Patent classifications
C22C23/06
Biodegradable magnesium alloys, methods of manufacture thereof and articles comprising the same
Disclosed herein is an article comprising a metal alloy; where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof; where the second element is chemically different from the third element; and where the second element and the third element are scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof; and a protective layer disposed upon the metal alloy and is reactively bonded to the metal alloy; where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another.
Biodegradable magnesium alloys, methods of manufacture thereof and articles comprising the same
Disclosed herein is an article comprising a metal alloy; where the metal alloy comprises a base metal, a second element and a third element; where the base metal is magnesium, calcium, strontium, zinc, or a combination thereof; where the second element is chemically different from the third element; and where the second element and the third element are scandium, yttrium, gadolium, cerium, neodymium, dysporium, or a combination thereof; and a protective layer disposed upon the metal alloy and is reactively bonded to the metal alloy; where the protective layer comprises a base non-metallic derivative, a second non-metallic derivative and a third non-metallic derivative of metals present in the metal alloy; and where the base non-metallic derivative, the second non-metallic derivative and the third non-metallic derivative are all chemically different from one another.
Mg—Gd—Y—Zn—Zr alloy and process for preparing the same
The present disclosure discloses a Mg—Gd—Y—Zn—Zr alloy which, in embodiments, includes high strength, toughness, corrosion resistance and anti-flammability. The disclosure includes a process for preparation thereof. Components and mass percentages in the Mg—Gd—Y—Zn—Zr alloy are: 3.0%≤Gd≤9.0%, 1.0%≤Y≤6.0%, 0.5%≤Zn≤3.0%, 0.2%≤Zr≤1.5%, the balance being Mg and inevitable impurities. The process for preparation thereof comprises: adding pure Mg into a smelting furnace for heating, then introducing mixed gases of CO.sub.2 and SF.sub.6 into the furnace for protection; adding other raw materials in sequence when the pure Mg is completely melted; preparing an ingot; conducting a homogenization treatment on the ingot prior to extrusion; conducting an aging treatment on the extruded alloy. The present disclosure includes a wrought magnesium alloy having both superior overall performances, good fracture toughness, corrosion resistance and anti-flammability, with a small amount of rare earth element by adjusting the proportion of the alloy elements and by conventional casting, extrusion and heat treatment processes.
Mg—Gd—Y—Zn—Zr alloy and process for preparing the same
The present disclosure discloses a Mg—Gd—Y—Zn—Zr alloy which, in embodiments, includes high strength, toughness, corrosion resistance and anti-flammability. The disclosure includes a process for preparation thereof. Components and mass percentages in the Mg—Gd—Y—Zn—Zr alloy are: 3.0%≤Gd≤9.0%, 1.0%≤Y≤6.0%, 0.5%≤Zn≤3.0%, 0.2%≤Zr≤1.5%, the balance being Mg and inevitable impurities. The process for preparation thereof comprises: adding pure Mg into a smelting furnace for heating, then introducing mixed gases of CO.sub.2 and SF.sub.6 into the furnace for protection; adding other raw materials in sequence when the pure Mg is completely melted; preparing an ingot; conducting a homogenization treatment on the ingot prior to extrusion; conducting an aging treatment on the extruded alloy. The present disclosure includes a wrought magnesium alloy having both superior overall performances, good fracture toughness, corrosion resistance and anti-flammability, with a small amount of rare earth element by adjusting the proportion of the alloy elements and by conventional casting, extrusion and heat treatment processes.
HIGH-STRENGTH MAGNESIUM ALLOY PROFILE, PREPARATION PROCESS THEREFOR AND USE THEREOF
Provided are a high-strength magnesium alloy profile, a preparation process therefor and the use thereof, wherein same relate to the technical field of the formation of high-strength magnesium alloys. A strengthening phase of the high-strength magnesium alloy profile in an extrusion state mainly comprises LPSO phase and β phase, wherein the volume fraction of LPSO phase is 1-40%; and the volume fraction of β phase is 1-20%. A strengthening phase of the high-strength magnesium alloy profile in an aging state mainly comprises LPSO phase, β phase, β′ phase and γ′ phase, wherein the volume fraction of LPSO phase is 1-40%; the volume fraction of β phase is 1-20%; the number density of β′ phase is 10.sup.15-10.sup.25 m.sup.−3, and the length to thickness ratio l/d thereof is 1:20; and the number density of γ′ phase is 10.sup.14-10.sup.24 m.sup.−3 and the length to thickness ratio l/d thereof is 1:50.
