ALUMINUM ALLOY WIRE ROD, ALUMINUM ALLOY STRANDED WIRE, COVERED WIRE, AND WIRE HARNESS, AND METHOD OF MANUFACTURING ALUMINUM ALLOY WIRE ROD

Abstract

An aluminum alloy wire rod having a composition comprising Mg: 0.1-1.0 mass %, Si: 0.1-1.2 mass %, Fe: 0.10-1.40 mass %, Ti: 0-0.100 mass %, B: 0-0.030 mass %, Cu: 0-1.00 mass %, Ag: 0-0.50 mass %, Au: 0-0.50 mass %, Mn: 0-1.00 mass %, Cr: 0-1.00 mass %, Zr: 0-0.50 mass %, Hf: 0-0.50 mass %, V: 0-0.50 mass %, Sc: 0-0.50 mass %, Co: 0-0.50 mass %, Ni: 0-0.50 mass %, and the balance: Al and inevitable impurities, wherein a number of compound particles present on a surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is less than or equal to one per 100 μm.sup.2, and a tensile strength is greater than or equal to 200 MPa.

Claims

1. An aluminum alloy wire rod having a composition comprising Mg: 0.1 mass % to 1.0 mass %, Si: 0.1 mass % to 1.2 mass %, Fe: 0.10 mass % to 1.40 mass %, Ti: 0 mass % to 0.100 mass %, B: 0 mass % to 0.030 mass %, Cu: 0 mass % to 1.00 mass %, Ag: 0 mass % to 0.50 mass %, Au: 0 mass % to 0.50 mass %, Mn: 0 mass % to 1.00 mass %, Cr: 0 mass % to 1.00 mass %, Zr: 0 mass % to 0.50 mass %, Hf: 0 mass % to 0.50 mass %, V: 0 mass % to 0.50 mass %, Sc: 0 mass % to 0.50 mass %, Co: 0 mass % to 0.50 mass %, Ni: 0 mass % to 0.50 mass %, and the balance: Al and inevitable impurities, wherein a number of compound particles present on a surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is less than or equal to one per 100 μm.sup.2, and a tensile strength is greater than or equal to 200 MPa.

2. The aluminum alloy wire rod according to claim 1, wherein the composition comprises both of or any one of Ti: 0.001 mass % to 0.100 mass % and B: 0.001 mass % to 0.030 mass %.

3. The aluminum alloy wire rod according to claim 1, wherein the composition comprises at least one of Cu: 0.01 mass % to 1.00 mass %, Ag: 0.01 mass % to 0.50 mass %, Au: 0.01 mass % to 0.50 mass %, Mn: 0.01 mass % to 1.00 mass %, Cr: 0.01 mass % to 1.00 mass %, Zr: 0.01 mass % to 0.50 mass %, Hf: 0.01 mass % to 0.50 mass %, V: 0.01 mass % to 0.50 mass %, Sc: 0.01 mass % to 0.50 mass %, Co: 0.01 mass % to 0.50 mass % and Ni: 0.01 mass % to 0.50 mass %.

4. The aluminum alloy wire rod according to claim 1, wherein a sum of contents of Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni is 0.10 mass % to 2.00 mass %.

5. The aluminum alloy wire rod according to claim 1, wherein the compound particles are Fe-based compound particles.

6. The aluminum alloy wire rod according to claim 1, wherein a thickness of a surface oxide layer is less than or equal to 500 nm.

7. The aluminum alloy wire rod according to claim 1, wherein the aluminum alloy wire rod has a plated film on a surface thereof, and a presence ratio of pinholes each having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is less than or equal to one pinhole/mm.sup.2.

8. The aluminum alloy wire rod according to claim 1, wherein the aluminum alloy wire rod is an aluminum alloy wire having a strand diameter of 0.1 mm to 0.5 mm.

9. An aluminum alloy stranded wire obtained by stranding a plurality of the aluminum alloy wires as claimed in claim 8.

10. A covered wire comprising a covering layer at an outer periphery of one of the aluminum alloy wire as claimed in claim 8.

11. A wire harness comprising: a covered wire including a covering layer at an outer periphery of one of an aluminum alloy wire rod and an aluminum alloy stranded wire; and a terminal fitted at an end portion of the covered wire, the covering layer being removed from the end portion, wherein the aluminum alloy wire rod had a composition comprising Mg: 0.1 mass % to 1.0 mass %, Si: 0.1 mass % to 1.2 mass %, Fe: 0.10 mass % to 1.40 mass %, Ti: 0 mass % to 0.100 mass %, B: 0 mass % to 0.030 mass %, Cu: 0 mass % to 1.00 mass %, Ag: 0 mass % to 0.50 mass %, Au: 0 mass % to 0.50 mass %, Mn: 0 mass % to 1.00 mass %, Cr: 0 mass % to 1.00 mass %, Zr: 0 mass % to 0.50 mass %, Hf: 0 mass % to 0.50 mass %, V: 0 mass % to 0.50 mass %, Sc: 0 mass % to 0.50 mass %, Co: 0 mass % to 0.50 mass %, Ni: 0 mass % to 0.50 mass %, and the balance: Al and inevitable impurities, wherein a number of compound particles present on a surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is less than or equal to one per 100 μm.sup.2, and a tensile strength is greater than or equal to 200 MPa.

12. A method of manufacturing an aluminum alloy wire rod comprising: forming a drawing stock through hot working subsequent to melting and casting an aluminum alloy material having a composition comprising Mg: 0.1 mass % to 1.0 mass %, Si: 0.1 mass % to 1.2 mass %, Fe: 0.10 mass % to 1.40 mass %, Ti: 0 mass % to 0.100 mass %, B: 0 mass % to 0.030 mass %, Cu: 0 mass % to 1.00 mass %, Ag: 0 mass % to 0.50 mass %, Au: 0 mass % to 0.50 mass %, Mn: 0 mass % to 1.00 mass %, Cr: 0 mass % to 1.00 mass %, Zr: 0 mass % to 0.50 mass %, Hf: 0 mass % to 0.50 mass %, V: 0 mass % to 0.50 mass %, Sc: 0 mass % to 0.50 mass %, Co: 0 mass % to 0.50 mass %, Ni: 0 mass % to 0.50 mass %, and the balance: Al and inevitable impurities; and subsequently, performing steps including at least a wire drawing step, an solution heat treatment and an aging heat treatment, wherein the solution heat treatment includes heating to a predetermined temperature in range of 450° C. to 580° C., retaining at the predetermined temperature for a predetermined time, and thereafter cooling at an average cooling rate of greater than or equal to 10° C./s to at least a temperature of 150° C.; and the aging heat treatment is performed at a predetermined temperature in a range of 20° C. to 250° C.

