replaced from 1350°C to 1410°C", other conditions and examples 1 is the same, and the final preparation uses AlCoCrFeNi 2.1 Joints of C / C composites brazed with high-entropy alloys. The shape of the joint is as figure 2 shown.
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