CN111020325A - Corrosion-resistant magnesium-lithium alloy - Google Patents

Corrosion-resistant magnesium-lithium alloy Download PDF

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Publication number
CN111020325A
CN111020325A CN201911308707.8A CN201911308707A CN111020325A CN 111020325 A CN111020325 A CN 111020325A CN 201911308707 A CN201911308707 A CN 201911308707A CN 111020325 A CN111020325 A CN 111020325A
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China
Prior art keywords
lithium alloy
magnesium
corrosion
alloy
percent
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CN201911308707.8A
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Chinese (zh)
Inventor
常萌蕾
陈东初
魏红阳
陆稼聪
田耕宇
李华军
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Foshan University
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Foshan University
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Priority to CN201911308707.8A priority Critical patent/CN111020325A/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

Abstract

The invention discloses a corrosion-resistant magnesium-lithium alloy which comprises the following components in percentage by weight: 8.1-11.9% of Li, 1.3-2.4% of Zr, 0.1-0.9% of Ce, 0.3-0.9% of Nd, 0.9-1.5% of La and the balance of Mg. According to the invention, three rare earth elements, namely Ce, Nd and La, are added into the magnesium-lithium alloy, so that the mechanical property of the magnesium-lithium alloy is ensured, and the corrosion resistance of the magnesium-lithium alloy is improved.

