8000-SERIES ALUMINUM ALLOY

Abstract

An 8000-series aluminum alloy, useful to form wires, including a rare-earth element. The alloy exhibits improved creep resistance and stress relaxation resistance, as compared to the same alloy that is substantially free of the rare-earth element, while the electrical conductivity of the alloy is substantially unaffected by the addition of the rare-earth element.

Description

The present application claims the benefit of the filing date of U.S. Ser. No. 62/595,781, filed 7 Dec. 2017 and entitled 8000-Series Aluminum Alloy.

TECHNICAL FIELD

The present disclosure generally relates to an improved 8030 aluminum alloy exhibiting high creep resistance and stress relaxation resistance.

BACKGROUND

Some applications, such as cable building wire, have been formed predominantly of copper due to copper's high electrical conductivity and excellent mechanical properties. Despite these qualities, it would be advantageous in those applications to use an aluminum alloy as a consequence of aluminum's higher electrical conductivity, when compared to copper, on a unit weight basis. However, such applications such as cable wires formed of typical aluminum alloys exhibit low creep resistance and stress relaxation resistance, causing cables, for example, formed from such alloys to exhibit poor termination performance making such conductors unsuitable for use in buildings. It would be advantageous to form an improved aluminum alloy which balances high electrical conductivity with high creep resistance and stress relaxation resistance.

SUMMARY

In accordance with one embodiment, an improved 8000-series aluminum alloy includes, by weight, about 0.30% to about 0.80% iron, about 0.10% to about 0.30% copper, and about 0.005% to about 0.1% of a rare-earth element (REE). The REE is selected from one or more of erbium, ytterbium, and scandium, and preferably from one or both of erbium and ytterbium.

In accordance with another embodiment, an improved 8000-series aluminum alloy includes, by weight, about 0.30% to about 0.80% iron, about 0.01% to about 0.20% silicon, and about 0.005% to about 0.1% of a REE. The REE is selected from one or more of erbium, ytterbium, and scandium, and preferably from one or both of erbium and ytterbium.

In accordance with another embodiment, a method of improving a standard 8000-series aluminum alloy includes melting the elements required by and in a proportion permitted by a definition of a standard 8000-series aluminum alloy (or possibly melting a composed standard 8000-series aluminum alloy); and admixing about 0.005% to about 0.1%, by weight, of a REE to form an improved 8000-series aluminum alloy. The REE is selected from one or more of erbium, ytterbium, and scandium, and preferably from one or both of erbium and ytterbium. The standard 8000-series aluminum alloy is one of an AA8030 aluminum alloy, an AA8176 aluminum alloy, and an AA8017 aluminum alloy.

DETAILED DESCRIPTION

As will be described herein, aluminum alloys exhibiting a balance of high electrical conductivity as well as high creep resistance and high stress relaxation resistance are disclosed. The aluminum alloys are suitable to form conductors for wires, such as cable building wires. Cables formed from such aluminum alloys can dependably be terminated at building sockets and terminals. Generally, such improved aluminum alloys can be formed through the inclusion of a suitable REE to certain 8000-series aluminum alloys to improve the creep resistance and stress relaxation resistance without impairing the electrical conductivity of the standard 8000-series aluminum alloy.

As can be appreciated, cable building wire is connected to, and terminated at, receptacles such as power outlets. Termination of cable building wire is typically accomplished by making an electrical connection with the terminal and then using a screw to secure the connection. As can be appreciated, various physical characteristics are important to prevent loosening and failure of a termination over time including the creep resistance and stress relaxation resistance characteristics exhibited by the cable. Creep is the measurement of the rate of change of a material's dimensions over a period of time when subjected to an applied force and controlled temperature. Stress relaxation is the time dependent decrease in stress of a metal under constant strain. Cables formed of metals having low resistance to creep and stress relaxation can deform and can cause undesirable failure of the termination due to loss of electrical contact.

As can be further appreciated, the electrical and mechanical properties of a metal can be influenced through several mechanisms including through the incorporation of additional elements to form alloys and through mechanical and thermal treatment of the metal. Such mechanisms can improve the creep and stress relaxation performance of a metal.

