Method for preparing cryomilled aluminum alloys and components extruded and forged therefrom
View Patent ↗High strength aluminum alloy powders, extrusions, and forgings are provided in which the aluminum alloys exhibit high strength at atmospheric temperatures and maintain high strength and ductility at extremely low temperatures. The alloy is produced by blending about 89 atomic % to 99 atomic % aluminum, 1 atomic % to 11 atomic % of a secondary metal selected from the group consisting of magnesium, lithium, silicon, titanium, zirconium, and combinations thereof, and up to about 10 atomic % of a tertiary metal selected from the group consisting of Be, Ca, Sr, Ba, Ra, Sc, V, Cr, Mn, Fe, Co, Ni, Cu, Zn, Y, Nb, Mo, Tc, Ru, Rh, Pd, Ag, Cd, W, and combinations thereof. The alloy is produced by nanostructure material synthesis, such as cryomilling, in the absence of refractory dispersoids. The synthesized alloy is then canned, degassed, consolidated, extruded, and optionally forged into a solid metallic component. Grain size within the alloy is less than 0.5 μm, and alloys with grain size less than 0.1 μm may be produced.
1. A method of producing an aluminum alloy comprising
providing a metal powder comprising
89 atomic % to 99 atomic % aluminum;
1 atomic % to 11 atomic % of a secondary metal selected from the group consisting of magnesium, lithium, silicon, titanium, zirconium, and combinations thereof; and
up to about 10 atomic % of a tertiary metal selected from the group consisting of Be, Ca, Sr, Ba, Ra, Sc, V, Cr, Mn, Fe, Co, Ni, Cu, Zn, Y, Nb, Mo, Tc, Ru, Rh, Pd, Ag, Cd, W, and combinations thereof; and,
processing the metal powder with a nanostructured material synthesis technique such that at least 0.3 weight % nitrogen is added to the metal;
wherein refractory material is not added to the metal during processing.
2. The method of claim 1 , further comprising the step of pre-alloying the provided metal powder prior to processing.
3. The method of claim 1 , wherein the synthesis technique is selected from the group consisting of cryomilling, gas condensation, chemical vapor deposition, plasma synthesis, rapid solidification, and severe plastic deformation, whereby a limited and controlled amount of nitrogen may be introduced into the alloy.
4. The method of claim 3 , wherein the synthesis technique is cryomilling.
5. The method of claim 4 , wherein the step of cryomilling comprises:
supplying the metal powder to a ball mill attritor;
maintaining the supply of metal powder in a liquid nitrogen medium;
activating the attritor, whereby the metal powder is repeatedly impinged between metal balls within the attritor;
deactivating the attritor; and,
removing the cryomilled metal powder from the attritor.
6. The method of claim 5 , wherein the step of cryomilling is continued until the equilibrium grain size of the metal is reached.
7. The method of claim 6 , wherein the step of cryomilling is continued for between 6 and 10 hours.
8. The method of claim 7 , wherein the step of cryomilling is continued for about 8 hours.
9. The method of claim 1 , wherein the step of providing a metallic powder comprises providing a metallic powder substantially free of oxides.
10. The method of claim 9 , wherein the metal powder is provided in a substantially oxygen-free atmosphere.
11. The method of claim 1 , wherein the secondary metal is magnesium.
12. The method of claim 11 , wherein the magnesium is present in an amount of 4 weight % to 10 weight % of the alloy.
13. The method of claim 12 , wherein aluminum is present in an amount of 82 weight % to 96 weight %, and a tertiary metals is provided that is selected from the group consisting of zinc, copper, cobalt, zirconium, and nickel.
14. The method of claim 13 , comprising 6 weight % to 9 weight % zinc, less than 2 weight % copper, less than 2 weight % cobalt, less than about 0.2 weight % zirconium, and less than about 0.2 weight % nickel.
15. A method of producing an extruded aluminum product comprising the steps of:
providing a refractory free metallic powder comprising
89 atomic % to 99 atomic % aluminum;
1 atomic % to 11 atomic % of a secondary metal selected from the group consisting of magnesium, lithium, silicon, titanium, zirconium, and combinations thereof; and
up to about 10 atomic % of a tertiary metal selected from the group consisting of Be, Ca, Sr, Ba, Ra, Sc, V, Cr, Mn, Fe, Co, Ni, Cu, Zn, Y, Nb, Mo, Tc, Ru, Rh, Pd, Ag, Cd, W, and combinations thereof;
cryomilling the metallic powder in a liquid nitrogen atmosphere;
removing gaseous components from the cryomilled powder;
consolidating the cryomilled powder into a metallic billet; and
extruding the metallic billet.
16. The method of claim 15 , wherein gaseous components are removed from the cryomilled powder by packing the cryomilled powder into a can having an evacuation port and providing a vacuum to the evacuation port, thereby evacuating gaseous components from the powder.
17. The method of claim 16 , wherein the removal of gaseous components occurs at a temperature between about 600° F. and about 850° F. for a time sufficient to reduce hydrogen content to a level below about 30 wppm.
18. The method of claim 17 , wherein consolidating the cryomilled powder comprises compressing the powder within a hot isostatic press.
19. The method of claim 18 , wherein the step of extruding the metal billet comprises preheating the consolidated metal powder to about 400° F. and extruding the consolidated powder with an extrusion area ratio of greater than 6:1 at a ram speed of about 0.2 inches per minute.