Description

Corrosion-resistant magnesium-lithium alloy
Technical Field
The invention belongs to the technical field of metal materials, and particularly relates to a corrosion-resistant magnesium-lithium alloy.
Background
The alloy obtained by taking magnesium and lithium as main alloy elements and adding other alloying elements on the basis is called magnesium-lithium alloy, and the density of the alloy is generally 1.35-1.65 g/cm3The density is 1/5 of steel and 1/2 of aluminum alloy, which are true, the density of magnesium-lithium alloy can be even lower than 1.0g/cm when the lithium content is higher3Gold known as being able to float on waterBelongs to the field of medicine.
The magnesium-lithium alloy material has excellent mechanical properties of low density, high specific stiffness and high specific strength by adding metallic lithium into magnesium, the structure of the magnesium-lithium alloy also changes remarkably with the change of lithium content, when the lithium content is lower than 5.7%, the alloy is α (Mg) single-phase structure, the crystal structure is a close-packed hexagonal structure (HCP), when the lithium content is higher than 10.3%, the alloy is β (Li) single-phase structure, the crystal structure is a body-centered cubic structure (BCC), and when the lithium content is 5.7-10.3%, the alloy is α (Mg) + β (Li) double-phase structure.
Besides the ultra-light characteristics, the magnesium-lithium alloy also has the following characteristics:
(1) because the addition of lithium can reduce the c/a axial ratio of magnesium lattice and improve the symmetry of close-packed hexagonal lattice on one hand, and β (Li) of body-centered cubic lattice appears when the lithium content is higher on the other hand, the plastic deformation capability of the magnesium-lithium alloy is obviously better than that of the common magnesium alloy;
(2) high specific strength and specific stiffness;
(3) the penetration resistance of high-energy particles is strong, and the electromagnetic shielding performance is excellent;
(4) the low-temperature mechanical property is good;
(5) the cutting processing performance is good.
However, since magnesium and lithium are both active metals and are in a two-phase structure, corrosion is very likely to occur at the phase interface in the use environment to generate a galvanic cell, so that magnesium and lithium are constantly dissolved at the anode and H is present at the cathode2And precipitating to accelerate the corrosion of the alloy.
The magnesium-lithium alloy has poor corrosion resistance and can be seriously corroded when placed in normal temperature atmosphere. Furthermore, magnesium lithium alloys are very susceptible to stress corrosion cracking in humid atmospheres. The influence of alloying elements on the corrosion resistance of magnesium-lithium alloys is related to the lithium content.
Disclosure of Invention
The invention provides a corrosion-resistant magnesium-lithium alloy which has good corrosion resistance while ensuring good mechanical properties.
In order to achieve the technical purpose, the invention adopts the following technical scheme.
A corrosion resistant magnesium lithium alloy comprising the following components in weight percent: 8.1-11.9% of Li, 1.3-2.4% of Zr, 0.1-0.9% of Ce, 0.3-0.9% of Nd, 0.9-1.5% of La and the balance of Mg.
Further, the alloy comprises the following components in percentage by weight: 9.3 to 10.8 percent of Li, 1.6 to 2.4 percent of Zr, 0.3 to 0.8 percent of Ce, 0.4 to 0.6 percent of Nd, 0.9 to 1.5 percent of La and the balance of Mg.
Further, the alloy comprises the following components in percentage by weight: 9.3-10.8% of Li, 1.6-2.4% of Zr, 0.3-0.8% of Ce, 0.5% of Nd, 1.0% of La and the balance of Mg.
The preparation method of the corrosion-resistant magnesium-lithium alloy comprises the following steps:
(1) preparing raw materials according to the weight percentage of each component in the corrosion-resistant magnesium-lithium alloy;
(2) vacuum smelting is carried out on the prepared raw materials to obtain alloy melt, and then the alloy melt is cast into a mould to be cooled to obtain as-cast magnesium-lithium alloy;
(3) and (3) sequentially carrying out solid solution treatment and stress relief annealing on the as-cast magnesium-lithium alloy obtained in the step (2) to finally obtain the corrosion-resistant magnesium-lithium alloy.
Further, the cooling mode in the step (2) is furnace cooling.
Further, the specific contents of the solution treatment are as follows: heating the as-cast magnesium-lithium alloy to 643-667K, wherein inert gas is required to be used for protection in the heating process, then preserving heat for 5-11 hours, and then rapidly cooling in an organic medium.
Further, the specific content of the stress relief annealing is as follows: and heating the magnesium-lithium alloy subjected to the solution treatment to 527-553K, preserving the heat for 1-2 h, and cooling along with the furnace.
The invention has the beneficial effects that Ce is added into the magnesium-lithium alloy, and the alloy grains can be obviously refined, the refining effect of the Ce in the magnesium alloy is that the composition is supercooled due to the enrichment of the front edge of a solid/liquid interface in the solidification process of the Ce, and a new nucleation zone is formed in the supercooled zone to form fine isometric crystals;
the alloy is added with Nd, and the addition of Nd can obviously refine and improve the form and distribution of α -Mg crystal grains, thereby obviously reducing the corrosion rate of the magnesium-lithium alloy, improving the equilibrium potential and corrosion potential of the magnesium-lithium alloy, reducing corrosion current and improving the corrosion resistance of the magnesium-lithium alloy;
la is added into the alloy, the weight loss corrosion rate of the alloy can be obviously reduced, and the La can form a net-like β phase structure in the magnesium-lithium alloy, so that a relatively effective corrosion-resistant film is formed on the surface of the alloy in the corrosion process, and the corrosion resistance of the magnesium-lithium alloy is greatly improved.
Detailed Description
Example 1
A corrosion resistant magnesium lithium alloy comprising the following components in weight percent: 9.3 percent of Li, 1.6 percent of ZrC, 0.8 percent of Ce, 0.6 percent of Nd, 0.9 percent of La and the balance of Mg.
The preparation method of the corrosion-resistant magnesium-lithium alloy comprises the following steps:
(1) preparing raw materials according to the weight percentage of each component in the corrosion-resistant magnesium-lithium alloy;
(2) vacuum smelting is carried out on the prepared raw materials to obtain alloy melt, and then the alloy melt is cast into a mould to be cooled along with a furnace to obtain as-cast magnesium-lithium alloy;
(3) sequentially carrying out solid solution treatment on the as-cast magnesium-lithium alloy obtained in the step (2), wherein the specific process comprises the following steps: heating the as-cast magnesium-lithium alloy to 650K, wherein inert gas is required to be used for protection in the heating process, then preserving heat for 6 hours, and then rapidly cooling in an organic medium;
(4) then, carrying out stress relief annealing on the magnesium-lithium alloy subjected to the solution treatment, wherein the specific process comprises the following steps: and heating the magnesium-lithium alloy subjected to the solution treatment to 530K, preserving the heat for 1h, and cooling along with the furnace.
Example 2
A corrosion resistant magnesium lithium alloy comprising the following components in weight percent: 9.4 percent of Li, 2.0 percent of ZrC, 0.7 percent of Ce, 0.5 percent of Nd, 1.0 percent of La and the balance of Mg.
The preparation method of the corrosion-resistant magnesium-lithium alloy comprises the following steps:
(1) preparing raw materials according to the weight percentage of each component in the corrosion-resistant magnesium-lithium alloy;
(2) vacuum smelting is carried out on the prepared raw materials to obtain alloy melt, and then the alloy melt is cast into a mould to be cooled along with a furnace to obtain as-cast magnesium-lithium alloy;
(3) sequentially carrying out solid solution treatment on the as-cast magnesium-lithium alloy obtained in the step (2), wherein the specific process comprises the following steps: heating the as-cast magnesium-lithium alloy to 650K, wherein inert gas is required to be used for protection in the heating process, then preserving heat for 6 hours, and then rapidly cooling in an organic medium;
(4) then, carrying out stress relief annealing on the magnesium-lithium alloy subjected to the solution treatment, wherein the specific process comprises the following steps: and heating the magnesium-lithium alloy subjected to the solution treatment to 530K, preserving the heat for 1h, and cooling along with the furnace.
Example 3
A corrosion resistant magnesium lithium alloy comprising the following components in weight percent: 10.9 percent of Li, 2.1 percent of ZrC, 0.8 percent of Ce, 0.5 percent of Nd, 1.1 percent of La and the balance of Mg.
The preparation method of the corrosion-resistant magnesium-lithium alloy comprises the following steps:
(1) preparing raw materials according to the weight percentage of each component in the corrosion-resistant magnesium-lithium alloy;
(2) vacuum smelting is carried out on the prepared raw materials to obtain alloy melt, and then the alloy melt is cast into a mould to be cooled along with a furnace to obtain as-cast magnesium-lithium alloy;
(3) sequentially carrying out solid solution treatment on the as-cast magnesium-lithium alloy obtained in the step (2), wherein the specific process comprises the following steps: heating the as-cast magnesium-lithium alloy to 650K, wherein inert gas is required to be used for protection in the heating process, then preserving heat for 6 hours, and then rapidly cooling in an organic medium;
(4) then, carrying out stress relief annealing on the magnesium-lithium alloy subjected to the solution treatment, wherein the specific process comprises the following steps: and heating the magnesium-lithium alloy subjected to the solution treatment to 530K, preserving the heat for 1h, and cooling along with the furnace.