A number of aluminum alloy grades have been standardized by the Accrediting Standards Committee H35 of the Aluminum Association. Standardized aluminum grades are defined by their elemental compositions with the various grades generally intended for specific applications and industries. For example, 1000-series aluminum alloys are defined as being high purity aluminum alloys and 7000-series aluminum alloys are defined as zinc and magnesium containing alloys. 1000-series aluminum alloys are useful in the overhead conductor industry while 7000-series aluminum alloys are useful in the aerospace industry. Certain 8000-series aluminum alloys have been standardized to provide aluminum alloys useful for the construction of cable wires. 8000-series aluminum alloys can include silicon, iron, copper, magnesium, zinc, and boron.

Specifically, certain 8000-series aluminum alloys, such as AA8176 and AA8030, can exhibit improved creep and stress relaxation resistance when compared to conventional aluminum alloys, such as AA1350. However, the creep resistance and stress relaxation resistance of such 8000-series alloys is still lower than comparable creep and stress relaxation values for the copper typically used to form cable building wire. This discrepancy can cause cables formed from 8000-series aluminum alloys to experience termination failure. The inventors have discovered that the addition of REEs to certain 8000-series alloys, such as AA8030, can allow for the formation of an aluminum alloy which exhibits higher creep resistance and stress relaxation resistance while still maintaining the electrical conductivity of the original alloy.

In certain embodiments, a suitable REE can be one or more of erbium, ytterbium, and scandium, and preferably one or both of erbium and ytterbium in view of relative costs. For example, in certain embodiments, the addition of trace amounts of erbium can increase the creep resistance, increase the stress relaxation resistance, and increase the tensile strength of an AA8030 alloy without reducing the electrical conductivity or the elongation at break values of the original alloy.

As can be appreciated, the elongation at break values of the aluminum alloys described herein can be greater than comparable elongation at break values for copper cable building wires. Improved elongation at break values can facilitate the tension forces required to pull cable wire through walls and plenum. In certain embodiments, the aluminum alloys used to form the cable building wires described herein can have an elongation at break value of about 15% to about 50%.

In certain embodiments, a REE can be added at about 0.001% to about 0.1% by weight of the aluminum alloy including, for example, at about 0.01% by weight of the aluminum alloy, at about 0.02% by weight of the aluminum alloy, at about 0.03% by weight of the aluminum alloy, and at about 0.04% by weight of the aluminum alloy.

In certain embodiments, the REE can be added to a standard 8000-series aluminum alloy, such as AA8030 aluminum alloy. AA8030 aluminum alloys are defined by unified number system (“UNS”) AA8030 standard and include, by weight, 0.30% to 0.80% iron, 0.15% to 0.30% copper, 0.10% or less silicon, 0.050% or less magnesium, 0.050% or less zinc, 0.0010% to 0.040% boron, and 0.030% or less of each other element with a total of less than 0.10% other elements, and the balance being aluminum. Known AA8030 aluminum alloys can exhibit a tensile creep rate at 100° C. under 45.5 MPa of stress of about 9.8*10⁻⁶ s⁻¹, and tensile stress relaxation times of about 660 seconds to reach 85% of an initial stress of 75 MPa at room temperature (e.g., at about 23° C.).

Alternatively, in other certain embodiments, the REE can be added to an AA8176 or an AA8017 aluminum alloy. AA8176 aluminum alloys include, by weight, 0.40% to 1.00% iron, less than 0.10% zinc, 0.030% to 0.15% silicon, 0.030% or less gallium, and 0.050% or less of each other element with a total of less than 0.15% other elements, and the balance being aluminum. AA8017 aluminum alloys include, by weight, 0.55% to 0.80% iron, 0.10% to 0.20% copper, 0.10% or less silicon, 0.05% or less zinc, 0.04% or less boron, 0.01% to 0.05% magnesium, 0.003% or less lithium, and 0.03% or less of each other element with a total of less than 0.10% other elements, and the balance being aluminum. As can be appreciated however, the REE can also be added to other aluminum alloys formed of iron, copper, and other elements.

