Light magnesium alloy and method for forming the same

Abstract

A magnesium alloy includes Mg, 1 to 12 wt % of Li, 1 to 10 wt % of Al and 0.2 to 3 wt % of Zn. The magnesium alloy has a microstructure which includes a nanoscale reinforcement phase, wherein the nanoscale reinforcement phase is a Li—Al compound.

Description

This application claims the benefit of Taiwan application Serial No. 105100403, filed on Jan. 7, 2016, the disclosure of which is incorporated by reference herein in its entirety.

TECHNICAL FIELD

The disclosure relates to an alloy and a method for manufacturing the same, and particularly to a magnesium alloy and a method for manufacturing the same.

BACKGROUND

High specific strength (i.e. the value of the strength of a material divided by its density) is a requirement of a metal material. The magnesium alloy has a low density, and thereby intrinsically provides a higher specific strength. Therefore, it is desired to further improve the strength and decrease the density of a magnesium alloy.

SUMMARY

According to some embodiments, a magnesium alloy is provided. The magnesium alloy includes magnesium (Mg), 1 to 12 wt % of lithium (Li), 1 to 10 wt % of aluminum (Al), and 0.2 to 3 wt % of zinc (Zn). The magnesium alloy has a microstructure which include a nanoscale reinforcement phase, and the nanoscale reinforcement phase is a Li—Al compound.

According to some embodiments, a method for manufacturing a magnesium alloy is provided. The method includes following steps. First, a magnesium alloy is formed by casting, wherein the magnesium alloy includes magnesium (Mg), 1 to 12 wt % of lithium (Li), 1 to 10 wt % of aluminum (Al), and 0.2 to 3 wt % of zinc (Zn). Then, a series of thermo-mechanical treatments are performed on the magnesium alloy to form a nanoscale reinforcement phase on the magnesium alloy, wherein the nanoscale reinforcement phase is a Li—Al compound.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a flowchart of a method for manufacturing a magnesium alloy according to embodiments.

FIGS. 2A-2E show analysis results of ALZ771 processed by a solid solution treatment and an optional aging treatment.

FIGS. 3A-3B show analysis results of ALZ771 processed by a thixomolding treatment and an optional aging treatment.

In the following detailed description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the disclosed embodiments. It will be apparent, however, that one or more embodiments may be practiced without these specific details.

In other instances, well-known structures and devices are schematically shown in order to simplify the drawing.

DETAILED DESCRIPTION

The disclosure relates to a magnesium alloy and a method for manufacturing the same. Through the reinforcement phase existing in the microstructure, properties of the magnesium alloy, such as the strength of the magnesium alloy, can be further enhanced. The magnesium alloy includes magnesium (Mg), 1 to 12 wt % of lithium (Li), 1 to 10 wt % of aluminum (Al), and 0.2 to 3 wt % of zinc (Zn). The microstructure of the magnesium alloy includes a nanoscale reinforcement phase, which is a Li—Al compound.

Magnesium is the main element of the magnesium alloy. That is, other than the compositions indicated in the disclosure, the remaining portion of the magnesium alloy is provided by magnesium. Using magnesium as the main element makes the magnesium alloy possess lightweight. The addition of lithium to the magnesium alloy can increase heat treatability and reduce the density of the magnesium alloy. The addition of aluminum, particularly under the conditions of solid solution, can increase the strength of the magnesium alloy at a room temperature. The addition of a small amount of zinc can improve the corrosion resistance of the magnesium alloy. In one embodiment, the magnesium alloy may include magnesium (Mg), 4 to 12 wt % of lithium (Li), 4 to 9 wt % of aluminum (Al), and 0.2 to 3 wt % of zinc (Zn). According to one embodiment, The magnesium alloy may further include other compositions, such as ≤0.3 wt % of manganese (Mn) and ≤0.2 wt % of silicon (Si). The addition of a small amount of manganese can improve the corrosion resistance of the magnesium alloy. The addition of a small amount of silicon can improve the strength of the magnesium alloy.

The properties of the magnesium alloy can be improved through suitably adjusting the structure of a nanoscale reinforcement phase as disclosed herein. For example, given that the nanoscale reinforcement phase exists, the yield strength can be increased by about 5 to 150%. Besides, a higher level of hardness can be achieved if the nanoscale reinforcement phase has a suitable size.

