Aluminum alloy and fastener member

Abstract

An aluminum alloy contains 0.7% to 1.8% of silicon, 0.5% to 2.1% of copper, 0.4% to 1.8% of manganese, 0.6% to 1.6% of magnesium, and 0.1% to 0.7% of zinc in terms of mass ratio and the balance aluminum with inevitable impurities.

Claims

1. A fastening member fastening a plurality of members together, wherein the fastening member is made of an aluminum alloy comprising, in terms of mass ratio: 0.7% to 1.8% of silicon; 1.5% to 2.1% of copper; 0.4% to 1.8% of manganese; 0.6% to 1.6% of magnesium; 0.1% to 0.7% of zinc 0.16% to 0.3% of titanium; and the balance aluminum with inevitable impurities, and wherein the fastening member has a tensile strength of 496 MPa or higher.

2. The fastening member according to claim 1, wherein the manganese is contained in an amount of 1.2% to 1.8% in terms of mass ratio.

3. The fastening member according to claim 1, wherein the silicon is contained in an amount of 1.4% to 1.8% in terms of mass ratio, and the magnesium is contained in an amount of 1.2% to 1.6% in terms of mass ratio.

4. The fastening member according to claim 1, comprising, in terms of mass ratio: 1.4% to 1.8% of the silicon; 1.5% to 2.1% of the copper; 1.2% to 1.8% of the manganese; 1.2% to 1.6% of the magnesium; 0.1% to 0.7% of the zinc; and 0.16% to 0.19% of the titanium.

5. The fastening member according to claim 1, further comprising at least one selected from the group consisting of, in terms of mass ratio: 0.05% to 0.15% of nickel; 0.05% to 0.15% of cobalt.

Description

BRIEF DESCRIPTION OF DRAWINGS

(1) FIG. 1 is a side view of a structure of a fastening member according to a first embodiment of the present invention.

(2) FIG. 2 is a plan view of a structure of a fastening member according to a second embodiment of the present invention.

(3) FIG. 3 is a side view of a structure of a fastening member according to a third embodiment of the present invention.

DESCRIPTION OF EMBODIMENTS

(4) The following describes modes for performing the present invention (hereinafter, referred to as “embodiments”) with reference to the accompanying drawings. The drawings are schematic, and the relation between the thickness and width of each part, the ratios in thickness of individual parts, and the like may be different from actual ones. Also between the drawings, some parts the mutual dimensional relation or ratio of which are different may be included.

First Embodiment

(5) FIG. 1 is a side view of a structure of a fastening member according to a first embodiment of the present invention. This fastening member 1 illustrated in FIG. 1 is a bolt (a kind of a male screw) made of an aluminum (Al) alloy. The fastening member 1 includes a cylindrical shaft 2, a head 3 provided on one end in an axial direction of the shaft 2 (the right-and-left direction in FIG. 1), and a neck 4 forming a boundary between the shaft 2 and the head 3. The shaft 2 has a screw part 22 formed with a screw thread 21 on its surface. The shape (a hexagonal trim shape) of the head 3 is only by way of example and may have other shapes (a hexagonal flange shape, a pan shape, a dish shape, a truss shape, a flat shape, and the like).

(6) The fastening member 1 is made of an aluminum alloy containing silicon (Si), copper (Cu), manganese (Mn), magnesium (Mg), zinc (Zn), and the balance aluminum (Al) with inevitable impurities. Specifically, the aluminum alloy according to the present embodiment contains 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, and 0.1% to 0.7% of Zn in terms of mass ratio. The aluminum alloy according to the present embodiment may contain at least one element selected from the group consisting of 0.05% to 0.15% of nickel (Ni), 0.05% to 0.15% of cobalt (Co), and 0.05% to 0.3% of titanium (Ti). In the following description, a content indicates a containing ratio in terms of mass ratio.

(7) Mg.sub.2Si is precipitated from Si by aging treatment and strength can be increased by the precipitation of Mg.sub.2Si. In particular, when a Mg content is 1.2% to 1.6%, and a Si content is 1.4% to 1.8%, the amount of a Mg.sub.2Si precipitate can be further increased, and strength can be further increased, which is thus preferable. Meanwhile, when the Si content exceeds 1.8%, the elongation of the alloy is decreased. When the Si content is less than 0.7%, the strength increasing effect by the Mg.sub.2Si precipitate is insufficient.

(8) CuAl.sub.2 and/or Al.sub.2CuMg are precipitated from Cu by aging treatment and strength can be increased by the precipitates. In particular, when a Cu content is 1.5% to 2.1%, the amount of these precipitates can be further increased, and strength can be further increased. Meanwhile, when the Cu content exceeds 2.1%, the corrosion resistance, stress corrosion cracking resistance, and elongation of the alloy are decreased. When the Cu content is less than 0.5%, the strength increasing effect by these precipitates is insufficient.

(9) Mn is an element that exhibits solid solution strengthening and produces Al—Mn—Si-based precipitates by aging treatment, and strength can be increased. In particular, when a Mn content is 1.2% to 1.8%, the amount of these precipitates can be further increased, and strength can be further increased. Meanwhile, when the Mn content exceeds 1.8%, the elongation of the alloy is decreased. When the Mn content is less than 0.4%, the strength increasing effect by these precipitates is insufficient.

(10) Mg.sub.2Si is precipitated from Mg by aging treatment and strength can be increased. In particular, when the Si content is 1.4% to 1.8%, and the Mg content is 1.2% to 1.6%, the amount of the Mg.sub.2Si precipitate can be further increased, and strength can be further increased. Meanwhile, when the Mg content exceeds 1.6%, elongation is decreased. When the Mg content is less than 0.6%, the strength increasing effect by the Mg.sub.2Si precipitate is insufficient.

