IP Library Patent Application 10793412
Patent Application
App. No. 10/793,412

Magnesium wrought alloy having improved extrudability and formability

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Patent No.
US None
App. No.
10/793,412
Abstract

In one aspect, the invention provides a magnesium-based casting alloy having relatively high strength and castibility, as well as an improved ductility and extrudability for wrought alloy applications. The magnesium-based wrought alloy comprises aluminum (Al) of between about 2.5 to about 4.0 wt. %, manganese (Mn) of less than about 0.6 wt. %, zinc (Zn) of less than about 0.3 wt. %, other impurities of less than about 0.1 wt. %, and a balance of magnesium (Mg). The invention further provides methods of forming a wrought alloy component and automotive components formed therefrom.

Claims (62)

1 . A metal alloy comprising:

aluminum (Al) from about 2.5 to about 3.5 wt. %; manganese (Mn) from about 0.2 to about 0.6 wt. %; zinc (Zn) less than about 0.3 wt. %; one or more impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg).

2 . The metal alloy according to claim 1 , wherein said aluminum is about 3 wt. %.

3 . The metal alloy according to claim 1 , wherein said manganese is about 0.4 wt. %.

4 . The metal alloy according to claim 1 , wherein said composition comprises said aluminum (Al) of about 3 wt. %; said manganese (Mn) of about 0.4 wt. %; and said zinc (Zn) less than about 0.22 wt. %.

5 . The metal alloy according to claim 1 , wherein said one or more impurities comprise: silicon (Si) of less than about 0.01 wt. %, copper (Cu) of less than about 0.01 wt. %, nickel (Ni) of less than about 0.002 wt. %, iron (Fe) of less than about 0.002 wt. %, and one or more additional impurities of less than about 0.02wt. %.

6 . The metal alloy according to claim 1 , wherein the alloy has an elongation of greater than 8% at room temperature.

7 . The metal alloy according to claim 1 , wherein the alloy has an extrusion speed of greater than 305 mm per minute at 360° C.

8 . The metal alloy according to claim 1 , wherein the alloy has a yield strength of greater than about 165 MPa.

9 . The metal alloy according to claim 1 , wherein the alloy has an ultimate tensile strength of greater than about 230 MPa.

10 . The metal alloy according to claim 1 , wherein the alloy is corrosion resistant.

11 . A magnesium-based wrought alloy having a composition comprising:

aluminum (Al) of between about 2.5 to about 4.0 wt. %; manganese (Mn) and zinc (Zn) collectively present at less than about 1.0 wt. %; impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg).

12 . The magnesium-based wrought alloy according to claim 11 , wherein the composition comprises aluminum (Al) from about 2.5 to about 3.5 wt. %; manganese (Mn) from about 0.2 to 0.6 wt. %; zinc (Zn) less than about 0.3 wt. %; one or more impurities of less than about 0.1 wt. %; and a balance of magnesium (Mg).

13 . The magnesium-based wrought alloy according to claim 11 , wherein the composition comprises manganese (Mn) from about 0.26 wt. % to about 0.6 wt.%; and zinc (Zn) less than 0.22 wt. %.

14 . The magnesium-based wrought alloy according to claim 11 above, wherein said one or more impurities comprise: silicon (Si) of less than about 0.01 wt. %, copper (Cu) of less than about 0.01 wt. %, nickel (Ni) of less than about 0.002 wt. %, iron (Fe) of less than about 0.002 wt. %, and one or more additional impurities of less than about 0.02 wt. %.

15 . The magnesium-based wrought alloy according to claim 11 , wherein said aluminum is about 3 wt. %.

16 . The magnesium-based wrought alloy according to claim 11 , wherein said manganese is about 0.4 wt. %.

17 . The magnesium-based wrought alloy according to claim 11 , wherein the composition comprises said aluminum (Al) of about 3 wt. %; said manganese (Mn) from about 0.4 wt. %; said zinc (Zn) less than about 0.22 wt. %; said one or more impurities of less than about 0.1 wt. %; and a balance of said magnesium (Mg).

18 . The magnesium-based wrought alloy according to claim 11 , wherein the wrought alloy has an elongation of greater than 8% at room temperature.

19 . The magnesium-based wrought alloy according to claim 11 , wherein the wrought alloy has an extrusion speed of greater than 305 mm per minute at 360° C.

20 . The magnesium-based wrought alloy according to claim 11 , wherein the wrought alloy has a yield strength of greater than about 165 MPa.

21 . The magnesium-based wrought alloy according to claim 11 , wherein the wrought alloy has an ultimate tensile strength of greater than about 230 MPa.

22 . The magnesium-based wrought alloy according to claim 11 , wherein the wrought alloy is corrosion resistant.

23 . A method of forming a wrought alloy element comprising:

forming a molten alloy material having a composition comprising aluminum (Al) of less than about 4.0 wt. %; manganese (Mn) and zinc (Zn) collectively present at less than about 1.0 wt. %; one or more impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg), at a casting temperature;

cooling said alloy material to solidify; and

processing said solidified alloy material by deformation, thereby forming the wrought alloy element.

24 . The method according to claim 23 , wherein said composition comprises aluminum (Al) from about 2.5 to about 3.5 wt. %; manganese (Mn) from about 0.2 to about 0.6 wt. %; and zinc (Zn) less than about 0.3 wt. %.