As can be appreciated, certain aluminum alloys described herein can still satisfy the requirements of standardized aluminum alloy grades. For example, the inclusion of about 0.01% to about 0.03%, by weight, of a REE to an AA8030 aluminum alloy is permitted by the AA8030 standard and inventive aluminum alloys AlFe_0.44Cu_0.17Si_0.02Er_0.01, AlFe_0.44Cu_0.17Si_0.02Er_0.02, and AlFe_0.44Cu_0.17Si_0.02Er_0.03, for example, can be considered AA8030 aluminum alloys. Certain inventive aluminum alloys can also be AA8176 or AA8017 aluminum alloys. As can be appreciated, however, certain aluminum alloys described herein alternatively may be outside the standards of any named aluminum alloys.

The addition of a REE can increase resistance to tensile creep and resistance to tensile stress relaxation. For example, the addition of about 0.01% to about 0.03% erbium to an AA8030 aluminum alloy can lower the tensile creep rate at 100° C. under 70 MPa of stress to about 1.0*10⁻⁵ s⁻¹ to about 2.0*10⁻⁷ s⁻¹. As can be appreciated, such improvements can be a 20× to 30×, or even greater, increase in tensile creep resistance as compared to a similar alloy formed without the REE. For an AA8176 aluminum alloy, the addition of about 0.01% to about 0.05% erbium can lower the tensile creep to less than about 2*10⁻⁷ s⁻⁷ under 70 MPa tensile stress at 100° C. Similarly, for an AA8017 aluminum alloy, the addition of about 0.01% to about 0.03% erbium can lower the tensile creep to about 1*10⁻⁶ s⁻¹ to about 1*10⁻⁸ s⁻¹ under 70 MPa tensile stress at 100° C.

Similarly, the tensile stress relaxation resistance of an improved AA8030 aluminum alloy including about 0.01% to about 0.03% erbium can improve the tensile stress relaxation time required to reach 85% of an initial stress, when measured at 25° C., to about 1,200 seconds to about 1,700 seconds. As can be appreciated, this is about a 2× improvement in stress relaxation times. For AA8176 and AA8017, the addition of about 0.01% to about 0.05% erbium can improve the tensile stress relaxation time required to reach 88% of an initial stress of 75 MPa, when measured at 25° C. to 2,500 seconds or greater for each alloy.

As can be appreciated, however, the inclusion and modification of the elements in an aluminum alloy can have a dramatic impact on various characteristics of the alloy. For example, the inclusion of about 0.03% zirconium can improve the creep and stress relaxation properties of an aluminum alloy but can undesirably lower the electrical conductivity of the alloy by about 1% as measured by the International Annealed Copper Standard (“IACS”). Similarly, including an additional 0.13% copper in an AA8030 alloy containing 0.44% iron and 0.17% copper (to form AlFe_0.44Cu_0.30) can cause a 1.4% IACS decrease in electrical conductivity.

Surprisingly, the addition of a REE as described herein can maintain the characteristics of the original alloy, such as electrical conductivity, while improving the creep resistance and stress relaxation resistance of the original alloy. For example, improved AA8030 aluminum alloys including a REE can maintain an IACS value of about 61.3% to about 61.4% as compared to an IACS value of about 61.2% for a standard AA8030 aluminum alloy formed without the REE.

Without being bound by theory, it is believed that the inclusion of a REE can improve the properties of an aluminum alloy by forming structured nano-precipitates which provide strength to reduce creep and stress relaxation. For example, it is believed that the addition of erbium can form Al₃Er (L1₂ structure) structured nano-precipitates and the addition of scandium can form Al₃Sc nano-precipitates. As can be appreciated, such nano-precipitates are stable at both room temperature and at elevated temperatures and can be effective in impeding the dislocation motion which causes creep and stress relaxation. It is additionally believed that such nano-precipitates can synergistically work with the precipitates formed from the interactions of the iron and copper found in the unmodified 8000-series aluminum alloy.

For example, in certain embodiments, iron can be included in an aluminum alloy as described herein at about 0.44%, by weight, or greater. Such iron loading levels can ensure that the aluminum alloy has sufficient precipitation of Al₆(Cu, Fe). As can be appreciated, increasing the loading level of copper can lower the electrical conductivity of an aluminum alloy making it more desirable in certain embodiments to increase the weight percentage of iron.

