Magnesium alloy having excellent mechanical properties and corrosion resistance and method for manufacturing the same

Patent metadata

Field	Value
Publication number	US-10947609-B2
Application number	US-201616066003-A
Country	US
Kind code	B2
Filing date	Nov 30, 2016
Priority date	Dec 28, 2015
Publication date	Mar 16, 2021
Grant date	Mar 16, 2021

Abstract

The present invention is to provide a magnesium alloy comprising 0.001 parts by weight to 1.0 parts by weight of scandium and the balance of magnesium and unavoidable impurities, based on 100 parts by weight of a magnesium alloy, wherein the magnesium alloy has increased Fe solubility and reduced corrosion while providing excellent mechanical properties and corrosion resistance, and a method for producing the same. The magnesium alloy of the present invention can improve the corrosion resistance of the magnesium alloy by using scandium which can simultaneously prevent from microgalvanic corrosion between a substrate and impurities without deteriorating mechanical properties and improve the passivation property of the coating formed on the surface.

First claim

What is claimed is:

1. A magnesium alloy comprising, with respect to 100 parts by weight of the magnesium alloy:
0.001 parts by weight to 1.0 parts by weight of scandium;
0.001 to 0.007 parts by weight of iron;
0.001 to 0.002 parts by weight of silicon;
0.005 to 0.015 parts by weight of calcium;
0.003 to 0.012 parts by weight of manganese; and
the balance of magnesium and unavoidable impurities,
wherein Fe solubility is increased and corrosion is reduced while mechanical properties and corrosion resistance are maintained.

2. The magnesium alloy of claim 1 , wherein the scandium is included in a range of 0.05 parts by weight to 0.5 parts by weight.

3. The magnesium alloy of claim 1 , wherein the magnesium alloy has a corrosion rate of 0.5 mm/y or less when immersed in 3.5 wt % salt water for 72 hours.

4. The magnesium alloy of claim 1 , wherein the magnesium alloy has a yield strength of 80 to 120 MPa, a tensile strength of 160 to 180 MPa, and an elongation of 6 to 13%.

5. The magnesium alloy of claim 1 , further comprising 0.5 to 7.0 parts by weight of zinc with respect to 100 parts by weight of the magnesium alloy.

6. The magnesium alloy of claim 5 , wherein the magnesium alloy has a yield strength of 120 to 190 MPa, a tensile strength of 210 to 310 MPa, and an elongation of 20 to 30%.

7. The magnesium alloy of claim 1 , further comprising 2.5 to 10 parts by weight of tin with respect to 100 parts by weight of the magnesium alloy.

8. The magnesium alloy of claim 7 , wherein the magnesium alloy has a yield strength of 130 to 280 MPa, a tensile strength of 210 to 310 MPa, and an elongation of 5 to 17%.

9. The magnesium alloy of claim 1 , further comprising 2 to 10 parts by weight of aluminum with respect to 100 parts by weight of the magnesium alloy.

10. The magnesium alloy of claim 9 , wherein the magnesium alloy has a yield strength of 130 to 200 MPa, a tensile strength of 230 to 320 MPa, and an elongation of 10 to 25%.

11. A method for producing the magnesium alloy of claim 1 , the method comprising:
casting an alloy, wherein the alloy comprises, with respect to 100 parts by weight of the alloy:
0.001 parts by weight to 1.0 parts by weight of scandium;
0.001 to 0.007 parts by weight of iron;
0.001 to 0.002 parts by weight of silicon;
0.005 to 0.015 parts by weight of calcium;
0.003 to 0.012 parts by weight of manganese; and
the balance of magnesium and unavoidable impurities;

homogenizing the cast alloy; and
extruding the homogenized magnesium alloy after pre-heating.

Assignees

• Korea Inst Mach & Materials
• Korea Institute Materials Science

Inventors

• Yim Chang-Dong
• You Bong-Sun
• Kim Ha-Sik
• Kim Young-Min
• Moon Byoung-Gi
• Bae Jun-Ho

Classifications

• C22C23/00 Primary

  Alloys based on magnesium · CPC title

• C22C23/04

  with zinc or cadmium as the next major constituent · CPC title

• C22C23/06 Primary

  with a rare earth metal as the next major constituent · CPC title

• C22C23/02

  with aluminium as the next major constituent · CPC title

• C22F1/06

  of magnesium or alloys based thereon · CPC title