13. The method of manufacturing an aluminum alloy wire rod according to claim 12, wherein an average cooling rate in a temperature range from 750° C. to 400° C. during casting is greater than or equal to 20° C./s, a re-heat treatment is performed after the casting and before the hot working, and the re-heat treatment includes a heating at a predetermined temperature of higher than or equal to 400° C., and retaining at the predetermined temperature for a time less than or equal to 10 minutes.

14. The aluminum alloy wire rod according to claim 2, wherein the composition comprises at least one of Cu: 0.01 mass % to 1.00 mass %, Ag: 0.01 mass % to 0.50 mass %, Au: 0.01 mass % to 0.50 mass %, Mn: 0.01 mass % to 1.00 mass %, Cr: 0.01 mass % to 1.00 mass %, Zr: 0.01 mass % to 0.50 mass %, Hf: 0.01 mass % to 0.50 mass %, V: 0.01 mass % to 0.50 mass %, Sc: 0.01 mass % to 0.50 mass %, Co: 0.01 mass % to 0.50 mass % and Ni: 0.01 mass % to 0.50 mass %.

15. The aluminum alloy wire rod according to claim 2, wherein a sum of contents of Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni is 0.10 mass % to 2.00 mass %.

16. The aluminum alloy wire rod according to claim 3, wherein a sum of contents of Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni is 0.10 mass % to 2.00 mass %.

17. The aluminum alloy wire rod according to claim 2, wherein the compound particles are Fe-based compound particles.

18. The aluminum alloy wire rod according to claim 3, wherein the compound particles are Fe-based compound particles.

19. The aluminum alloy wire rod according to claim 4, wherein the compound particles are Fe-based compound particles.

20. The aluminum alloy wire rod according to claim 2, wherein a thickness of a surface oxide layer is less than or equal to 500 nm.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0020] FIG. 1 is a surface SEM photograph of a surface of an aluminum alloy wire rod according to the present disclosure observed with a scanning electron microscope (SEM) at a magnification of 1500×.

[0021] FIG. 2 is a surface SEM photograph of a surface of a conventional aluminum alloy wire rod was observed with a scanning electron microscope (SEM) at a magnification of 1500×.

DETAILED DESCRIPTION

[0022] Then, the embodiments of the present disclosure will be described. Hereinafter, reasons for limiting the chemical compositions, the surface texture and the like of an aluminum alloy wire rod according to the present disclosure will be described.

[0023] (I) Chemical Composition

<Mg: 0.1 Mass % to 1.0 Mass %>

[0024] Mg (magnesium) has an effect of strengthening by forming a solid solution in an aluminum matrix, and a part of it has an effect of improving tensile strength by being precipitated as a β″-phase (beta double prime phase) or the like together with Si. In a case where it forms an Mg—Si cluster as a solute atom cluster, it is an element having an effect of improving a tensile strength and an elongation. However, in a case where Mg content is less than 0.10 mass %, the above effects are insufficient. In a case where Mg content is in excess of 1.00 mass %, there is an increased possibility of formation of an Mg-concentration part on a grain boundary, which may cause a decrease in tensile strength and elongation. In addition, due to an increased amount of Mg element forming the solid solution, the 0.2% yield strength is increased, and when a cable is formed by using a wire rod, the ease of routing and handling of an electric wire is decreased and the conductivity is also decreased. Accordingly, the Mg content is 0.1 mass % to 1.0 mass %. The Mg content is, when a high strength is of importance, preferably 0.5 mass % to 1.0 mass %, and when a conductivity is of importance, preferably greater than or equal to 0.1 mass % and less than 0.5 mass %. Based on the points described above, the content of Mg is generally preferably 0.30 mass % to 0.70 mass %.

<Si: 0.1 Mass % to 1.2 Mass %>

[0025] Si (silicon) has an effect of strengthening by forming a solid solution in an aluminum matrix, and a part of it has an effect of improving tensile strength and a bending fatigue resistance by being precipitated as a β″-phase (beta double prime phase) or the like together with Mg. Also, in a case where it forms an Mg—Si cluster or a Si—Si cluster as a solute atom cluster, it is an element having an effect of improving a tensile strength and an elongation. However, in a case where Si content is less than 0.1 mass %, the above effects are insufficient. In a case where Si content is in excess of 1.2 mass %, there is an increased possibility of formation of an Si-concentration part on a grain boundary, which may cause a decrease in tensile strength and elongation. Also, due to an increased amount of a solid solution of an Si element, the 0.2% yield strength is increased, the ease of routing and handling is decreased, and the conductivity is also decreased. Accordingly, the Si content is 0.1 mass % to 1.2 mass %. The Si content is, when high strength is of importance, preferably 0.5 mass % to 1.2 mass %, and in case where conductivity is of importance, preferably greater than or equal to 0.1 mass % and less than 0.5 mass %. Based on the points described above, the Si content is generally preferably 0.3 mass % to 0.7 mass %.

<Fe: 0.10 Mass % to 1.40 Mass %>

[0026] Fe (iron) is an element that contributes to refinement of crystal grains mainly by forming an Al—Fe based intermetallic compound and provides improved tensile strength. Fe dissolves in Al only by 0.05 mass % at 655° C., and even less at room temperature. Accordingly, the remaining Fe that cannot dissolve in Al will be crystallized or precipitated as an intermetallic compound such as Al—Fe, Al—Fe—Si, and Al—Fe—Si—Mg. The intermetallic compound mainly constituted with Fe and Al as exemplified by the above-described intermetallic compounds is referred to as the Fe-based compound in the present description. This intermetallic compound contributes to the refinement of crystal grains and provides improved tensile strength. Further, Fe has, also by Fe that has dissolved in Al, an effect of providing an improved tensile strength. In a case where Fe content is less than 0.10 mass %, those effects are insufficient. In a case where Fe content is in excess of 1.40 mass %, a wire drawing workability decreases due to coarsening of crystallized materials or precipitates, and also the 0.2% yield strength increases, thus the ease of routing and handling decreases and further the elongation is decreased. Therefore, the Fe content is 0.10 mass % to 1.40 mass %, and preferably 0.15 mass % to 0.70 mass %, and more preferably 0.15 mass % to 0.45 mass %.