Specifically, the nanoscale reinforcement phase may include a plurality of particle structures and/or a plurality of rod structures. In one embodiment, the particle structures have a diameter of 3 to 900 nm. In one embodiment, the particle structures have a diameter of 3 to 500 nm. In one embodiment, the particle structures have a diameter of 3 to 20 nm. In one embodiment, the rod structures have a diameter of 15 to 70 nm and a length of 500 to 2,000 nm. In one embodiment, the rod structures have a diameter of 50 to 150 nm and a length of 1,500 to 3,300 nm. In one embodiment, the rod structures have a diameter of 100 to 700 nm and a length of 2,500 to 10,000 nm. In one embodiment, the rod structures have a diameter of 3 to 15 nm and a length of 60,000 to 150,000 nm.

In some embodiments, in addition to the Li—Al compound as described above, the magnesium alloy may further include at least another nanoscale reinforcement phase, which is selected from a group composed of: Mg—Li compound, Mg—Al compound (such as Mg₁₇A1₁₂ phase), and Mg—Li—Al compound (such as MgLi₂A1 phase). In some embodiments, a small amount of other elements may solidly dissolve in the Li—Al compound and these compounds. Here, a “compound” may also be referred as a “phase”.

Embodiments of a method for manufacturing a magnesium alloy are described below. However, the embodiments are for explanatory and exemplary purposes only, not for limiting the scope of the invention. Referring to FIG. 1, a flowchart of a method for manufacturing a magnesium alloy according to embodiments is shown. In the step 101, a magnesium alloy is formed by casting. The magnesium alloy may have any one of the composition proportions as described above. For example, the magnesium alloy may include magnesium (Mg), 1 to 12 wt % of lithium (Li), 1 to 10 wt % of aluminum (Al), and 0.2 to 3 wt % of zinc (Zn). In the step 102, a thermo-mechanical treatment is performed on the magnesium alloy to from a desired nanoscale reinforcement phase in the magnesium alloy. The nanoscale reinforcement phase at least includes a lithium-aluminum phase, and may also include other types of nanoscale reinforcement phase, such as a Mg—Li phase, a Mg—Al phase, and/or a Mg—Li—Al phase.

Specifically, the thermo-mechanical treatment can be selected from at least one of: a solid solution treatment, a homogenization treatment, an aging treatment, a T5 heat treatment, a T6 heat treatment, a thixomolding treatment, a semi-solid metal casting treatment, an extrusion treatment, a forging treatment, and a rolling treatment. In one embodiment, the thermo-mechanical treatment includes a solid solution treatment and an aging treatment. In one embodiment, the thermo-mechanical treatment includes performing an aging treatment at 30 to 350° C. for 0.1 to 350 hr. In one embodiment, the thermo-mechanical treatment includes a thixomolding treatment.

Through the thermo-mechanical treatment, the nanoscale reinforcement phase can be formed and/or adjusted. In particular, the size of the nanoscale reinforcement phase can be adjusted. As such, the magnesium alloy can have better properties. In some experimental examples, the magnesium alloy obtained from the step 101 can have a yield strength of about 150 MPa. After the step 102 (such as a rolling treatment or a thixomolding treatment, the yield strength can further be increased to over 300 MPa.

A number of experimental examples of the magnesium alloy having nanoscale reinforcement phase are provided below. The exemplary magnesium alloy includes magnesium (Mg), 7 wt % of lithium (Li), 7 wt % of aluminum (Al), and 1 wt % of zinc (Zn), and is referred as ALZ771 hereinafter.

FIGS. 2A-2E show analysis results of ALZ771 processed by a solid solution and an optional aging treatment with various aging time at 100° C. According to the results of X-ray diffraction (XRD, D8, Bruker), as shown in FIG. 2A, the ALZ771 processed by the solid solution and the optional aging treatment with various aging time at 100° C. includes Li—Al phase, as indicated by the arrow 201. ALZ771 also includes MgLi₂A1 phase, as indicated by the arrow 202. FIG. 2B shows the microstructure of the ALZ771 after the solid solution treatment, which is observed using a scanning electron microscope (SEM, Inspect F, FEI). It can be seen that the microstructure includes rod structures of Li—Al phase, and the rod structures have a diameter of 15 to 70 nm and a length of 500 to 2,000 nm and are distributed in the α phase, as indicated by the arrow 203. FIG. 2C shows the microstructure of the ALZ771 after the solid solution treatment and the aging treatment at 100° C. for 1 hr, which is observed using the SEM. It can be seen that the microstructure includes rod structures of Li—Al phase, and the rod structures have a diameter of 50 to 150 nm and a length of 1,500 to 3,300 nm and are distributed in the α phase, as indicated by the arrow 204. FIG. 2D shows the microstructure of the ALZ771 after the solid solution treatment and the aging treatment at 100° C. for 41 hr, which is observed using the SEM. It can be seen that the microstructure includes rod structures of Li—Al phase, and the rod structures have a diameter of 100 to 700 nm and a length of 2,500 to 10,000 nm and are distributed in the α phase, as indicated by the arrow 205. FIG. 2E shows the results of Vickers hardness test (Hv hardness, HM-100 Series, Miztoyo). As shown in FIG. 2Em the hardness of ALZ771 can be further increased through a suitable aging treatment. It should be noted that improvement in the hardness of ALZ771 is most significant when ALZ771 is optionally processed with an aging treatment at 100° C. for 41 hr.