HIGH-STRENGTH MAGNESIUM ALLOY PROFILE, PREPARATION PROCESS THEREFOR AND USE THEREOF
Provided are a high-strength magnesium alloy profile, a preparation process therefor and the use thereof, wherein same relate to the technical field of the formation of high-strength magnesium alloys. A strengthening phase of the high-strength magnesium alloy profile in an extrusion state mainly comprises LPSO phase and β phase, wherein the volume fraction of LPSO phase is 1-40%; and the volume fraction of β phase is 1-20%. A strengthening phase of the high-strength magnesium alloy profile in an aging state mainly comprises LPSO phase, β phase, β′ phase and γ′ phase, wherein the volume fraction of LPSO phase is 1-40%; the volume fraction of β phase is 1-20%; the number density of β′ phase is 10.sup.15-10.sup.25 m.sup.−3, and the length to thickness ratio l/d thereof is 1:20; and the number density of γ′ phase is 10.sup.14-10.sup.24 m.sup.−3 and the length to thickness ratio l/d thereof is 1:50.
Degradable corrosion-resistant high strength and ductility magnesium alloy for biomedical use and preparation method therefor
The present disclosure provides a degradable corrosion-resistant high strength and ductility magnesium alloy for biomedical use and the preparation method therefor. With regard to a total weight of the magnesium alloy of 100%, the composition of components of the magnesium alloy comprises: 1.0 to 4.5% of Nd, 0.2 to 2.0% of Zn, 0 to 1.0% of Ca, 0 to 1.0% of Zr, and balance of Mg. The magnesium alloy is prepared by producing a magnesium alloy ingot by means of vacuum semi-continuous casting and according to the components and weight percentage thereof followed by solid solution treatment and extrusion. The degradable corrosion-resistant high strength and ductility magnesium alloy for biomedical use provided by the present disclosure has the advantages of being non-toxic and fully degradable, good corrosion resistance as well as high strength and ductility etc., and can be used for preparing a vascular stent.
MAGNESIUM ALLOY WITH HIGH THERMAL CONDUCTIVITY, INVERTER HOUSING, INVERTER AND VEHICLE
A magnesium alloy with high thermal conductivity, an inverter housing, an inverter and a vehicle are provided. Based on the total mass of the magnesium alloy with high thermal conductivity, the magnesium alloy with high thermal conductivity includes: 2.0-4.0 wt % of Al, 0.1-0.3 wt % of Mn, 1.0-2.0 wt % of La, 2.0-4.0 wt % of Ce, 0.1-1.0 wt % of Nd, 0.5-2.0 wt % of Zn, 0.1-0.5 wt % of Ca, less than 0.1 wt % of Sr, less than 0.1 wt % of Cu, and magnesium.
MAGNESIUM ALLOY WITH HIGH THERMAL CONDUCTIVITY, INVERTER HOUSING, INVERTER AND VEHICLE
A magnesium alloy with high thermal conductivity, an inverter housing, an inverter and a vehicle are provided. Based on the total mass of the magnesium alloy with high thermal conductivity, the magnesium alloy with high thermal conductivity includes: 2.0-4.0 wt % of Al, 0.1-0.3 wt % of Mn, 1.0-2.0 wt % of La, 2.0-4.0 wt % of Ce, 0.1-1.0 wt % of Nd, 0.5-2.0 wt % of Zn, 0.1-0.5 wt % of Ca, less than 0.1 wt % of Sr, less than 0.1 wt % of Cu, and magnesium.
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.