[0027] The aluminum alloy wire rod of the present disclosure includes Mg, Si and Fe as essential components as described above, and may further contain any one of Ti and B, and at least one of Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni, as necessary.

<Ti: 0.001 Mass % to 0.100 Mass %>

[0028] Ti (titanium) is an element having an effect of refining the structure of an ingot during dissolution casting. In a case where an ingot has a coarse structure, the ingot may crack during casting or a wire break may occur during a wire rod processing step, which is industrially undesirable. In a case where the Ti content is less than 0.001 mass %, the aforementioned effect cannot be achieved sufficiently, and in a case where Ti content exceeds 0.100 mass %, the conductivity tends to decrease. Accordingly, the Ti content is 0.001 mass % to 0.100 mass %, preferably 0.005 mass % to 0.050 mass %, and more preferably 0.005 mass % to 0.030 mass %.

<B: 0.001 Mass % to 0.030 Mass %>

[0029] Similarly to Ti, B (boron) is an element having an effect of refining the structure of an ingot during dissolution casting. In a case where an ingot has a coarse structure, the ingot may crack during casting or a wire break is likely to occur during a wire rod processing step, which is industrially undesirable. In a case where the B content is less than 0.001 mass %, the aforementioned effect cannot be achieved sufficiently, and in a case where the B content exceeds 0.030 mass %, the conductivity tends to decrease. Accordingly, the B content is 0.001 mass % to 0.030 mass %, preferably 0.001 mass % to 0.020 mass %, and more preferably 0.001 mass % to 0.010 mass %.

[0030] To contain at least one of <Cu: 0.01 mass % to 1.00 mass %>, <Ag: 0.01 mass % to 0.50 mass %>, <Au: 0.01 mass % to 0.50 mass %>, <Mn: 0.01 mass % to 1.00 mass %>, <Cr: 0.01 mass % to 1.00 mass %> and <Zr: 0.01 mass % to 0.50 mass %>, <Hf: 0.01 mass % to 0.50 mass %>, <V: 0.01 mass % to 0.50 mass %>, <Sc: 0.01 mass % to 0.50 mass %>, <Co: 0.01 mass % to 0.50 mass %>, and <Ni: 0.01 mass % to 0.50 mass %>

[0031] Each of Cu (copper), Ag (silver), Au (gold), Mn (manganese), Cr (chromium), Zr (zirconium), Hf (hafnium), V (vanadium), Sc (scandium), Co (cobalt) and Ni (nickel) is an element having an effect of refining crystal grains and also having an effect of suppressing the production of abnormal coarse grown grains, and Cu, Ag and Au are elements further having an effect of increasing a grain boundary strength by being precipitated at a grain boundary. In a case where at least one of the elements described above is contained by 0.01 mass % or more, the aforementioned effects can be achieved, and a tensile strength and an elongation can be further improved. On the other hand, in a case where any one of Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni has a content exceeding the upper limit thereof mentioned above, a compound containing such elements coarsens and deteriorates wire drawing workability, a wire break is likely to occur and also a conductivity tends to decrease. Therefore, ranges of contents of Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni are the ranges described above, respectively. Among elements in this group of elements, it is particularly preferable to contain Ni. This is because when Ni is contained, a crystal grain refinement effect and an abnormal grain growth suppressant effect become significant, a tensile strength and elongation improve, and also, there is recognized an effect to suppress a decrease in conductivity and a wire break during wire drawing. From the viewpoint of satisfying such effects while ensuring a good balance between these effects, it is further preferable that the Ni content is 0.05 mass % to 0.30 mass %.

[0032] As for Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni, with the increase of the contents of these elements, the conductivity and the elongation tend to decrease, the wire drawing workability tends to be degraded, and the increase of the 0.2% yield strength tends to degrade the ease of routing and handling. Therefore, it is preferable that a sum of the contents of the elements is less than or equal to 2.00 mass %. Since in the aluminum alloy wire rod of the present disclosure, Fe is an essential element, the sum of the contents of Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni is preferably 0.10 mass % to 2.00 mass %. In a case where the above elements are added alone, the compound containing the element tends to coarsen more as the content increases. Since this may degrade wire drawing workability and a wire break is likely to occur, the content ranges of the respective elements are as specified above.

[0033] In order to moderately decrease the yield strength value, while maintaining a high conductivity, the sum of the contents of Fe, Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni is particularly preferably 0.10 mass % to 0.80 mass %, and further preferably 0.15 mass % to 0.60 mass %. On the other hand, although the conductivity is slightly decreased, in order to further appropriately decrease the tensile strength, the elongation and the yield strength value in relation to the tensile strength, the aforementioned content sum is particularly preferably greater than 0.80 mass % and less than or equal to 2.00 mass %, and further preferably 1.00 mass % to 2.00 mass %.

<Balance: Al and Inevitable Impurities>

[0034] The balance, i.e., components other than those described above, includes Al (aluminum) and inevitable impurities. Herein, inevitable impurities mean impurities contained by an amount which could be contained inevitably during the manufacturing process. Since inevitable impurities could cause a decrease in conductivity depending on a content thereof, it is preferable to suppress the content of the inevitable impurities to some extent considering the decrease in the conductivity. Components that may be inevitable impurities include, for example, Ga (gallium), Zn (zinc), Bi (bismuth), and Pb (lead).

[0035] (II) Surface Texture and Strength Characteristic of Aluminum Alloy Wire Rod

[0036] The present disclosure is based on the premise that the chemical composition is limited, and requires a number of compound particles present on a surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is less than or equal to one particle per 100 μm.sup.2, and a tensile strength is greater than or equal to 200 MPa.

