Claims
- 1. A process for making a workpiece suitable for being hot worked to produce a wrought metal product, where said process comprises the following sequential steps:
- (a) Providing an aluminum alloy characterized by a melting range of about 20.degree. K. or more under Standard Conditions, said alloy being in the form of a powder consisting essentially of particles solidified at a rate on the order of about 1000.degree. K./sec or more;
- (b) Producing a compact by the application of isostatic pressure to said powder, such that the density of said compact is about 60% to 85% of the theoretical density of said alloy;
- (c) Exposing said compact to a dynamic atmosphere which is essentially devoid of water and gaseous oxidants of said alloy and heating the composite to a temperature of up to about 650.degree. K. to degas the surface films and to preferably remove H.sub.2 O as H.sub.2 O;
- (d) While said compact is exposed to said atmosphere, further heating said compact such that its exterior surfaces attain temperatures at which about 2 to 20 wt% of said alloy would be liquid under Standard Conditions, volatilizing alloying materials from a liquid surface region to form a reduced volatile alloying material surface region of about 0.1 to 1 millimeters, thereby raising the solidus temperature of said surface region at an equilibrium point causing resolidification of said surface region at said equilibrium point, and then cooling said compact such that its exterior surfaces attain temperatures of about 150.degree. K. or more below the solidus of said alloy, such that said compact becomes sinter-sealed by attaining a Degree of Sealing of about 80% or more.
- 2. A process according to claim 1 wherein following step (d), said compact is hot worked to produce a wrought metal product which has about the same density as the theoretical density of said alloy.
- 3. A process according to claim 1 wherein step (b) is carried out by producing said compact in a vacuum atmosphere which consists essentially of residual air at a pressure of about 10 torr or less.
- 4. A process according to claim 1 wherein for purposes of steps (c) and (d) said atmosphere consists essentially of a dynamic vacuum at a pressure of about 10.sup.-1 torr or less.
- 5. A process according to claim 1 wherein for purposes of step (c), said atmosphere consists essentially of a dynamic inert gas atmosphere at a pressure of less than 10.sup.-1 torr and step (d) is an inert atmosphere of about 1 torr or less pressure.
- 6. A process according to claim 1 wherein following step (b), said compact is loaded into a vacuum furnace and then heated under vacuum to a temperature of about 300.degree. C., followed by carrying out step (d).
- 7. A process according to claim 1 wherein step (b) is carried out by loading and packing said powder into a flexible container, having the pressure of air in said container reduced to about 10 torr or less, sealing the container under vacuum and applying hydraulic pressure to said container such that the density of said compact is about 75% to 85% of the theoretical density of said alloy.
- 8. A process according to claim 1 wherein said powder consists essentially of particles scalped through about 30 USS mesh screen and having a Fisher APD of about 25 microns, and a gradation of sizes.
- 9. A process according to claim 1 wherein said powder consists essentially of F temper particles each having the composition of said alloy.
- 10. A process according to claim 1 wherein said alloy consists essentially of about 80% or more Al, by weight, and one or more elements selected from the group consisting of Mg, Zn, Ca, and Li, and at least one or more elements from the group consisting of Fe, Cu, Mn, Si, Mo, Cr, Ni, Zr, Ti, V, B, Co and Hf.
- 11. A process according to claim 10 wherein said powder consists essentially of particles having varying compositions whereby said powder constitutes a mixture; there being for at least one constituent element X of said alloy, where X is from the group consisting of Cu, Mg, Ca, Zn, Si and Li, a separate composition consisting essentially of about 10 to 100 wt% X, balance aluminum; and there being a single separate composition which comprises the predominant amount of aluminum needed together with all of the constituent elements of said alloy which are from the group consisting of Fe, Mn, Mo, Ca, Cr, Zr, Ni, Y, Ti, B, Co and Hf.
- 12. A process according to claim 1 wherein said loading comprises a filling of the bottom of said flexible container with a first alloy, placing a sleeve within said flexible container, filling said sleeve with a second alloy, filling spaces between said sleeve and said flexible container with said first alloy, removing said sleeve and filling the top of said flexible container with said first alloy.
CROSS REFERENCE TO RELATED APPLICATIONS
This is a continuation-in-part of U.S. application Ser. No. 112,631, filed Jan. 16, 1980 now abandoned.
US Referenced Citations (3)
Non-Patent Literature Citations (3)
Entry |
Otto, "Metallurgical Factors Controlling Structure in High Strength Aluminum P/M Products," NTIS AD/A-030 606 (1976). |
Lewis et al., "A Feasibility Study for Development of Structural Aluminum Alloys from Rapidly Solidified Powders for Aerospace Structural Applications," AFML-TR-78-102 (1978). |
Goetzel, Treatis on Powder Metallurgy, vol. II (1950) pp. 489-501 and 722-741. |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
112631 |
Jan 1980 |
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