US2015315690A1PendingUtilityA1
Method for manufacturing extruded magnesium alloy and extruded magnesium alloy manufactured thereby
Est. expiryJan 4, 2033(~6.5 yrs left)· nominal 20-yr term from priority
C22C 23/04C22C 23/02C22F 1/06C22C 23/00B22D 21/04B21C 23/002
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Claims
Abstract
Provided are a method of preparing a magnesium alloy extrudate and a magnesium alloy extrudate prepared thereby. Specifically, the present invention is related to a method of preparing a magnesium alloy extrudate including melting a magnesium alloy raw material (step 1), casting the magnesium alloy raw material melted in step 1 to prepare a magnesium alloy billet (step 2), homogenizing the magnesium alloy billet prepared in step 2 (step 3), applying 3% to 20% of compressive deformation to the homogenized magnesium alloy billet of step 3 (step 4), and extruding the compressive deformed magnesium alloy billet of step 4 (step 5), and a magnesium alloy extrudate prepared thereby.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A method of preparing a magnesium alloy extrudate, the method comprising:
melting a magnesium alloy raw material; casting the melted magnesium alloy raw material melted in step 1 in a temperature range of 650° C. to 750° C. to prepare a magnesium alloy billet; homogenizing the magnesium alloy billet prepared in by heat treating in a temperature range of 400° C. to 550° C. for 0.5 hours to 96 hours and cooling; applying 3% to 20% of compressive deformation to the homogenized magnesium alloy billet; and extruding the compressive deformed magnesium alloy billet.
2 . (canceled)
3 . (canceled)
4 . The method as set forth in claim 1 , wherein the homogenizing is performed after preheating in a temperature range of 250° C. to 350° C.
5 . The method as set forth in claim 1 , wherein the compressive deformation is performed in a longitudinal direction of the magnesium alloy billet.
6 . The method as set forth in claim 1 , wherein the compressive deformation is performed in a temperature range of room temperature to 250° C.
7 . The method as set forth in claim 1 , wherein the extrusion is performed after preheating in a temperature range of 200° C. to 450° C.
8 . The method as set forth in claim 1 , further comprising performing an aging treatment after the extrusion.
9 . The method as set forth in claim 8 , wherein the aging treatment is performed in a temperature range of 150° C. to 250° C. for 1 hour to 360 hours.
10 . A magnesium alloy extrudate prepared by the method of claim 1 .
11 . A part for transportation equipment manufactured using the magnesium alloy extrudate of claim 8 .Cited by (0)
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