[0037] The present inventors have carried out assiduous studies as to whether or not the particle size and the presence ratio of the compound present on the surface of the wire rod are correlated with generation of pinholes on a surface of a plated film when forming a plated film on the surface of the wire rod.

[0038] Consequently, it has been found that when a number of compound particles having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter present on the surface of the wire rod is greater than one per 100 μm.sup.2, defects such as pinholes or asperities tend to occur after plating, and accelerate the decrease of a corrosion resistance, degradation of an exterior appearance, and a decrease in a use-life due to the concentration of stress. Herein, “a diameter in terms of equivalent circle diameter” means a diameter of a perfect circle having the same area as the actual area of a target compound particle.

[0039] FIG. 1 shows a typical exemplary surface SEM photograph obtained when a surface of an aluminum alloy wire rod (product of the present disclosure) of an embodiment according to the present disclosure was observed by using a scanning electron microscope (SEM) at a magnification of 1500×, and FIG. 2 is a surface SEM photograph obtained when a surface of a conventional aluminum alloy wire rod (conventional product) was observed under the same conditions as in FIG. 1. As can be seen from FIG. 1 and FIG. 2, the number of the compound particles having a diameter of greater than or equal to 1 μm present on the surface of the aluminum alloy wire rod is extremely small as compared to the conventional product.

[0040] As the compound particles present on the surface of an aluminum alloy wire rod, various compounds are possible, and examples of such compounds include mainly a Fe-based compound, and for example, an Al—Fe-based compound, an Al—Fe—Si-based compound, an Al—Fe—Si—Mg-based compound and an Al—Fe—Mn—Si-based compound.

[0041] The tensile strength of an aluminum alloy wire rod is required to be greater than or equal to 200 MPa. This is because when the tensile strength of an aluminum alloy wire rod is less than 200 MPa, when disposed as a wire harness in a transportation vehicle, such as an automobile, at a portion where a large tensile force is acting, a wire break might occur, and thus a usage portion will be limited. Accordingly, the tensile strength of the aluminum alloy wire rod was 200 MPa.

[0042] Further, the thickness of the surface oxide layer of the wire rod surface is preferably less than or equal to 500 nm. This is because when the thickness is greater than 500 nm, a pretreatment step of plating for removing an oxide film requires a long time, and productivity might largely decrease.

[0043] According to the aluminum alloy wire rod of the present disclosure, in a case where a plated film is formed on a surface of the wire rod, the number of pinholes present on a surface of the plated film surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter can be made to be less than or equal to one pinhole/mm.sup.2, and it is also possible to suppress the decrease in corrosion resistance, the degradation of an exterior appearance and a decrease in a use-life due to the concentration of stress.

[0044] Such an aluminum alloy wire rod can be obtained by combining and controlling the alloy composition and the manufacturing process. Hereinafter, a description is made of a preferred method of manufacturing an aluminum alloy wire rod of the present disclosure.

[0045] (Method of Manufacturing an Aluminum Alloy Wire Rod According to an Example of the Present Disclosure)

[0046] The aluminum alloy wire rod according to an Example of the present disclosure can be manufactured by a manufacturing method including forming a drawing stock through hot working subsequent to melting and casting an aluminum alloy material having a composition consisting of or comprising Mg: 0.1 mass % to 1.0 mass %, Si: 0.1 mass % to 1.2 mass %, Fe: 0.10 mass % to 1.40 mass %, Ti: 0 mass % to 0.100 mass %, B: 0 mass % to 0.030 mass %, Cu: 0 mass % to 1.00 mass %, Ag: 0 mass % to 0.50 mass %, Au: 0 mass % to 0.50 mass %, Mn: 0 mass % to 1.00 mass %, Cr: 0 mass % to 1.00 mass %, Zr: 0 mass % to 0.50 mass %, Hf: 0 mass % to 0.50 mass %, V: 0 mass % to 0.50 mass %, Sc: 0 mass % to 0.50 mass %, Co: 0 mass % to 0.50 mass %, Ni: 0 mass % to 0.50 mass %, and the balance: Al and inevitable impurities; the manufacturing method being based on the premise that subsequently, steps including at least a wire drawing step, a solution heat treatment step and an aging heat treatment step are performed; wherein the solution heat treatment is performed by heating to a predetermined temperature in a range of 450° C. to 580° C., holding for a predetermined time, and subsequently cooling at an average cooling rate of greater than or equal to 10° C./s at least to a temperature of 150° C.; and the aging heat treatment is performed by heating to a predetermined temperature in a range of 20° C. to 250° C.

[0047] Specific examples of the method of manufacturing an aluminum alloy wire rod of the present disclosure include a manufacturing method including sequentially performing each step of [1] melting, [2] casting, [3] hot working (such as grooved roll working), [4] first wire drawing, [5] first heat treatment (intermediate heat treatment), [6] second wire drawing, [7] second heat treatment (solution heat treatment), and [8] third heat treatment (aging heat treatment). It is to be noted that a stranding step or a wire resin-covering step may be provided before or after the second heat treatment or after the aging heat treatment. Hereinafter, steps of [1] to [8] will be described.

[0048] [1] Melting Step

[0049] In the melting, a material is prepared by adjusting quantities of each component such that the aforementioned aluminum alloy composition is obtained, and the material is melted.

[0050] [2] Casting and [3] Hot Working (Such as Grooved Roll Working)

[0051] Subsequently, in the casting step, it is required to increase the cooling rate to reduce and refine crystallization of the compound particles, in particular Fe-based compound particles. From this viewpoint, in the present disclosure, the cooling rate, during casting, in a temperature range from 750° C. to 400° C., is greater than or equal to 20° C./s, additionally a re-heat treatment is performed after the casting and before the hot working, and in the re-heat treatment, heating is performed at a predetermined temperature higher than or equal to 400° C., and a period of time in which the temperature is retained at the predetermined temperature is preferably less than or equal to 10 minutes. Herein, the cooling rate in a temperature range from 750° C. to 400° C. is greater than or equal to 20° C./s in order that the period of time in which the temperature is retained in the Fe crystallization temperature region and the Fe-based compound precipitation temperature region be reduced and the production of the Fe-based compound be suppressed. Also, in the re-heat treatment performed after casting and before hot working, the period of time in which the temperature is retained at the predetermined temperature higher than or equal to 400° C. is less than or equal to 10 minutes, firstly in order that the production of the Fe-based compound be suppressed by reducing the period of time in which the temperature is retained in the precipitation temperature region of the Fe-based compound, and secondly, because a thickness of a surface oxide layer composed of an Al oxide or a Mg oxide can be made to be less than or equal to 500 nm.