Generally, the aluminum alloys described herein can be formed in any manner known in the art. For example, the aluminum alloys can be formed by casting an as-cast shape, hot rolling the as-cast shape into a redraw rod, and then drawing the redraw rod into a conductive element, such as a wire. This process can be performed continuously. Additional details of forming an aluminum alloy are disclosed in U.S. patent application Ser. No. 15/294,273 and U.S. Patent App. Publication No. 2015/0259773 each of which is incorporated herein by reference.

Cables formed from the aluminum alloys described herein can be useful as cable building wire. In certain embodiments, the cables can be used with standard building connectors such as connectors which comply with the requirements of UL 486A. Generally, the cable building wires can be used as known in the art. For example, the building cable wires can be installed and used in compliance with NECA/AA 104-2000 standards.

The cable building wires can be formed in any suitable manner. For example, the metal alloys described herein can be formed into stranded or solid conductors in various embodiments. Additionally, the cable building wires can be formed of any suitable gauge as determined by the various needs of a particular application. For example, in certain embodiments, building cable wires can be 8 American wire gauge (“AWG”), 10 AWG, or 12 AWG. Additionally, the building cable wire can be coated with an insulator or jacket as known in the art. The building cable wires disclosed herein can weigh less than a copper building cable wire conducting a similar amount of ampacity.

The aluminum alloys described herein also can be used to form alternative articles in certain embodiments. For example, the aluminum alloys can be used to form conductive elements inside of a power receptacle or can be used to form articles which must be resistant to creep.

Examples

Tables 1 to 3 depict the mechanical and electrical properties of several Example aluminum alloys. The measured properties include the ultimate tensile strength (“UTS”), the elongation at break, the electrical conductivity as measured by the International Annealed Copper Standard (“IACS”), the tensile creep rate as measured at 100° C. under 70 MPa of applied stress, and the tensile stress relaxation time as measured by the time the stress of a sample reaches 85% (Table 1) or 88% (Tables 2 and 3) of the initial stress when measured at 25° C. Ultimate tensile strength was measured in accordance to ASTM B941; tensile creep was measured in accordance to ASTM E139; and tensile stress relaxation time was measured in accordance to ASTM E328.

Table 1 depicts examples of AA8030 aluminum alloys. Table 2 depicts examples of AA8176 aluminum alloys. Table 3 depicts examples of AA8017 aluminum alloys.

TABLE 1
				Tensile	Tensile stress
		Elongation		creep	relaxation
	UTS	at break	IACS	rate	to 85% initial
Example	(MPa)	(%)	(%)	(s−1)	stress (s)
Comp. Ex. 1. - AA8030	96 ± 1	23 ± 2	61.2	~1*10−3	650
(AlFe0.44Cu0.17Si0.02)
Inv. Ex. 2. - AA8030	101 ± 1	21 ± 2	61.3	~1*10−5	1,350
(AlFe0.44Cu0.17Si0.02Er0.01)
Inv. Ex. 3. - AA8030	100 ± 1	20 ± 2	61.4	~1*10−5	1,210
(AlFe0.44Cu0.17Si0.02Er0.02)
Inv. Ex. 4. - AA8030	101 ± 1	20 ± 2	61.4	~1*10−5	1,400
(AlFe0.44Cu0.17Si0.02Er0.03)
Inv. Ex. 5. -	100 ± 1	21 ± 2	60.8	~1*10−5	1,700
(AlFe0.44Cu0.17Si0.02Er0.04)

TABLE 2
				Tensile	Tensile stress
		Elongation		creep	relaxation
	UTS	at break	IACS	rate	to 88% initial
Example	(MPa)	(%)	(%)	(s−1)	stress (s)
Comp. Ex. 6. - AA8176	98 ± 2	14 ± 1	60.6	~2*10−6	220
(AlFe0.55Si0.04)
Inv. Ex. 7. - AA8176	106 ± 2	10 ± 2	60.3	~2*10−7	650
(AlFe0.55Si0.04Er0.005)
Inv. Ex. 8. - AA8176	116 ± 2	8 ± 1	60.6	~2*10−8	2,550
(AlFe0.55Si0.04Er0.01)
Inv. Ex. 9. - AA8176	127 ± 1	5 ± 0.5	60.6	<1*10−8	3,050
(AlFe0.55Si0.04Er0.02)
Inv. Ex. 10. - AA8176	133 ± 1	6 ± 1	60.5	<1*10−8	3,900
(AlFe0.55Si0.04Er0.03)
Inv. Ex. 11. -	136 ± 1	3 ± 0.1	60.7	<1*10−8	4,900
(AlFe0.55Si0.04Er0.05)