Claims (7)

1. A corrosion resistant magnesium lithium alloy, wherein the alloy comprises the following components in weight percent: li8.1-11.9%, Zr 1.3-2.4%, Ce 0.1-0.9%, Nd 0.3-0.9%, La 0.9-1.5%, and the balance Mg.
2. The corrosion-resistant magnesium-lithium alloy according to claim 1, wherein said alloy comprises the following components in weight percent: 9.3 to 10.8 percent of Li, 1.6 to 2.4 percent of Zr, 0.3 to 0.8 percent of Ce, 0.4 to 0.6 percent of Nd, 0.9 to 1.5 percent of La0, and the balance of Mg.
3. The corrosion-resistant magnesium-lithium alloy according to claim 1, wherein said alloy comprises the following components in weight percent: 9.3-10.8% of Li, 1.6-2.4% of Zr, 0.3-0.8% of Ce, 0.5% of Nd, 1.0% of La and the balance of Mg.
4. The method for preparing the corrosion-resistant magnesium-lithium alloy according to any one of claims 1 to 3, which is characterized by comprising the following steps:
(1) preparing raw materials according to the weight percentage of each component in the corrosion-resistant magnesium-lithium alloy;
(2) vacuum smelting is carried out on the prepared raw materials to obtain alloy melt, and then the alloy melt is cast into a mould to be cooled to obtain as-cast magnesium-lithium alloy;
(3) and (3) sequentially carrying out solid solution treatment and stress relief annealing on the as-cast magnesium-lithium alloy obtained in the step (2) to finally obtain the corrosion-resistant magnesium-lithium alloy.
5. The method for preparing the corrosion-resistant magnesium-lithium alloy according to claim 4, wherein the cooling manner in the step (2) is furnace cooling.
6. The preparation method of the corrosion-resistant magnesium-lithium alloy according to claim 4, wherein the solution treatment specifically comprises: heating the as-cast magnesium-lithium alloy to 643-667K, wherein inert gas is required to be used for protection in the heating process, then preserving heat for 5-11 hours, and then rapidly cooling in an organic medium.
7. The preparation method of the corrosion-resistant magnesium-lithium alloy according to claim 4, wherein the stress relief annealing comprises the following specific contents: and heating the magnesium-lithium alloy subjected to the solution treatment to 527-553K, preserving the heat for 1-2 h, and cooling along with the furnace.
CN201911308707.8A 2019-12-18 2019-12-18 Corrosion-resistant magnesium-lithium alloy Pending CN111020325A (en)

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Cited By (1)

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CN113355570A (en) * 2021-06-23 2021-09-07 西安四方超轻材料有限公司 High-elongation soluble magnesium-lithium alloy material and preparation method thereof

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113355570A (en) * 2021-06-23 2021-09-07 西安四方超轻材料有限公司 High-elongation soluble magnesium-lithium alloy material and preparation method thereof

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