[0052] It is to be noted that a method of setting an average cooling rate in the temperature range from 750° C. to 400° C. during casting to be greater than or equal to 20° C./s is not particularly limited, but examples of such a method include: a method using a Properzi-type continuous casting rolling mill which is an assembly of a casting wheel and a belt, and a so-called an in-water spinning method, namely, a method in which a molten metal flow is jetted approximately in parallel at the same velocity from an inner side of a rotating drum containing water, and the molten metal is cooled and solidified in the water. In a method using a continuous casting rolling mill, a bar of a diameter of 5 mm to 13 mm can be obtained at an average cooling rate of greater than or equal to 20° C./sec, and by using the in-water spinning method, a bar having a diameter of 1 mm to 13 mm can be obtained at an average cooling rate of greater than or equal to 30° C./sec. Casting and hot rolling may be performed by billet casting and an extrusion technique.

[0053] [4] First Wire Drawing

[0054] Subsequently, the surface is stripped, if necessary and the bar is made into an appropriate size of, for example, 5 mmφ to 12.5 mmφ, and wire drawing is performed by cold rolling. A reduction ratio η is preferably within a range of 1 to 6. Herein, the reduction ratio η is represented by η=ln(A.sub.0/A.sub.1), where A.sub.0 is a wire rod cross sectional area before wire drawing and A.sub.1 is a wire rod cross sectional area after wire drawing. In a case where the reduction ratio η is less than 1, in a heat treatment of a subsequent step, recrystallized grains coarsen and a tensile strength and an elongation significantly decrease, which may cause a wire break. In a case where the reduction ratio η is greater than 6, the wire drawing becomes difficult and may be problematic from a quality point of view since a wire break might occur during a wire drawing process. The stripping of the surface has an effect of cleaning the surface, but does not need to be performed.

[0055] [5] First Heat Treatment (Intermediate Heat Treatment)

[0056] Then, a first heat treatment is applied to the work piece that has been subjected to cold drawing. The first heat treatment of the present disclosure is performed for regaining the flexibility of the work piece and for improving the wire drawing workability. It is not necessary to perform the first heat treatment if the wire drawing workability is sufficient and a wire break will not occur. In order to prevent the coarsening of the intermetallic compound and to suppress the growth of the surface oxide layer, the first heat treatment is preferably performed at 400° C. or lower, and the period of time of being exposed to a temperature higher than 400° C. is preferably less than 10 minutes.

[0057] [6] Second Wire Drawing

[0058] After the first heat treatment, wire drawing is further carried out in a cold processing. During this drawing, a reduction ratio η is preferably within a range of 1 to 6. The reduction ratio η has an influence on formation and growth of recrystallized grains. This is because, if the reduction ratio η is less than 1, during the heat treatment in a subsequent step, there is a tendency such that coarsening of recrystallized grains occur and the tensile strength and the elongation drastically decrease, and if the reduction ratio η is greater than 6, wire drawing becomes difficult and there is a tendency such that problems arise in quality, such as a wire break during wire drawing. It is to be noted that in a case where the first heat treatment is not performed, the first wire drawing and the second wire drawing may be performed in series.

[0059] [7] Second Heat Treatment (Solution Heat Treatment)

[0060] The second heat treatment is performed on the work piece that has been subjected to wire drawing. The second heat treatment of the present disclosure is a solution heat treatment for dissolving randomly contained compounds of Mg and Si into an aluminum matrix. With the solution treatment, it is possible to even out the Mg and Si concentration parts during a working (it homogenizes) and leads to a suppression in the segregation of a Mg compound and a Si compound at grain boundaries after the final aging heat treatment. The second heat treatment is specifically a heat treatment including heating to a predetermined temperature in a range of 450° C. to 580° C., retaining at the predetermined temperature for a predetermined time, and thereafter cooling at an average cooling rate of greater than or equal to 10° C./s to at least a temperature of 150° C. When a predetermined temperature during the second heat treatment is higher than 580° C., the crystal grain size is coarsened and abnormally grown grains are produced, and in a case where the predetermined temperature is lower than 450° C., Mg.sub.2Si cannot be sufficiently solid dissolved. Therefore, the predetermined temperature during the heating in the second heat treatment is in a range of 450° C. to 580° C., and although the predetermined temperature may vary depending on the contents of Mg and Si, the predetermined temperature is preferably in a range of 450° C. to 540° C., and more preferably in a range of 480° C. to 520° C. The sum of the periods of time for retaining the wire rod at 400° C. or higher in the re-heat treatment and the first heat treatment (the intermediate heat treatment) after casting is preferably set to fall within a range of less than or equal to 10 minutes. When the average cooling rate at least to a temperature of 150° C. is slower than 10° C./s, Mg and Si are once solid-dissolved in the aluminum matrix and tend to be easily precipitated again as a compound of Mg and Si. Accordingly, in the present disclosure, the solution heat treatment is performed by heating to a predetermined temperature within a range of 450° C. to 580° C., retaining at the predetermined temperature for a predetermined time, and thereafter cooling at an average cooling rate of greater than or equal to 10° C./s at least to the temperature of 150° C.

[0061] A method of performing the second heat treatment may be, for example, batch heat treatment, salt bath, or may be continuous heat treatment such as high-frequency heating, conduction heating, and running heating.

[0062] In a case where high-frequency heating and conduction heating are used, the wire rod temperature increases with a passage of time, since it normally has a structure in which an electric current continues to flow through the wire rod. Accordingly, since the wire rod may melt when an electric current continues to flow through, it is necessary to perform heat treatment for an appropriate time range. In a case where running heating is used, since it is an annealing in a short time, the temperature of a running annealing furnace is usually set higher than a wire rod temperature. Since the wire rod may melt with a heat treatment over a long time, it is necessary to perform heat treatment in an appropriate time range. The heating retention times in all the heat treatments are each required to be longer than or equal to a predetermined time in order to dissolve compounds of Mg and Si randomly contained in a work piece into an aluminum matrix. Hereinafter, the heat treatment by each method will be described.