FIGS. 3A-3B show analysis results of ALZ771 processed by a thixomolding solution and an optional aging treatment. According to the results of XRD, as shown in FIG. 3A, the ALZ771 processed by the thixomolding solution and the optional aging treatment includes Li—Al phase, as indicated by the arrow 301. ALZ771 also includes MgLi₂A1 phase and Mg₁₇A1₁₂ phase, as indicated by the arrows 302 and 303, respectively. FIG. 3B shows the microstructure of the ALZ771 after the thixomolding, which is observed using the SEM. It can be seen that the microstructure includes particle structures of Li—Al phase, and the particle structures have a diameter of 3 to 20 nm, as indicated by the arrow 304. The microstructure also includes rod structures of Li—Al phase, and the rod structures have a diameter of 3 to 15 nm and a length of 60,000 to 150,000 nm, as indicated by the arrow 305. Both of the particle structures and the rod structures are distributed in the α phase. Further, the yield strength is tested using a tensile test. After the thixomolding treatment, the yield strength of ALZ771 is increased from 99.3 MPa, which is measured after the casting step, to 122.2 MPa. The yield strength is also tested using a bending test. After the thixomolding treatment, the yield strength of ALZ771 is increased from 341.7 MPa, which is measured after the casting step, to 361 MPa. That is, forming and/or adjusting the nanoscale reinforcement phase through a thermo-mechanical treatment, such as a thixomolding treatment, can increase the strength of the magnesium alloy.

It will be apparent to those skilled in the art that various modifications and variations can be made to the disclosed embodiments. It is intended that the specification and examples be considered as exemplary only, with a true scope of the disclosure being indicated by the following claims and their equivalents.

Claims

1. A magnesium alloy, comprising: magnesium (Mg);7 wt % of lithium (Li);7 wt % of aluminum (Al); and1 wt % of zinc (Zn);wherein the magnesium alloy has a microstructure which comprises a nanoscale reinforcement phase, and the nanoscale reinforcement phase is a Li—Al compound.

2. The magnesium alloy according to claim 1, wherein the nanoscale reinforcement phase comprises a plurality of particle structures and/or a plurality of rod structures.

3. The magnesium alloy according to claim 2, wherein the particle structures have a diameter of 3 to 900 nm.

4. The magnesium alloy according to claim 2, wherein the particle structures have a diameter of 3 to 500 nm.

5. The magnesium alloy according to claim 2, wherein the particle structures have a diameter of 3 to 20 nm.

6. The magnesium alloy according to claim 2, wherein the rod structures have a diameter of 15 to 70 nm and a length of 0.5 to 2 μm.

7. The magnesium alloy according to claim 2, wherein the rod structures have a diameter of 50 to 150 nm and a length of 1.5 to 3.3 μm.

8. The magnesium alloy according to claim 2, wherein the rod structures have a diameter of 100 to 700 nm and a length of 2.5 to 10 μm.

9. The magnesium alloy according to claim 2, wherein the rod structures have a diameter of 3 to 15 nm and a length of 60 to 150 μm.

10. The magnesium alloy according to claim 1, further comprising at least another nanoscale reinforcement phase selected from a group composed of: a Mg—Li phase, a Mg—Al phase, and a Mg—Li—Al phase.

11. The magnesium alloy according to claim 1, further comprising: ≤0. 3 wt % of manganese (Mn); and≤0.2 wt % of silicon (Si).

12. A method for manufacturing a magnesium alloy, comprising: forming a magnesium alloy by casting, wherein the magnesium alloy comprises: magnesium (Mg);7 wt % of lithium (Li);7 wt % of aluminum (Al); and1 wt % of zinc (Zn); andperforming a thermo-mechanical treatment on the magnesium alloy to form a nanoscale reinforcement phase in the magnesium alloy, wherein the nanoscale reinforcement phase is a Li—Al compound.

13. The method according to claim 12, wherein the thermo-mechanical treatment is selected from at least one of: a solid solution treatment, a homogenization treatment, an aging treatment, a T5 heat treatment, a T6 heat treatment, a thixomolding treatment, a semi-solid metal casting treatment, an extrusion treatment, a forging treatment, and a rolling treatment.

14. The method according to claim 12, wherein the thermo-mechanical treatment comprises performing an aging treatment at 30 to 350° C. for 0.1 to 350 hr.