TABLE 3
				Tensile	Tensile stress
		Elongation		creep	relaxation
	UTS	at break	IACS	rate	to 88% initial
Example	(MPa)	(%)	(%)	(s−1)	stress (s)
Comp. Ex. 12. - AA8017	107 ± 1	16 ± 2	61.0	~2*10−6	1,050
(AlFe0.55Cu0.17Mg0.03Si0.02)
Inv. Ex. 13. - AA8017	115 ± 1	14 ± 1	60.8	~7*10−7	2,750
(AlFe0.55Cu0.17Mg0.03Si0.02Er0.02)

As depicted by Tables 1 to 3, the Inventive Examples exhibited significantly improved tensile creep resistance and tensile stress relaxation resistance as compared to their respective Comparative Examples while maintaining electrical conductivity.

In some embodiments, an 8000-series aluminum alloy comprises: aluminum; about 0.30% to about 0.80%, by weight, iron; about 0.10% to about 0.30%, by weight, copper, and about 0.001% to about 0.1%, by weight, of a REE selected from one or more of erbium, ytterbium, and scandium, and preferably from one or both of erbium and ytterbium. In some embodiments, the alloy comprises about 0.005% to about 0.1%, by weight, of the REE. In some embodiments, the alloy comprises about 0.01% to about 0.03%, by weight, of the REE. In some embodiments, the alloy further comprises: about 0.02%, by weight, silicon; the alloy comprises about 0.44%, by weight, iron, and about 0.17%, by weight, copper; the REE comprises about 0.01% to about 0.03%, by weight, erbium; and the alloy is an AA8030 aluminum alloy. In some embodiments, the AA8030 alloy exhibits one or more of: i) a tensile creep rate of about 1*10⁻⁵ s⁻¹ to about 2*10⁻⁸ s⁻¹ when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 1,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8030 alloy exhibits: i) a tensile creep rate of about 1*10⁻⁵ s⁻¹ to about 2*10⁻⁸ s⁻¹ when measured in accordance to ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 1,000 seconds or greater when measured in accordance to ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8030 alloy exhibits an electrical conductivity at least as great as an electrical conductivity of an AA8030 aluminum alloy substantially free of the REE. In some embodiments, the AA8030 alloy exhibits an ultimate tensile strength of at least about 99 MPa when measured in accordance with ASTM B941. In some embodiments, the AA8030 alloy exhibits an elongation at break at least as great as an elongation at bread of an AA8030 aluminum alloy substantially free of the REE. In some embodiments, the 8000-series aluminum alloy further comprises: about 0.03%, by weight, magnesium, and about 0.02%, by weight, silicon; the alloy comprises about 0.55%, by weight, iron, and about 0.17%, by weight, copper; the REE comprises about 0.01% to about 0.03%, by weight, erbium; and the alloy is an AA8017 aluminum alloy. In some embodiments, the AA8017 alloy exhibits one or more of: i) a tensile creep rate of about 1*10⁻⁵ s⁻¹ to about 2*10⁻⁸ s⁻¹ when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8017 alloy exhibits: i) a tensile creep rate of about 1*10⁻⁵ s⁻¹ to about 2*10⁻⁸ s⁻¹ when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8017 alloy exhibits an electrical conductivity at least as great as an electrical conductivity of an AA8017 aluminum alloy substantially free of the REE. In some embodiments, the AA8017 alloy exhibits an ultimate tensile strength of at least about 114 MPa when measured in accordance with ASTM B941.

