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US 2020/0048749 A1Published application
High-performance 6000-series aluminum alloy structures
AssigneeNanoAL LLC
InventorsNhon Q. VO, Francisco U. FLORES, Vincent R. JANSEN, Joseph R. CROTEAU
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Abstract
Aluminum-magnesium-silicon alloys, fabricated by inventive processes, that exhibit high strength, high conductivity, and high thermal stability.
Claims36
An aluminum alloy structure, comprising:
- about 0.6% to about 0.9% by weight magnesium, about 0.35% to about 0.7% by weight silicon, about 0.2% to about 0.5% by weight zirconium, and about 0.005% to about 0.2% by weight tin, with aluminum as the remainder;
- and
- Al3Zr nanoscale precipitates having an average diameter of no more than about 20 nm, having an L12 structure in an α-Al face centered cubic matrix, and having an average number density of at least about 2021 m−3;
- wherein the aluminum alloy structure has a thermal conductivity of at least about 185 W/mK, a yield strength of at least about 270 MPa, and a tensile strength of at least about 290 MPa.
1 more element
An aluminum alloy structure, comprising:
- about 0.6% to about 0.9% by weight magnesium, about 0.35% to about 0.7% by weight silicon, about 0.2% to about 0.5% by weight zirconium, and about 0.005% to about 0.2% by weight tin, with aluminum as the remainder;
- and
- Al3Zr nanoscale precipitates having an average diameter of no more than about 20 nm, having an L12 structure in an a-Al face centered cubic matrix, and having an average number density of at least about 2021 m−3;
- wherein the aluminum alloy structure has a yield strength of at least about 400 MPa, a tensile strength of at least about 420 MPa, and an elongation at break of at least about 3%.
1 more element
An aluminum alloy structure, comprising:
- about 0.6% to about 0.9% by weight magnesium, about 0.35% to about 0.7% by weight silicon, about 0.2% to about 0.5% by weight zirconium, and about 0.005% to about 0.2% by weight tin, with aluminum as the remainder;
- and
- Al3Zr nanoscale precipitates having an average diameter of no more than about 20 nm, having an L12 structure in an α-Al face centered cubic matrix, and having an average number density of at least about 2021m−3;
- wherein the aluminum alloy structure has a yield strength of at least about 270 MPa, a tensile strength of at least about 290 MPa, and an elongation at break of at least about 8%.
1 more element
An aluminum alloy structure,comprising:
- aluminum;
- magnesium;
- and
- silicon;
- wherein the structure has a high electrical conductivity value EC of at least about 47.5% IACS, and has a high tensile strength Value of at least [960 MPa−(11 MPa/% IACS)(EC % IACS)].
2 more elements
An aluminum alloy structure, comprising:
- about 0.6% to about 0.9% by weight magnesium, about 0.35% to about 0.7% by weight silicon, about 0.2% by weight iron, and about 0.1% weight tin, with aluminum as the remainder;
- and
- wherein the aluminum alloy structure has a yield strength of at least about 400 MPa, a tensile strength of at least about 410 MPa, and an elongation at break of at least about 2%.
A method of fabricating an aluminum alloy structure, the method comprising:
- a) melting aluminum, while adding master alloys, at a temperature of about 700° C. to about 900° C. to form melted constituents;
- b) then casting the melted constituents into a casting mold at ambient temperature to form a casted ingot;
- c) then cold-rolling the casted ingot to form a rolled structure;
- d) then heat aging the rolled structure at a temperature about 350° C. to about 460° C. for a time of about 0.5 hours to about 8 hours to form an aged structure;
- e) then solutionizing the aged structure at a temperature of about 500° C. to about 580° C. for a time of about 0.2 hours to about 6 hours to form a solutionized structure;
- and
- f) then heat aging the solutionized structure at a temperature about 100° C. to about 200° C. for a time of about 0.5 hours to about 48 hours to form the aluminum alloy structure.
4 more elements
A method of fabricating an aluminum alloy structure, the method comprising:
- a) melting aluminum., while adding master alloys, at a temperature of about 700° C. to about 900° C. to form melted constituents;
- b) then casting the melted constituents into a casting mold at ambient temperature to form a casted ingot;
- c) then heat aging the casted ingot at a temperature of about 350° C. to about 460° C. for a time of about 0.5 hours to about 8 hours to form a first aged structure;
- d) then solutionizing the first aged structure at a temperature of about 500° C. to about 580° C. for a time of about 0.2 hours to about 6 hours to form a solutionized structure;
- e) then heat aging the solutionized structure at a temperature about 160° C. to about 220° C. for a time of about 0.2 hours to about 6 hours to form a second aged structure;
- f) then cold-rolling the second aged structure to form a rolled structure;
- and
- g) then heat aging the rolled structure at a temperature about 80° C. to about 120° C. for a time of about 24 hours to about 100 hours to form the aluminum alloy structure.
5 more elements
A method of fabricating an aluminum alloy structure, the method comprising:
- a) melting aluminum, while adding master alloys, at a temperature of about 700° C. to about 900° C. to form melted constituents;
- b) then casting the melted constituents into a casting mold at ambient temperature form a casted ingot;
- c) then solutionizing the casted ingot at a temperature of about 500° C. to about 580° C. for a time of about 0.2 hours to about 6 hours to form a solutionized ingot;
- d) then heat aging the solutionized ingot at a temperature about 180° C. to about 235° C. for a time of about 0.5 hours to about 48 hours to form an aged ingot;
- and
- e) then cold-rolling the aged ingot at ambient temperature with an area reduction from about 1000% to about 8000% to form the cold-rolled aluminum alloy structure.
3 more elements
Dependencies are inferred from the claim text.