Aluminum magnesium containing alloy materials

A lithium-magnesium alloy and alloy technology, applied in the field of lithium-magnesium alloy materials, can solve the problems of few β single-phase alloy research reports, no commercial alloy data, poor thermal stability, etc., and achieve good plasticity, low density, high ratio the effect of strength

Inactive Publication Date: 2006-10-25
BEIHANG UNIV
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The current research on Mg-Li alloys is limited to α single-phase alloys or α+β dual-phase alloys, and there are few research reports on β single-phase alloys, and there are no relevant commercial alloys.
The Mg-Li alloy β single-

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0015] The above-mentioned components are prepared using the following preparation methods to prepare lithium-containing magnesium alloy materials, and the steps are as follows:

[0016] (1) Take out the alloy elements according to the proportioning scale;

[0017] (2) Smelting alloys by smelting methods;

[0018] (3) Pouring into ingots in a protective atmosphere;

[0019] (4) Peel the ingot;

[0020] (5) Carry out the homogenization treatment of the stripped ingot at 350℃±10℃ / 24h;

[0021] (6) Homogenize the ingot after homogenization treatment at 430℃±10℃ / 48h;

[0022] (7) The processed ingot is deformed into a product at room temperature or 250°C±5°C.

[0023] The performance test is performed on the lithium-containing magnesium alloy material prepared by the above method, and the test is carried out with a gold image microscope, MTS material mechanical property testing machine, and one-tenths balance equipment, and the tensile strength of the lithium-containing magnesium all

Example Embodiment

[0025] Example 1: To prepare 100 kilograms of lithium-containing magnesium alloy materials according to the following ratio, the elements to be taken out are:

[0026] Lithium (Li) 15 kg, aluminum (Al) 5 kg, zinc (Zn) 1 kg, zirconium (Zr) 0.80 kg, rare earth element rhenium (Re) 1.2 kg and the balance magnesium (Mg).

[0027] The preparation method includes smelting the weighed elements at a melting temperature of 680°C, and pouring them into an ingot under an argon atmosphere. The ingot is stripped with a machine tool and an acid solution to obtain a clean surface. The ingots are homogenized at 350℃±10℃ / 24h, and the homogenized ingots are then homogenized at 430℃±10℃ / 48h. The homogenized ingots are at room temperature or 250 Under the condition of ℃±5℃, it can be processed into products after forging or rolling deformation.

[0028] The product was kept at a temperature of 250°C for 4 hours and then taken out. It can meet the general performance requirements. HV-10A small load V

Example Embodiment

[0029] Example 2: To prepare 100 kilograms of lithium-containing magnesium alloy materials according to the following ratio, the elements to be taken out are:

[0030] 10 kg of lithium (Li), 4.5 kg of aluminum (Al), 1 kg of zinc (Zn), 0.80 kg of zirconium (Zr), 1.2 kg of rare earth element rhenium (Re) and the balance of magnesium (Mg).

[0031] The preparation method includes smelting the elements weighed out above at a smelting temperature of 720°C, and smelting them in SF 6 The ingot is poured into an ingot under the protective environment of mixed gas, and the ingot is stripped with a machine tool and acid solution to obtain a clean surface, and the stripped ingot is subjected to a homogenization treatment at 350℃±10℃ / 24h. After homogenization treatment The ingot is homogenized at 430℃±10℃ / 48h, and the homogenized ingot is processed into products by forging or rolling deformation at room temperature or 250℃±5℃.

[0032] The product was kept at a temperature of 250°C for 4 hou

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Abstract

The invention discloses a lithium-containing magnesium alloy material, which is a single-phase alloy of Mg-Li alloy in the β-phase region. Aluminum (Al), 1.0%-4.0% zinc (Zn), 0.4%-1.5% zirconium (Zr), 1.2%-5.5% rare earth rhenium (Re) and the rest magnesium (Mg). The material tensile strength of the present invention is σ b =180~280Mpa, the yield strength is σ s =130~260Mpa, elongation δ=15~68%, density 1.31~1.60.

Description

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Claims

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Application Information

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Owner BEIHANG UNIV
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