3D printing aluminum-lithium alloy and application thereof
A technology for printing aluminum and lithium alloys, which is applied in metal processing equipment, transportation and packaging, and additive manufacturing. It can solve the problems of insufficient advantages, large solidification stress, and limited printing materials, and achieve low-cost effects.
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Embodiment 1
[0047] A 3D printing aluminum-lithium alloy, the ratio of elements in mass percent is: Li 2.5%, Zn 6.0%, Cu2.4%, Mg 2.5%, Zr 0.10%, Fe 0.02%, Si 0.01%, Na 0.0003% , Ca 0.0005%, H0.0005%, the balance is Al;
[0048] This embodiment also provides the use of powder bed electron beam 3D printing technology (SEBM) to use 3D printing aluminum-lithium alloys for making aircraft head components, and its application method includes the following steps:
[0049] (1) Batching: take metal raw materials according to the above-mentioned alloy mass percentage and carry out batching;
[0050] (2) Billet preparation: melt the ingredients in a 50kg class vacuum induction melting furnace, use a graphite crucible, vacuum degree 1000Pa, melting temperature 760°C, pouring temperature 700°C, pour into a metal mold with a diameter of 80mm to obtain an ingot ;
[0051] (3) Annealing and elongation deformation: the ingot is subjected to homogenization annealing, the annealing temperature is 510°C, an...
Embodiment 2
[0060] A 3D printing aluminum-lithium alloy, the ratio of elements in mass percent is: Li 2.9%, Zn 5.5%, Cu2.0%, Mg 2.6%, Zr 0.12%, Fe 0.02%, Si 0.01%, Na 0.0004% , Ca 0.0005%, H0.0007%, the balance is Al;
[0061] This embodiment also provides the use of powder bed electron beam 3D printing technology (SEBM) to use 3D printing aluminum-lithium alloys for making aircraft connector rear covers, and its application method includes the following steps:
[0062] (1) Batching: take metal raw materials according to the above-mentioned and alloy mass percentages and carry out batching;
[0063] (2) Billet preparation: melt the ingredients in a 30kg class vacuum induction melting furnace, use a graphite crucible, vacuum degree 1000Pa, melting temperature 760°C, pouring temperature 700°C, pour into a metal mold with a diameter of 50mm to obtain an ingot ;
[0064] (3) Annealing and extrusion deformation: The ingot is subjected to homogenization annealing at a temperature of 510°C for...
Embodiment 3
[0073] The national standard 2195 and 1420 aluminum-lithium alloy formulations are used, and the remaining implementation methods are the same as in Example 2; at the same time, the aluminum-lithium alloy is also used to make a connector back cover for an aircraft, and the quality and performance are shown in Table 3.
[0074] table 3
[0075]
[0076] It can be seen from Table 3 that the alloy in the present invention can obtain defect-free aircraft components through 3D printing, while the two most widely used aluminum-lithium alloys in the world, 2195 and 1420 aluminum-lithium alloys, have many components after printing. Cannot be used as a product. Table 3 compares the structure and performance of the printed parts. Obviously, the density, density, strength, grain size and grain characteristics of the aluminum-lithium alloy printed components of the present invention are significantly better than 2195 and 1420 aluminum-lithium alloys. The alloy and its preparation meth...
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Abstract
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