High strength aluminum alloy and process

Claim 2

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy having a composition consisting essentially, by weight, of magnesium in a small but effective amount for increased strength up to about 7%, about 0.3% up to about 4% oxygen, up to about 21/2% carbon, and the balance essentially aluminum, and characterized by a tensile strength (UTS) at room temperature above 66.3 ksi.

Claim 3

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the alloy has a tensile strength (UTS) at room temperature of at least 69.7 ksi.

Claim 4

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the magnesium content is at least about 2%.

Claim 5

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 3, wherein the magnesium content is up to about 5%.

Claim 6

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the magnesium content is about 4% up to about 5%.

Claim 7

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the carbon content is at least 0.2%.

Claim 8

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 3, wherein the oxygen content is about 0.4% to about 2%.

Claim 9

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 3, wherein the carbon content is about 0.2% to 2%.

Claim 10

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the alloy is characterized by a room temperature tensile strength (UTS) of about 69.7 ksi up to about 87.9 ksi and an elongation of about 6% to about 8%.

Claim 11

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the alloy is characterized in the extruded condition by a tensile strength (UTS) at room temperature of at least about 93.3 ksi.

Claim 12

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 1, wherein the dispersoids are present in a small but effective amount for improved strength up to about 81/2 volume %.

Claim 13

An oxide dispersion-strengthened mechanically alloyed aluminum-base alloy according to claim 11, wherein the oxide dispersoid is present in an amount of about 1% up to less than 5%.

Claim 14

A process for working an oxide dispersion-strengthened mechanically alloyed aluminum-magnesium powder at elevated temperature to produce a consolidated worked product, said aluminum-magnesium power having a composition consisting essentially, by weight, of magnesium in a small but effective amount for increased strength up to about 7%, about 0.3% up to about 4% oxygen, up to about 21/2% carbon, and the balance essentially aluminum, and characterized by a tensile strength (UTS) at room temperature of above 66.3 ksi and said powder having in compacted form a working temperature-strength profile which includes a critical working temperature-strength transition zone characterized by a sharp lowering of room temperature strength relative to increased working temperature, comprising: (a) determining the working temperature-strength profile of the selected charge material, said profile being characterized by an overall decrease in strength relative to the working temperature; and (b) working the charge material at a temperature selected with reference to the working temperature-strength profile to optimize the workability of the charge material and the strength of the worked product.

Claim 15

A process for working an oxide dispersion-strengthened mechanically alloyed aluminum-magnesium powder at elevated temperature to produce a consolidated worked product, said aluminum-magnesium power having a composition consisting essentially, by weight, of magnesium in a small but effective amount for increased strength up to about 7%, about 0.3% up to about 4% oxygen, up to about 21/2% carbon, and the balance essentially aluminum, and characterized by a tensile strength (UTS) at room temperature of above 66.3 ksi and said powder having in compacted form a working temperature-strength profile which includes a critical working temperature-strength transition zone characterized by a sharp lowering of room temperature strength relative to increased working temperature, comprising: (a) determining the working temperature-strength profile of the selected charge material, said profile being characterized by an overall decrease in strength relative to the working temperature; and (b) working the charge material at a temperature selected with reference to the working temperature-strength profile to optimize the workability of the charge material and the strength of the worked product.

Claim 16

A process according to claim 13, wherein the said critical transition zone is preceded by a plateau region in which the strength of the product is substantially unaffected by increased temperature.

Claim 17

A process according to claim 13, wherein working of the charge material is carried out at a temperature selected in the plateau region for maximum strength.

Claim 18

A process according to claim 13, wherein working of the charge material is carried out at a temperature selected above the maximum temperature of the plateau region to achieve optimum workability of the charge material with sacrifice in strength of the worked product.

Claim 19

A process according to claim 13, wherein the working step comprises extruding the charge material.

Claim 20

A process according to claim 17, wherein for maximum strength the extrusion is carried out at a minimum ratio.

Claim 21

A process according to claim 13, wherein the dispersoids of the dispersion-strengthened mechanically alloyed aluminum is present in a small but effective amount of dispersoid for improved strength up to about 81/2 volume %.

Claim 22

A process according to claim 19, wherein the charge material consists essentially of about 2% up to about 5% Mg, up to about 21/2% C, about 0.3% up to about 4% O, and the extrusion is carried out at a temperature below the critical working temperature-strength transition zone to obtain optimum strength in the worked product.

Claim 23

A process according to claim 20, wherein the extrusion is caried out at a temperature up to the equivalent of about 750° F.

Claim 24

A process according to claim 20, wherein the extrusion is carried out at a maximum extrusion ratio.

Claim 25

A process for treating a dispersion-strengthened mechanically alloyed aluminum containing, by weight, from about 2% up to about 7% Mg, up to about 21/2% C, and from 0.3 up to about 4% O, by a method including steps comprising hot working said aluminum to form a consolidated product, the improvement of optimizing the strength of the consolidated product and workability during hot working by employing processing conditions in the interrelationship set forth by the following formula: UTS=0.059T.sub.1 -0.014T.sub.2 -0.034T.sub.3 -0.55E.sub.R +11.5(wt. % O)+20.1(wt. % C)-0.18ε-3t+214.6 where UTS=Ultimate Tensile Strength in ksi (at room temperature) T 1 =Degas Temperature T 2 =Compaction Temperature T 3 =Extrusion Temperature E R =Extrusion Ratio, which is the ratio of the cross sectional area of the extruded billet to the cross sectional of the extruded rod. ε=Strain Rate (sec -1 ) t=Time at highest degassing temperature (hours).

Claim 26

A process for treating a dispersion-strengthened mechanically alloyed aluminum containing, by weight, from about 2% up to about 7% Mg, up to about 21/2% C, and from 0.3 up to about 4% O, by a method including steps comprising hot working said aluminum to form a consolidated product, the improvement of optimizing the strength of the consolidated product and workability during hot working by employing processing conditions in the interrelationship set forth by the following formula: UTS=0.059T.sub.1 -0.014T.sub.2 -0.034T.sub.3 -0.55E.sub.R +11.5(wt. % O)+20.1(wt. % C)-0.18ε-3t+214.6 where UTS=Ultimate Tensile Strength in ksi (at room temperature) T 1 =Degas Temperature T 2 =Compaction Temperature T 3 =Extrusion Temperature E R =Extrusion Ratio, which is the ratio of the cross sectional area of the extruded billet to the cross sectional of the extruded rod. ε=Strain Rate (sec -1 ) t=Time at highest degassing temperature (hours).