Claims
- 1. A process for preparing a reinforced composite alloy without residual porosity, having improved properties and particularly good ductility, consisting of a matrix of very pure aluminium having dispersed therein 3 to 20% by weight of a refractory material addition in grain form, said addition being insoluble in aluminum both in the solid and liquid states, and said addition grains being dispersed homogeneously throughout the aluminum matrix to which they are bonded individually, said process comprising the following steps:
- a. forming a dispersion of grains of a refractory material using a fluidized suspension in a stream of preheated gas, which is neutral with respect to the addition grains and to the aluminum;
- b. desorbing moisture, oxygen and nitrogen from said grains to superficially activate said grains;
- c. introducing said dispersion into molten aluminum with energetic stirring, at a temperature selected in the range from 850.degree. to 1300.degree. C to form a homogeneous composite alloy;
- d. degasing the homogeneous composite alloy;
- e. casting and solidifying the composite alloy;
- f. subjecting the solidified composite alloy; to at least one hot-rolling step at about 400.degree. C; and
- g. subjecting the rolled composite alloy to at least one annealing step at about 350.degree. C.
- 2. A process according to claim 1, wherein said addition consists of TiB.sub.2 grains having substantially the same average size selected in the range from one fraction of a micron to a few microns, said molten aluminum being kept at a temperature substantially equal to 900.degree. C.
- 3. A process according to claim 2, wherein said matrix consists of 99.5% pure aluminum, and said addition consists of 10 to 20% by weight of said TiB.sub.2 grains.
- 4. The process according to claim 1, wherein said addition consists of TiN grains having substantially the same average size selected in the range from one fraction of a micron to a few microns, the molten aluminum being kept at a temperature substantially equal to 900.degree. C.
- 5. A process according to claim 4, wherein said matrix consists of 99.5% pure aluminum and said addition consists of 10 to 20% by weight of said TiN grains.
Priority Claims (1)
Number |
Date |
Country |
Kind |
72.20864 |
Jun 1972 |
FR |
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Parent Case Info
This is a division of application Ser. No. 368,434, filed June 8, 1973, now U.S. Pat. No. 3,858,640.
US Referenced Citations (5)
Number |
Name |
Date |
Kind |
3366515 |
Fraser et al. |
Jan 1968 |
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3399086 |
Das et al. |
Aug 1968 |
|
3476614 |
Jehenson et al. |
Nov 1969 |
|
3728108 |
Sifferlen et al. |
Apr 1973 |
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3884676 |
Nadkarni et al. |
May 1975 |
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Divisions (1)
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Number |
Date |
Country |
Parent |
368434 |
Jun 1973 |
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