US2022259705A1PendingUtilityA1
Magnesium alloy and method for producing same
Assignee: LKR LEICHTMETALLKOMPETENZZENTRUM RANSHOFEN GMBHPriority: Jul 8, 2019Filed: Mar 25, 2020Published: Aug 18, 2022
Est. expiryJul 8, 2039(~12.9 yrs left)· nominal 20-yr term from priority
C22C 21/02C22F 1/047C22F 1/043C22C 21/08C22F 1/183C22F 1/04C22C 24/00C22C 21/16C22F 1/06C22C 23/02C22C 23/00C22C 21/10C22F 1/05C22F 1/16C22C 14/00C22C 21/00C22C 9/04
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Claims
Abstract
The invention relates to a magnesium alloy. To obtain a magnesium alloy which exhibits both a high strength and also a high deformability, a magnesium alloy is provided according to the invention, comprising (in at %) 15.0% to 70.0% lithium, greater than 0.0% aluminum, and magnesium and production-related impurities as a remainder, wherein a ratio of aluminum to magnesium (in at %) is 1:6 to 4:6. The invention also relates to a method for producing the magnesium alloy.
Claims
exact text as granted — not AI-modified1 . A magnesium alloy, comprising (in at %),
15.0% to 70.0% lithium, greater than 0.0% aluminum, optionally also greater than 0.0 to 3.0 wt % calcium, optionally also greater than 0.0 to 3.0 wt % rare earth metals, in particular yttrium, optionally also 3.0 wt % to 10.0 wt % zinc, optionally also 2.0 wt % to 10.0 wt % silicon, magnesium and production-related impurities as a remainder, wherein a ratio of aluminum to magnesium (in at %) is 1.2:6 to 4:6.
2 . The magnesium alloy according to claim 1 , wherein the magnesium alloy comprises (in at %) 30.0% to 60.0%, in particular 40% to 50% lithium.
3 . The magnesium alloy according to claim 1 , wherein the ratio of aluminum to magnesium (in at %) is 2:6 to 3.5:6.
4 .- 5 . (canceled)
6 . The magnesium alloy according to claim 1 , wherein the magnesium alloy contains calcium and rare earth metals, in particular yttrium, wherein a total amount of calcium and rare earth metals, in particular yttrium, is greater than 0.0 to 3.0 wt %.
7 .- 8 . (canceled)
9 . A method for producing a magnesium alloy according to claim 1 , wherein a heat treatment of the magnesium alloy is carried out in order to optimize a strength and/or deformability of the magnesium alloy.
10 . The method according to claim 9 , wherein the heat treatment is carried out at a temperature greater than 200° C., in particular between 200° C. and 400° C., for more than 20 minutes, in particular more than 1 hour.
11 . A feedstock, semi-finished product, or element having a magnesium alloy according to claim 1 .
12 . A feedstock, semi-finished product, or element obtainable using the method according to claim 9 .Join the waitlist — get patent alerts
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