25 . The method according to claim 23 , wherein said composition comprises manganese (Mn) from about 0.26 to about 0.6 wt. %; and zinc (Zn) less than about 0.22 wt. %.

26 . The method according to claim 23 above, wherein said one or more impurities comprise: silicon (Si) of less than about 0.01 wt. %, copper (Cu) of less than about 0.01 wt. %, nickel (Ni) of less than about 0.002 wt. %, iron (Fe) of less than about 0.002 wt. %, and additional impurities of less than about 0.02 wt. %.

27 . The method according to claim 23 , wherein said solidified alloy material comprises an ingot.

28 . The method according to claim 23 , wherein said solidified alloy material comprises a billet.

29 . The method according to claim 23 , wherein said casting temperature is greater than about 600° C.

30 . The method according to claim 23 , wherein said processing comprises a hot-working process.

31 . The method according to claim 23 , wherein said processing comprises a cold-working process.

32 . The method according to claim 23 , wherein said processing is selected from the group consisting of: extruding, rolling, bending, hydroforming, stamping, superplastic forming, gas forming, electromagnetic forming, and combinations thereof.

33 . The magnesium-based wrought alloy according to claim 23 , wherein said aluminum is about 3 wt. %.

34 . The method according to claim 23 , wherein said manganese is about 0.4 wt. %.

35 . The method according to claim 23 , wherein the composition comprises said aluminum (Al) of about 3 wt. %; said manganese (Mn) of about 0.4 wt. %; said zinc (Zn) less than about 0.22 wt. %; said one or more impurities of less than about 0.1 wt. %; and a balance of said magnesium (Mg).

36 . The method according to claim 23 , wherein said processed alloy material has an elongation of greater than 8% at room temperature.

37 . The method according to claim 23 , wherein said processed alloy material has an extrusion speed of greater than 305 mm per minute at 360° C.

38 . The method according to claim 23 , wherein said processed alloy material has a yield strength of greater than about 165 MPa.

39 . The method according to claim 23 , wherein said processed alloy material has an ultimate tensile strength of greater than about 230 MPa.

40 . The method according to claim 23 , wherein said processed alloy material is corrosion resistant.

41 . A component for use in a vehicle comprising a magnesium-based wrought alloy comprising aluminum (Al) of less than about 4.0 wt. %; manganese (Mn) and zinc (Zn) collectively present at less than about 1.0 wt. %; one or more impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg).

42 . The component according to claim 41 , wherein said alloy comprises aluminum (Al) from about 2.5 to about 3.5 wt. %; manganese (Mn) from about 0.2 to 0.6 wt. %; and zinc (Zn) less than about 0.3 wt. %.

43 . The component according to claim 41 , wherein said alloy comprises manganese (Mn) from about 0.26 to about 0.6 wt. % and zinc (Zn) less than about 0.22 wt. %.

44 . The component according to claim 41 , wherein said one or more impurities comprise: silicon (Si) of less than about 0.01 wt. %, copper (Cu) of less than about 0.01 wt. %, nickel (Ni) of less than about 0.002 wt. %, iron (Fe) of less than about 0.002 wt. %, and additional impurities of less than about 0.02 wt.

45 . The component according to claim 41 , wherein said alloy forms a tubular structure.

46 . The component according to claim 41 , wherein said alloy forms a rolled structure.

47 . The component according to claim 41 , wherein said alloy forms an extruded structure.

48 . The component according to claim 41 , wherein said alloy forms an automotive part selected from the group consisting of frames, support members, cross-members, instrument panel beams, roof rails, engine cradles, transfer cases, and steering components.

49 . The component according to claim 41 , wherein said alloy forms a structure by one or more metal forming processes selected from the group consisting of bending, extruding, rolling, hydroforming, stamping, superplastic forming, gas forming, electromagnetic forming, and combinations thereof.

50 . A magnesium-based wrought alloy having a composition comprising:

aluminum (Al) of between about 2.5 to about 4.0 wt. %; manganese (Mn) and zinc (Zn) collectively present at less than about 1.0 wt. %; impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg); wherein the wrought alloy has an elongation of greater than 8% at room temperature.

51 . The magnesium based alloy according to claim 50 , wherein the wrought alloy has a yield strength greater than about 165 MPa.

52 . The magnesium based alloy according to claim 50 , wherein the wrought alloy has an ultimate tensile strength of greater than about 230 MPa.

53 . A magnesium-based wrought alloy having a composition comprising:

aluminum (Al) of between about 2.5 to about 4.0 wt. %; manganese (Mn) and zinc (Zn) collectively present at less than about 1.0 wt. %; impurities collectively less than about 0.1 wt. %; and a balance of magnesium (Mg); wherein the wrought alloy having an extrusion speed of greater than 305 mm per minute at 360° C.

54 . The magnesium based alloy according to claim 53 , wherein the wrought alloy has a yield strength greater than about 165 MPa.

55 . The magnesium based alloy according to claim 53 above, wherein the wrought alloy has an ultimate tensile strength of greater than about 230 MPa.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 4, 2004
From: LUO, AIHUA A.; SACHDEV, ANIL K.
To: GENERAL MOTORS CORPORATION
Reel/Frame 015051/0888 →