[0063] The continuous heat treatment by high-frequency heating is a heat treatment by joule heat generated from the wire rod itself by an induced current by the wire rod continuously passing through a magnetic field caused by a high frequency. Steps of rapid heating and quenching are included, and the wire rod can be heat-treated by controlling the wire rod temperature and the heat treatment time. The cooling is performed after rapid heating by continuously allowing the wire rod to pass through water or in a nitrogen gas atmosphere. The heating treatment time is 0.01 s to 2 s, preferably 0.05 s to 1 s, and more preferably 0.05 s to 0.5 s.

[0064] The continuous conducting heat treatment is a heat treatment by joule heat generated from the wire rod itself by allowing an electric current to flow in the wire rod that continuously passes two electrode wheels. Steps of rapid heating and quenching are included, and the wire rod can be heat-treated by controlling the wire rod temperature and the heat treatment time. The cooling is performed after rapid heating by continuously allowing the wire rod to pass through water, atmosphere or a nitrogen gas atmosphere. The heating treatment time is 0.01 s to 2 s, preferably 0.05 s to 1 s, and more preferably 0.05 s to 0.5 s.

[0065] A continuous running heat treatment is a heat treatment in which the wire rod continuously passes through a heat treatment furnace retained at a high-temperature. Steps of rapid heating and quenching are included, and the wire rod can be heat-treated by controlling the temperature in the heat treatment furnace and the heat treatment time. The cooling is performed after rapid heating by continuously allowing the wire rod to pass through water, atmosphere or a nitrogen gas atmosphere. The heating treatment time is preferably 0.5 s to 30 s.

[0066] In a case where at least one of the wire rod temperature or the heat treatment time is lower than the condition defined above, the solution heat treatment will be incomplete, and solute atom clusters, a β″phase and a Mg.sub.2Si precipitate produced during the aging heat treatment, which is a post-process, are reduced, and the improvement magnitudes of the tensile strength, the shock resistance, the bending fatigue resistance and the conductivity are decreased. In a case where at least one of the wire rod temperature or the annealing time is higher than the condition specified above, the crystal grains coarsen and a partial fusion (eutectic fusion) of a compound phase of an aluminum alloy wire rod occurs, and the tensile strength and the elongation decrease, and a wire break is likely to occur during the handling of the conductor.

[0067] [8] Third Heat Treatment (Aging Heat Treatment)

[0068] Subsequently, a third heat treatment is applied. The third heat treatment is an aging heat treatment performed for producing Mg and Si compounds and solute atom clusters. In the present disclosure, the heating temperature of the aging heat treatment is 20° C. to 250° C. In a case where the heating temperature in the aging heating treatment is lower than 20° C., the production of the solute atom clusters is slow and requires time to obtain necessary tensile strength and elongation, and thus it is disadvantageous for mass-production. In a case where the heating temperature is higher than 250° C., in addition to the Mg.sub.2Si needle-like precipitate (β″ phase) most contributing to the strength, coarse Mg.sub.2Si precipitates are produced to decrease the strength. Accordingly, in the present disclosure, the heating temperature of the aging heat treatment is 20° C. to 250° C. In a case where it is necessary to produce solute atom clusters that are more effective in improving the elongation, the heating temperature in the aging heat treatment is preferably 20° C. to 70° C., and in a case where the β″ phase is simultaneously precipitated, and the balance between the tensile strength and the elongation is required to be achieved, the heating temperature in the aging heat treatment is preferably 100° C. to 150° C.

[0069] Moreover, as for the heating retention time in the aging heat treatment, the optimal time is varied depending on the temperature. Moreover, for the purpose of improving the tensile strength and the elongation, and reducing the 0.2% yield strength in relation to the tensile strength, the heating time is preferably long when the temperature is low and the heating time is preferably short when the temperature is high. For example, a long heating time is ten days or less, and, a short heating time is, preferably, 15 hours or less, and more preferably, 8 hours or less. It is to be noted that, in order to prevent dispersion of the properties, it is preferable to increase the cooling rate as much as possible in the cooling in the aging heat treatment. Of course, even in a case where cooling cannot be performed quickly due to the manufacturing process, the cooling rate can be appropriately set if the cooling time is an aging condition with which solute atom clusters are produced sufficiently.

[0070] A strand diameter of the aluminum alloy wire rod of the present embodiment is not particularly limited and can be determined appropriately according to the purpose of use, and is preferably 0.1 mm to 0.5 mmφ for a fine wire, and 0.8 mm to 1.5 mmφ for a middle sized wire. The aluminum alloy wire rod of the present embodiment is advantageous in that the aluminum alloy wire can be used as a thin single wire as an aluminum alloy wire, but may also be used as an aluminum alloy stranded wire obtained by stranding a plurality of them together, and among the aforementioned steps [1] to [8] of the manufacturing method of the present disclosure, after bundling and stranding a plurality of aluminum alloy wire rods obtained by sequentially performing the respective steps [1] to [6], the steps of [7] the second heat treatment (the solution heat treatment) and [8] the third heat treatment (the aging heat treatment) may also be performed.

[0071] Also, in the present embodiment, such a homogenizing heat treatment as performed in the prior art may be further performed as an additional step after continuous casting rolling. Since the homogenizing heat treatment can uniformly disperse the added elements, a crystallized material, a solute atom cluster and the β″ precipitation phase are easily produced uniformly in the subsequent third heat treatment, and the improvement of the tensile strength, the improvement of the elongation, and the improvement of the yield strength in relation to the tensile strength are obtained more stably. The homogenizing heat treatment is performed at a heating temperature of preferably 450° C. to 600° C. and more preferably 500° C. to 600° C. Also, the cooling in the homogenizing heat treatment is preferably a slow cooling at an average cooling rate of 0.1° C./min to 10° C./min because of the easiness in obtaining a uniform compound.

[0072] Also, the aluminum alloy wire rod of the present embodiment can be used as an aluminum alloy wire, or as an aluminum alloy stranded wire obtained by stranding a plurality of aluminum alloy wires, and may also be used as a covered wire having a covering layer at an outer periphery of the aluminum alloy wire or the aluminum alloy stranded wire, and, in addition, the aluminum alloy wire rod can also be used as a wire harness having a covered wire and a terminal fitted at an end portion of the covered wire, the covering layer being removed from the end portion.

