Boron carbide aluminum matrix composite material and preparation method thereof
A technology of boron carbide aluminum and composite materials, which is applied in anodic oxidation, reactors, nuclear engineering, etc., can solve the problems that aluminum substrates are prone to corrosion, damage the mechanical properties of materials, and complex processes, etc., and achieve good r-ray and neutron absorption performance , to avoid corrosion, the effect of a wide range of application prospects
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[0035] Example 1
[0036] The mass percentage of the boron carbide aluminum-based composite material provided in this embodiment is: nuclear grade boron carbide powder: 5%, and 6061 aluminum alloy powder: 95%.
[0037] The preparation method of the boron carbide aluminum-based composite material of this embodiment is as follows figure 1 As shown, including the following steps:
[0038] (1) The raw material powder preparation step: mix 950g 6061 aluminum alloy powder with a particle size of 0.5μm nuclear grade boron carbide powder 50g and a particle size of 100μm, and the mixing time is 8 hours to obtain 1000g mixed powder;
[0039] (2) Hot isostatic pressing step: put the mixed powder into a sheath, vacuum exhaust temperature is 200℃, sealed, hot isostatic pressing treatment, pressing pressure is 80MPa, temperature is 400℃, holding time is 1 hour, get hot isostatic pressing blank;
[0040] (3) Machining steps: the hot isostatic pressing blanks are removed from the jacket, and processed...
Example Embodiment
[0043] Example 2
[0044] The mass percentage of the boron carbide aluminum-based composite material provided in this embodiment is: nuclear grade boron carbide powder: 40%, and 6061 aluminum alloy powder: 60%.
[0045] The preparation method of the boron carbide aluminum-based composite material of this embodiment is as follows:
[0046] (1) The raw material powder preparation step: mix 950g 6061 aluminum alloy powder with a particle size of 75μm nuclear grade boron carbide powder and a particle size of 3μm 50g, and the mixing time is 24 hours to obtain 1000g of mixed powder;
[0047] (2) Hot isostatic pressing forming step: put the mixed powder into a sheath, vacuum exhaust temperature is 500 ℃, sealed, hot isostatic pressing treatment, pressing pressure is 150 MPa, temperature is 600 ℃, holding time is 4 hours, get hot isostatic pressing blank;
[0048] (3) Machining steps: the hot isostatic pressing blanks are removed from the jacket, and processed according to the requirements of ...
Example Embodiment
[0051] Example 3
[0052] The mass percentage of the boron carbide aluminum-based composite material provided in this embodiment is: nuclear grade boron carbide powder: 31%, and 6061 aluminum alloy powder: 69%.
[0053] The preparation method of the boron carbide aluminum-based composite material of this embodiment is as follows:
[0054] (1) The raw material powder preparation step: mix 950g 6061 aluminum alloy powder with a particle size of 25μm nuclear grade boron carbide powder and a particle size of 75μm 50g, and the mixing time is 15 hours to obtain 1000g of mixed powder;
[0055] (2) Hot isostatic pressing forming step: put the mixed powder into a sheath, vacuum exhaust temperature is 300 ℃, sealed, hot isostatic pressing treatment, pressing pressure is 130MPa, temperature is 500 ℃, holding time is 3 hours, get hot isostatic pressing blank;
[0056] (3) Machining steps: the hot isostatic pressing blanks are removed from the jacket, and processed according to the requirements of ...
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