Patent classifications
C22C23/06
Magnesium alloy
The invention relates to a magnesium alloy containing (in % by weight) more than 0.0 to 7.0% zinc, optionally more than 0.0 to 1.0% zirconium, optionally more than 0.0 to 1.0% calcium, optionally more than 0.0 to 1.0% manganese, optionally more than 0.0 to 0.5% silicon, optionally more than 0.0 to 1.0% silver, a max. up to 0.5% aluminum and at least one element selected from the group comprising more than 0.05 to 0.6% yttrium, more than 0.05 to 4.0% ytterbium, more than 0.05 to 4.0% gadolinium, with the residue being magnesium and impurities due to production. The invention also relates to a use of a magnesium alloy of this type and an implant therefrom and a method for producing a body of a magnesium alloy according to the invention.
Wrought magnesium alloy
An extrusion of a magnesium-based alloy consisting of, by weight: 0.5 to 1.5% manganese, 0.15 to 0.4% rare earth including lanthanum wherein the lanthanum content of the alloy is 0.15% to less than 0.3%, and up to 0.1% strontium, the balance being magnesium except for incidental impurities which includes zinc.
Magnesium alloy
Magnesium alloy containing, in % by mass, 1.0 to 2.0% of Zn, 0.05 to 0.80% by mass of Zr, 0.05 to 0.40% by mass of Mn, and the balance consisting of Mg and unavoidable impurities. The magnesium alloy may further contain, in % by mass, 0.005% or more and less than 0.20% of Ca.
RADIATION SHIELDING AND MITIGATING ALLOYS, METHODS OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME
Embodiments of the present disclosure include compositions that include magnesium and gadolinium or magnesium and one or more metals.
RADIATION SHIELDING AND MITIGATING ALLOYS, METHODS OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME
Embodiments of the present disclosure include compositions that include magnesium and gadolinium or magnesium and one or more metals.
High Conductivity Magnesium Alloy
A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m−K, and/or ductility exceeding 15-20% elongation to failure.
Magnesium-based hydrogen storage material and method for preparing the same
A method for preparing a magnesium-based hydrogen storage material, includes: a Mg—Ce—Ni family amorphous alloy is prepared by a rapid cooling process; the amorphous alloy is pulverized, so as to obtain a amorphous powder; the amorphous alloy is activated, so as to obtain a MgH.sub.2—Mg.sub.2NiH.sub.4—CeH.sub.2.73 family nanocrystalline composite; the abovementioned composite is carried out a hydrogen absorption and desorption cycle, then the composite is placed in a pure Ar atmosphere for passivation, finally, the passivated composite is oxidized, so as to obtain a MgH.sub.2—Mg.sub.2NiH.sub.4—CeH.sub.2.73—CeO.sub.2 family nanocrystalline composite.
Magnesium-based hydrogen storage material and method for preparing the same
A method for preparing a magnesium-based hydrogen storage material, includes: a Mg—Ce—Ni family amorphous alloy is prepared by a rapid cooling process; the amorphous alloy is pulverized, so as to obtain a amorphous powder; the amorphous alloy is activated, so as to obtain a MgH.sub.2—Mg.sub.2NiH.sub.4—CeH.sub.2.73 family nanocrystalline composite; the abovementioned composite is carried out a hydrogen absorption and desorption cycle, then the composite is placed in a pure Ar atmosphere for passivation, finally, the passivated composite is oxidized, so as to obtain a MgH.sub.2—Mg.sub.2NiH.sub.4—CeH.sub.2.73—CeO.sub.2 family nanocrystalline composite.
A CASTING MAGNESIUM ALLOY FOR PROVIDING IMPROVED THERMAL CONDUCTIVITY
A casting magnesium alloy for providing improved thermal conductivity A magnesium alloy for providing improved thermal conductivity includes from 1 wt.% to 5 wt.% of lanthanum, from 1 wt.% to 5 wt.% of cerium or a combination thereof, and from 0.5 wt.% to 3 wt.% of neodymium, from 0.5 wt.% to 3 wt.% of gadolinium or a combination thereof, and from 0.0 wt.% to 0.2 wt.% of yttrium, and up to 0.8 wt.% of praseodymium, and up to 0.8 wt.% manganese, and up to 1.0 wt.% aluminium, and up to 0.8 wt.% zinc, and up to 20ppm beryllium, and with balanced magnesium and inevitable impurities.
A CASTING MAGNESIUM ALLOY FOR PROVIDING IMPROVED THERMAL CONDUCTIVITY
A casting magnesium alloy for providing improved thermal conductivity A magnesium alloy for providing improved thermal conductivity includes from 1 wt.% to 5 wt.% of lanthanum, from 1 wt.% to 5 wt.% of cerium or a combination thereof, and from 0.5 wt.% to 3 wt.% of neodymium, from 0.5 wt.% to 3 wt.% of gadolinium or a combination thereof, and from 0.0 wt.% to 0.2 wt.% of yttrium, and up to 0.8 wt.% of praseodymium, and up to 0.8 wt.% manganese, and up to 1.0 wt.% aluminium, and up to 0.8 wt.% zinc, and up to 20ppm beryllium, and with balanced magnesium and inevitable impurities.