In some embodiments, an 8000-series aluminum alloy comprises: aluminum; about 0.30% to about 0.80%, by weight, iron; about 0.01% to about 0.20%, by weight, silicon; and about 0.001% to about 0.1%, by weight, of a REE selected from one or more of erbium, ytterbium, and scandium, and preferably from one or both of erbium and ytterbium. In some embodiments, the alloy comprises about 0.005% to about 0.1%, by weight, of the REE. In some embodiments, the alloy comprises about 0.01% to about 0.05%, by weight, of the REE. In some embodiments, the alloy comprises about 0.55%, by weight, iron, and about 0.04%, by weight, silicon; the REE comprises about 0.005% to about 0.05%, by weight, erbium; and the alloy is an AA8176 aluminum alloy. In some embodiments the AA8176 alloy exhibits one or more of: i) a tensile creep rate of less than about 2*10⁻⁷ s⁻¹ when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.0% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8176 alloy exhibits: i) a tensile creep rate of less than about 2*10⁻⁷ s⁻¹ when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress; ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and iii) an electrical conductivity of about 60.0% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”). In some embodiments, the AA8176 alloy exhibits an ultimate tensile strength of at least about 104 MPa when measured in accordance with ASTM B941.

In some embodiments, a method of making an 8000-series aluminum alloy comprises: making a melt comprising the following constituents: a) each of the elements that is both required by and in a proportion permitted by a definition of a standard aluminum alloy selected from a group consisting of AA8030, AA8176, and AA8017; and b) about 0.001% to about 0.1%, by weight, of a REE, the REE consisting of one or more of erbium, ytterbium, and scandium, and preferably one or both of erbium and ytterbium; and solidifying the melt, and cooling a resulting solid piece. In some embodiments, the method comprises the REE comprising about 0.005% to about 0.05%, by weight, of erbium.

It should be understood that every maximum numerical limitation given throughout this specification includes every lower numerical limitation, as if such lower numerical limitations were expressly written herein. Every minimum numerical limitation given throughout this specification will include every higher numerical limitation, as if such higher numerical limitations were expressly written herein. Every numerical range given throughout this specification will include every narrower numerical range that falls within such broader numerical range, as if such narrower numerical ranges were all expressly written herein.

Every document cited herein, including any cross-referenced or related patent or application, is hereby incorporated herein by reference in its entirety unless expressly excluded or otherwise limited. The citation of any document is not an admission that it is prior art with respect to any invention disclosed or claimed herein or that it alone, or in any combination with any other reference or references, teaches, suggests, or discloses any such invention. Further, to the extent that any meaning or definition of a term in this document conflicts with any meaning or definition of the same term in a document incorporated by reference, the meaning or definition assigned to that term in the document shall govern.

The foregoing description of embodiments and examples has been presented for purposes of description. It is not intended to be exhaustive or limiting to the forms described. Numerous modifications are possible in light of the above teachings. Some of those modifications have been discussed and others will be understood by those skilled in the art. The embodiments were chosen and described for illustration to those of ordinary skill in the art. The scope of the claims is not limited to the examples or embodiments set forth herein.

Claims

1. An 8000-series aluminum alloy comprising:

aluminum;

about 0.30% to about 0.80%, by weight, iron;

about 0.10% to about 0.30%, by weight, copper; and

about 0.001% to about 0.10/%, by weight, of a rare-earth element (REE) selected from one or both of erbium and ytterbium.

2. The 8000-series aluminum alloy of claim 1, wherein the alloy comprises about 0.005% to about 0.1%, by weight, of the REE.

3. The 8000-series aluminum alloy of claim 1, wherein the alloy comprises about 0.01% to about 0.03%, by weight, of the REE.

4. The 8000-series aluminum alloy of claim 1, the alloy further comprising:

about 0.02%, by weight, silicon; and

wherein the alloy comprises about 0.44%, by weight, iron, and about 0.17%, by weight, copper,

wherein the REE comprises about 0.01% to about 0.03%, by weight, erbium; and

wherein the alloy is an AA8030 aluminum alloy.

5. The 8000-series aluminum alloy of claim 4, wherein the alloy exhibits one or more of:

i) a tensile creep rate of about 1*10−5 s−1 to about 2*10−8 s−1 when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 1,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

6. The 8000-series aluminum alloy of claim 4, wherein the alloy exhibits:

i) a tensile creep rate of about 1*10−5 s−1 to about 2*10−8 s−1 when measured in accordance to ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 1,000 seconds or greater when measured in accordance to ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

7. The 8000-series aluminum alloy of claim 4, wherein the alloy exhibits an electrical conductivity at least as great as an electrical conductivity of an AA8030 aluminum alloy substantially free of the REE.