EXAMPLES

[0073] The present disclosure will be described in detail on the basis of the following examples. It is to be noted that the present disclosure is not limited to the examples described below.

Examples and Comparative Examples

[0074] Mg, Si, Fe, and Al, and selectively added Ti, B, Cu, Ag, Au, Mn, Cr, Zr, Hf, V, Sc, Co and Ni were placed in a Properzi-type continuous casting rolling mill such that the contents (mass %) were as shown in Table 1, and a molten metal containing these raw materials was continuously rolled while being cast with a water-cooled mold in the Properzi-type continuous casting rolling mill under the conditions shown in Table 2, and thus a bar of φ9 mm was obtained. Then, the first wire drawing was applied to the bar so as to obtain a predetermined reduction ratio. Then, the first heat treatment (the intermediate heat treatment) was applied to a work piece subjected to the first wire drawing under the conditions shown in Table 2, and thereafter, further a second wire drawing was applied to the work piece subjected to the first heat treatment until a wire size of φ0.3 mm was achieved so as to obtain a predetermined reduction ratio. Then, the second heat treatment (the solution heat treatment) was applied under the conditions shown in Table 2. Both in the first heat treatment and in the second heat treatment, in a case of a batch heat treatment, the wire rod temperature was measured with a thermocouple wound around the wire rod. In the continuous conducting heat treatment, since the measurement at a part where the temperature of the wire rod was the highest was difficult due to equipment, the temperature was measured with a fiber optic radiation thermometer (manufactured by Japan Sensor Corporation) at a position upstream of a portion where the temperature of the wire rod was highest, and the maximum temperature was calculated in consideration of joule heat and heat dissipation. In each of the high-frequency heating and the consecutive running heat treatment, the wire rod temperature in the vicinity of the heat treatment section outlet was measured. After the second heat treatment, the third heat treatment (the aging heat treatment) was applied under the conditions shown in Table 1, and aluminum alloy wires were produced.

[0075] For each of the produced aluminum alloy wires of Examples and Comparative Examples, the respective characteristics were measured by the methods shown below. The results thus obtained are shown in Table 3. Physical properties were also measured when various platings were further applied to the surface of the respective produced aluminum alloy wires, and the results thus obtained are also shown in Table 3.

[0076] [Evaluation Methods]

[0077] (A) Measurements of Particle Sizes and Presence Ratio of Compound Particles Present on Wire Rod Surface

[0078] By using a scanning electron microscope (SEM), the particle size and the presence ratio of the compound particles present on the wire rod surface, specifically, the presence ratio of the particles present on the wire rod surface and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is measured by the following technique. A first spot is a region of 1000 μm.sup.2 observed at an arbitrary position on a surface of the wire rod. A second spot is a region of 1000 μm.sup.2 observed at a position on the surface of the wire rod spaced apart from the first spot by 1000 mm or more in a lengthwise direction of the wire rod. A third spot is a region of 1000 μm.sup.2 observed at a position on the surface of the wire rod spaced apart from the first spot by 2000 mm or more in the lengthwise direction of the wire rod and spaced apart from the second spot by 1000 mm or more in the lengthwise direction of the wire rod, and, the presence ratio (particle(s)/100 μm.sup.2) of the compound particles present on the surface of the wire rod and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is calculated. It is to be noted that the aforementioned diameter was obtained by binarizing an obtained SEM image and obtaining an area of a compound particle, and by converting the same area into an equivalent circle diameter.

[0079] (B) Measurement of Thickness of Surface Oxide Layer of Wire Rod

[0080] A thickness of the surface oxide layer of the wire rod is measured by using an Auger electron spectrometer. An average value calculated from the measurement values at three spots in total is taken as a thickness of the surface oxide layer of the wire rod. The measurements are performed by spacing apart the first spot and the second spot by 1000 mm or more in the lengthwise direction of the wire rod, spacing apart the first spot and the third spot by 2000 mm or more in the lengthwise direction of the wire rod, and spacing apart the second spot and the third spot by 1000 mm or more in the lengthwise direction of the wire rod.

[0081] (C) Measurements of Tensile Strength and Elongation after Fracture

[0082] In conformity with JIS Z 2241: 2011, a tensile test was carried out for each of three materials under test (aluminum alloy wires), and the average values of the tensile strength and the elongation after fracture were obtained. The tensile strength of greater than or equal to 200 MPa was regarded as a pass level so as to keep the tensile strength of a crimp portion at a connection portion between an electric wire and a terminal and to withstand a load abruptly applied during an installation work to a car body.

[0083] (D) Conductivity

[0084] In a constant temperature bath in which a test piece of 300 mm in length is held at 20° C. (±0.5° C.), a resistivity was measured for three materials under test (aluminum alloy wires) each time using a four terminal method, and an average conductivity was calculated. The distance between the terminals was 200 mm. The conductivity of greater than or equal to 45% IACS was regarded as an acceptable level.

[0085] (E) Measurement of Presence Ratio of Pinholes Present on Surface after Plating

[0086] By using a scanning electron microscope (SEM), the diameter and the presence ratio of the pinholes present on the surface of the wire rod, specifically the presence ratio of the pinholes present on the surface of the wire rod and having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter are measured by the following technique. A first spot is a region of 1000 μm.sup.2 observed at an arbitrary position on the surface of the wire rod. A second spot is a region of 1000 μm.sup.2 observed at a position spaced apart from the first spot by 1000 mm or more in the lengthwise direction of the wire rod. A third spot is a region of 1000 μm.sup.2 observed at a position of the wire rod spaced apart from the first spot by 2000 mm or more in the lengthwise direction of the wire rod and spaced apart the second spot by 1000 mm or more in the lengthwise direction of the wire rod, and a presence ratio (pinhole(s)/100 μm.sup.2) of the pinholes present on the surface of the wire rod and each having a diameter of greater than or equal to 1 μm in terms of equivalent circle diameter is calculated.

