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Aluminum alloys with grain refiners, and methods for making and using the same

Pending Publication Date: 2019-01-31
HRL LAB
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The patent text claims that the microstructure of additively manufactured aluminum alloy is free of cracks and porous void defects. This results in a high quality product that can be used in various applications.

Problems solved by technology

The vast majority of the more than 5,500 alloys in use today cannot be additively manufactured because the melting and solidification dynamics during the printing process lead to intolerable microstructures with large columnar grains and cracks.
3D-printable metal alloys are limited to those known to be easily weldable.
The limitations of the currently printable alloys, especially with respect to specific strength, fatigue life, and fracture toughness, have hindered metal-based additive manufacturing.
In contrast, most aluminum alloys used in automotive, aerospace, and consumer applications are wrought alloys of the 2000, 5000, 6000, or 7000 series, which can exhibit strengths exceeding 400 MPa and ductility of more than 10% but cannot currently be additively manufactured.
These same elements promote large solidification ranges, leading to hot tearing (cracking) during solidification—a problem that has been difficult to surmount for more than 100 years since the first age-hardenable alloy, duralumin, was developed.
This mechanism results in solute enrichment in the liquid near the solidifying interface, locally changing the equilibrium liquidus temperature and producing an unstable, undercooled condition.
As a result, there is a breakdown of the solid-liquid interface leading to cellular or dendritic grain growth with long channels of interdendritic liquid trapped between solidified regions.
As temperature and liquid volume fraction decrease, volumetric solidification shrinkage and thermal contraction in these channels produces cavities and hot tearing cracks which may span the entire length of the columnar grain and can propagate through additional intergranular regions.
Note that aluminum alloys Al 7075 and Al 6061 are highly susceptible to the formation of such cracks, due to a lack of processing paths to produce fine equiaxed grains.
Producing equiaxed structures requires large amounts of undercooling, which has thus far proven difficult in additive processes where high thermal gradients arise from rastering of a direct energy source in an arbitrary geometric pattern.

Method used

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  • Aluminum alloys with grain refiners, and methods for making and using the same
  • Aluminum alloys with grain refiners, and methods for making and using the same
  • Aluminum alloys with grain refiners, and methods for making and using the same

Examples

Experimental program
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Effect test

example 1

inement of Pure Aluminum

[0307]In this example, tantalum (Ta) particles are added to pure aluminum as a grain refiner, and compared to pure aluminum with no Ta particle addition. The concentration of Ta in the aluminum-tantalum material is about 1 vol %. The average Ta particle size is approximately 50 nm. In both cases, the metal or functionalized metal is melted and resolidified by selective laser melting.

[0308]FIG. 6A shows an image of non-grain-refined pure aluminum, revealing large columnar grains. FIG. 6B shows an image of grain-refined aluminum with Ta particles, revealing fine equiaxed growth and a substantially crack-free microstructure.

[0309]This example demonstrates the effectiveness of grain refinement of pure aluminum using Ta addition.

example 2

inement of Aluminum Alloy Al 7075

[0310]In this example, zirconium (Zr) nanoparticles are added to aluminum alloy Al 7075 as a grain refiner, and compared to pure Al 7075 with no Zr nanoparticle addition. The concentration of Zr in the functionalized alloy is about 1 vol %. The average Zr nanoparticle size is approximately 500-1500 nm. In both cases, the alloy or functionalized alloy is melted and resolidified by selective laser melting.

[0311]FIG. 7A shows an image of non-grain-refined aluminum alloy Al 7075, revealing columnar grains and significant cracking. FIG. 7B shows an image of grain-refined aluminum alloy Al 7075 with Zr particles, revealing fine equiaxed grains and a substantially crack-free microstructure. Without being limited by theory, it is believed that Zr forms a preferred nucleating phase at sufficient concentration to reduce the critical undercooling required for equiaxed nucleation.

[0312]It is also noted that both of FIGS. 7A and 7B (scale bars 100 μm) exhibit a c...

example 3

Manufacturing of Aluminum Alloy Al 7075 with Zr Grain Refiner

[0314]In this example, zirconium (Zr) nanoparticles are first added to aluminum alloy Al 7075. The concentration of Zr in the functionalized alloy is about 1 vol %. The average Zr nanoparticle size is approximately 500-1500 nm. The functionalized alloy is solution heat-treated and artificially aged, which is indicated by “T6” in the alloy name (Al 7075+Zr-T6), as described above. A control aluminum alloy, Al 7075-T6, is compared to Al 7075+Zr-T6, as is AlSi10Mg, another common alloy for comparison.

[0315]The functionalized alloy (Al 7075+Zr-T6) is 3D-printed by selective laser melting. The control alloys Al 7075-T6 and AlSi10Mg are 3D-printed with the same technique. It is believed that at least a portion of the Zr nanoparticles are in the form of Al3Zr nucleant particles following 3D printing.

[0316]FIG. 9 shows a stress-strain curve of the functionalized aluminum alloy versus the two non-functionalized aluminum alloys, ind...

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Abstract

We have developed a scalable approach to directly incorporate grain-refining nanoparticles into conventional hot-tear-susceptible aluminum alloy powders. These aluminum alloy powders may be additively manufactured into high-strength, crack-free aluminum alloys with fine equiaxed microstructures by incorporating nanoparticle nucleants to control solidification during additive manufacturing. Some variations provide an additively manufactured aluminum alloy comprising aluminum, one or more strengthening elements, and at least one grain-refining element, wherein the additively manufactured aluminum alloy has a microstructure with equiaxed grains. Aluminum alloys with grain refiners are useful in many processes beyond additive manufacturing. Some variations provide an aluminum alloy comprising aluminum, copper, magnesium, at least one of zinc or silicon, and grain-refining nanoparticles selected from zirconium, tantalum, niobium, or titanium, wherein the aluminum alloy has a microstructure that is substantially crack-free with equiaxed grains.

Description

PRIORITY DATA[0001]This patent application is a non-provisional application with priority to U.S. Provisional Patent App. No. 62 / 452,989, filed on Feb. 1, 2017, which is hereby incorporated by reference herein.FIELD OF THE INVENTION[0002]The present invention generally relates to metal alloys with grain refiners, and methods of making and using the same.BACKGROUND OF THE INVENTION[0003]Aluminum and its alloys are characterized by a relatively low density, high electrical and thermal conductivities, and a resistance to corrosion in some common environments, including the ambient atmosphere. Recent attention has been given to alloys of aluminum as engineering materials for transportation to reduce fuel consumption due to high specific strength. The mechanical strength of aluminum may be enhanced by cold work and by alloying. Principal alloying elements include copper, magnesium, silicon, zinc, and manganese.[0004]Generally, aluminum alloys are classified as either cast or wrought. Som...

Claims

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Application Information

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IPC IPC(8): C22C21/10C22F1/053B33Y80/00B23K26/342B22F1/16B22F1/17
CPCC22C21/10C22F1/053B33Y80/00B23K26/342B23K2103/10C22C21/00C22C32/00C22C32/001C22C32/0052C22C32/0068C22C32/0073C22C32/0089C22C32/0005C22C32/0047C22C32/0031B22F1/065B33Y70/00C22C21/16C22C21/06C22C21/02C22C21/08C22C21/14C22C21/18C22C21/04C22C1/0416C22C1/10C22C1/1084Y02P10/25B22F1/17B22F1/16B22F10/66B22F10/25B22F10/28B22F10/64B22F10/36B22F10/38B22F10/366B22F10/32B22F10/68B33Y70/10C22C1/047
Inventor MARTIN, JOHN H.YAHATA, BRENNAN
Owner HRL LAB
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