8. The 8000-series aluminum alloy of claim 4, wherein the alloy exhibits an ultimate tensile strength of at least about 99 MPa when measured in accordance with ASTM B941.

9. The 8000-series aluminum alloy of claim 4, wherein the alloy exhibits an elongation at break at least as great as an elongation at break of an AA8030 aluminum alloy substantially free of the REE.

10. The 8000-series aluminum alloy of claim 1, the alloy further comprising:

about 0.03%, by weight, magnesium; and

about 0.02%, by weight, silicon; and

wherein the alloy comprises about 0.55%, by weight, iron, and about 0.17%, by weight, copper,

wherein the REE comprises about 0.01% to about 0.03%, by weight, erbium; and

wherein the alloy is an AA8017 aluminum alloy.

11. The 8000-series aluminum alloy of claim 10, wherein the alloy exhibits one or more of:

i) a tensile creep rate of about 1*10−5 s−1 to about 2*10−8 s−1 when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

12. The 8000-series aluminum alloy of claim 10, wherein the alloy exhibits:

i) a tensile creep rate of about 1*10−5 s−1 to about 2*10−8 s−1 when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.5% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

13. The 8000-series aluminum alloy of claim 10, wherein the alloy exhibits an electrical conductivity at least as great as an electrical conductivity of an AA8017 aluminum alloy substantially free of the REE.

14. The 8000-series aluminum alloy of claim 10, wherein the alloy exhibits an ultimate tensile strength of at least about 114 MPa when measured in accordance with ASTM B941.

15. An 8000-series aluminum alloy comprising:

aluminum;

about 0.30% to about 0.80%, by weight, iron;

about 0.01% to about 0.20%, by weight, silicon; and

about 0.001% to about 0.1%, by weight, of a rare-earth element (REE) selected from one or both of erbium and ytterbium.

16. The 8000-series aluminum alloy of claim 15, wherein the alloy comprises about 0.005% to about 0.1%, by weight, of the REE.

17. The 8000-series aluminum alloy of claim 15, wherein the alloy comprises about 0.01% to about 0.05%, by weight, of the REE.

18. The 8000-series aluminum alloy of claim 15,

wherein the alloy comprises about 0.55%, by weight, iron, and about 0.04%, by weight, silicon;

wherein the REE comprises about 0.005% to about 0.05%, by weight, erbium; and

wherein the alloy is an AA8176 aluminum alloy.

19. The 8000-series aluminum alloy of claim 18, wherein the alloy exhibits one or more of:

i) a tensile creep rate of less than about 2*10−7 s−1 when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.0% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

20. The 8000-series aluminum alloy of claim 18, wherein the alloy exhibits:

i) a tensile creep rate of less than about 2*10−7 s−1 when measured in accordance with ASTM E139 at 100° C. with 70 MPa of applied stress;

ii) a tensile strength relaxation time, to reach about 85% of 75 MPa initial tensile stress, of about 2,000 seconds or greater when measured in accordance with ASTM E328 at 25° C.; and

iii) an electrical conductivity of about 60.0% or greater when measured in accordance with the International Annealed Copper Standard (“IACS”).

21. The 8000-series aluminum alloy of claim 18, wherein the alloy exhibits an ultimate tensile strength of at least about 104 MPa when measured in accordance with ASTM B941.

22. A method of making an 8000-series aluminum alloy, the method comprising:

making a melt comprising the following constituents: a) each of the elements that is both required by and in a proportion permitted by a definition of a standard aluminum alloy selected from a group consisting of AA8030, AA8176, and AA 8017; and b) about 0.001% to about 0.1%, by weight, of a rare-earth element (REE), the REE consisting of one or both of erbium and ytterbium; and

solidifying the melt, and cooling a resulting solid piece.

23. The method of claim 22, wherein the REE comprises about 0.005% to about 0.05%, by weight, of erbium.