[0087] (F) Evaluation of Platability

[0088] The neutral salt spray test described in JIS Z 2371: 2015 was performed for 96 hours, and the results were classified into two grades on the basis of an exterior appearance after the test. A case where substantially no degradation was found was marked with “◯” and the case where degradation was found was marked with “X”.

[0089] (G) Comprehensive Evaluation

[0090] The comprehensive evaluations shown in Table 3 are indicated by four grades “A” to “D,” according to the standards shown in Table 4 presented below, and “A,” “B” and “C” were each regarded as a pass level, and “D” was regarded as rejectable.

TABLE-US-00001 TABLE 1 Chemical Composition (mass %) No. Mg Si Fe Ti B Cu Ag Au Mn Cr Zr Hf V Sc Co Ni Al Example 1 0.4 0.7 0.10 0.01 0.005 — — — 0.05 — — — — — — — Balance 2 0.4 0.7 0.10 0.01 0.005 — — — — — 0.05 — — — — — 3 0.4 0.7 0.20 0.01 0.005 — — — — — — — — — — 0.05 4 0.4 0.7 0.20 0.01 0.005 — — — 0.05 — — — — — — — 5 0.4 0.7 0.30 0.01 0.005 — — — 0.05 — — — — — — — 6 0.4 0.7 0.30 0.01 0.005 — — — 0.10 0.10 — — — 0.10 0.05 — Comparative 1 0.4 0.7 0.01 0.005 — — — 0.05 — — — — — — — Balance Example 2 0.4 0.7 0.01 0.005 — — — — 0.05 — — — — — — 3 0.4 0.7 0.20 0.01 0.005 0.05 — — — — — — — — — — 4 0.4 0.7 0.10 0.01 0.005 — — — — — 0.05 — — — — — 5 0.4 0.7 0.10 0.01 0.005 — — — — — 0.05 — — — — — N.B. Numerical values in bold italic in the table are out of appropriate range of the present invention.

TABLE-US-00002 TABLE 2 Solution heat treatment conditions Casting conditions Average Average cooling rate cooling rate Re-heat at least to a Aging heat from 750° C. treatment conditions temperature treatment conditions to 400 C° Temp. Temp. Retention of 150° C. Temp. Retention No. (° C./s) (° C.) Time (s) (° C.) time (s) (° C./s) (° C.) time (h) Example 1 25 550 10 500 30 15 150 5 2 25 550 10 500 60 17 150 5 3 25 550 10 500 120 15 150 5 4 25 550 5 540 10 20 150 5 5 25 550 10 540 60 21 150 5 6 25 550 10 540 120 22 150 5 Comparative 1 25 550 10 500 30 19 150 5 Example 2 25 550 10 540 10 18 150 5 3 25 550 3600 540 3600 18 150 5 4 25 550 10 60 20 150 5 5 25 550 10 500 60 21 5 N.B. Numerical values in bold italic in the table are out of appropriate range of the present invention.

TABLE-US-00003 TABLE 3 Al alloy wire rod Presence ratio of compound Plated Al Alloy wire rod particles Characteristics greater than or Presence equal to 1 μm ratio of present on Thickness Characteristics pinholes on surface of surface Tensile Elongation plating Evaluation (particle(s)/ oxide strength after fracture Conductivity surface of No. 100 μm.sup.2) layer (nm) (MPa) (%) (% IACS) Type of plating (pinhole(s)/mm.sup.2) platability Evaluation Example 1 1 50 250 15 49.5 Zn plating 0 ◯ B 2 0 30 255 16 49.5 Zn plating 0 ◯ A 3 0 30 255 15 49.5 Zn plating 0 ◯ A 4 0 20 260 15 49.5 Electroless Ni—P 0 ◯ A plating 5 0 30 260 16 49.5 Electroless Ni—P 0 ◯ A plating 6 1 20 280 12 43.0 Electroless Ni—P 1 ◯ C plating Comparative 1 20 270 52.0 Zn plating X Example 2 1 30 16 48.0 Electroless Ni—P 0 ◯ plating 3 600 250 14 49.0 Electroless Ni—P X plating 4 0 550 19 49.5 Zn plating 0 ◯ 5 0 30 12 49.5 Zn plating 0 ◯ N.B. Numerical values in bold italic in the table are out of appropriate range of the present invention or characteristics are of rejectable level.

TABLE-US-00004 TABLE 4 Al Alloy wire rod Plated Al Alloy wire rod Characteristics Characteristics Elongation Presence proportion Tensile after of pinholes on Evaluation Comprehensive strength fracture Conductivity plating surface of evaluation (MPs) (%) (% IACS) (pinhole(s)/mm.sup.2) platability A 250 or more 10 or more 45 or more 0 ○ B 250 or more 10 or more 45 or more 1 or less ○ C 200 or more 5 or more 40 or more 1 or less ○ D Of the above-described characteristics, at least one characteristic does not satisfy the pass evaluation standard C

[0091] From the results shown in Table 3, the following are elucidated. Each of the aluminum alloy wires of Examples 1 to 6 had a tensile strength, an elongation after fracture and a conductivity, all being at pass level, is excellent in platability, and had a comprehensive evaluation was a pass level. In contrast, in each of the aluminum alloy wires of Comparative Examples 1 and 3, the presence ratio of the compound particles present on the wire rod surface and having a particle size of greater than or equal to 1 μm is out of the scope of the present disclosure. Accordingly, the presence ratio of the pinholes generated on the plated film surface in a case where a subsequent plating was performed increased, thus the platability was poor, and the comprehensive evaluation was “rejectable”. In Comparative Example 2, the Fe content in the wire rod was too small. Consequently, the tensile strength was insufficient, and the comprehensive evaluation was “rejectable”. Moreover, in each of Comparative Example 4 in which the heating temperature of the solution heat treatment was higher than the scope of the present disclosure, and Comparative Example 5 in which the heating temperature of the aging heat treatment was higher than the scope of the present disclosure, the tensile strength was insufficient and the comprehensive evaluation was “rejectable”.

[0092] The aluminum alloy wire rod of the present disclosure is capable of having sufficient mechanical characteristics even when used in a small-diameter wire having a strand diameter of less than or equal to 0.5 mm, and is accordingly useful as a battery cable, a wire harness or a conducting wire for a motor, equipped on a transportation vehicle, and as a wiring structure of an industrial robot.