(11) MgZn.sub.2 is precipitated from Zn by aging treatment and strength can be increased. When a Zn content exceeds 0.7%, the corrosion resistance, stress corrosion cracking resistance, and elongation of the alloy are decreased. When the Zn content is less than 0.1%, the strength increasing effect by these precipitates is insufficient.

(12) Ni is an element that forms precipitates with Al, Fe, Cu, and the like to improve heat resistance and can be added as needed. When a Ni content exceeds 0.15%, corrosion resistance, stress corrosion cracking resistance, and elongation are decreased. When the Ni content is less than 0.05%, the strength increasing effect by these precipitates is insufficient.

(13) Co is an element that forms precipitates with Al and the like to improve heat resistance and can be added as needed. When a Co content exceeds 0.15%, the elongation of the alloy is decreased. When the Co content is less than 0.05%, the strength increasing effect by these precipitates is insufficient.

(14) Ti is an element that increases strength through micronization of a cast structure and can be added as needed. When a Ti content exceeds 0.3%, the elongation of the alloy is decreased. When the Ti content is less than 0.05%, the strength increasing effect by micronization of the structure is insufficient.

(15) The fastening member 1 made of the aluminum alloy containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance Al with inevitable impurities has a tensile strength of 470 MPa or higher and 800 MPa or below. In addition, the fastening member 1 has a 0.2% proof stress of 400 MPa or higher and an elongation at break of 12% or less, which has thus improved toughness.

(16) The fastening member 1 is formed by performing wiredrawing processing, header processing, or the like on a rod-shaped member made of the aluminum alloy. When the fastening member 1 is formed by performing the wiredrawing processing and the header processing on the rod-shaped member, fiber flows, in which metallic crystals are elongated in a fiber form along the surface shape, are observed on the screw part 22. When a crack occurs on the screw part 22, the crack advances across the fiber flows. Consequently, the presence of the fiber flows can inhibit stress corrosion cracking.

(17) The first embodiment of the present invention described above manufactures the fastening member 1 using the aluminum alloy containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance aluminum (Al) with inevitable impurities and can thereby provide a fastening member having improved strength and toughness.

Second Embodiment

(18) FIG. 2 is a plan view of a structure of a fastening member according to a second embodiment of the present invention. This fastening member 5 illustrated in FIG. 2 is a nut (a kind of a female screw) made of the aluminum alloy. The fastening member 5 has a hollow cylindrical shape, in which a screw thread 52 is formed on an inner face of a hole 51 formed at the central part thereof. The shape (a hexagonal nut) of the fastening member 5 illustrated in FIG. 2 is only by way of example and can also be embodied as nuts having other shapes (a flange-equipped nut, a cap nut, a high nut, and the like).

(19) The fastening member 5 is formed using the aluminum alloy and is formed in a ring shape. The fastening member 5 is formed by performing wiredrawing processing, core hollowing processing, header processing, or the like on a rod-shaped member made of the aluminum alloy.

(20) The second embodiment of the present invention described above manufactures the fastening member 5 using the aluminum alloy containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance aluminum (Al) with inevitable impurities and can thereby provide a fastening member having improved strength and toughness in a manner similar to the first embodiment.

Third Embodiment

(21) FIG. 3 is a side view of a structure of a fastening member according to a third embodiment of the present invention. This fastening member 6 illustrated in FIG. 3 is a rivet made of the aluminum alloy. The fastening member 6 includes a cylindrical shaft 7, a head 8 provided on one end in a height direction of a cylinder forming the shaft 7 (the right-and-left direction in FIG. 3), and a neck 9 forming a boundary between the shaft 7 and the head 8. The shape (a round shape) of the head 8 illustrated in FIG. 3 is only by way of example and may have other shapes (a dish shape and the like).

(22) The fastening member 6 can be formed by performing wiredrawing processing, header processing, or the like on a rod-shaped member made of the aluminum alloy.

(23) The third embodiment of the present invention described above manufactures the fastening member 6 using the aluminum alloy containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance aluminum (Al) with inevitable impurities and can thereby provide a fastening member having improved strength and toughness in a manner similar to the first embodiment.

(24) Although the modes for performing the present invention have been described, the present invention should not be limited only by the first to the third embodiments. The fastening member according to the present invention can also be embodied as a machine screw or a tapping screw, which are male screws other than the bolt, for example.

(25) The present invention can thus include various kinds of embodiments that are not described herein, and various kinds of design changes can be made without departing from the technical ideas determined by the scope of claims.

EXAMPLES

(26) The following describes examples of the aluminum alloy according to the present invention. The present invention is not limited to these examples.

First to Tenth Examples and First to Fifth Comparative Examples

(27) Aluminum alloys of the individual compositions listed in Table 1 were melted with an electric furnace and were then cast to obtain ingots. Subsequently, these ingots were heated at a temperature of 500° C. to 560° C. to perform homogenization treatment. Furthermore, the ingots were subjected to hot rolling and wiredrawing processing to obtain wire rods with a diameter of 10 mm to 11 mm. These wire rods were cut into a certain dimension and were subjected to header processing to obtain blanks. The blanks were subjected to solution treatment under a condition with a temperature of 530° C. to 560° C., were subjected to artificial aging at a temperature of 150° C. to 200° C., and were then subjected to rolling to manufacture bolts with a nominal diameter of 8 mm and a pitch of 1.25 mm. These bolts were subjected to a tensile test to determine the tensile strength, 0.2% proof stress, and elongation at break thereof. Table 1 lists the results.

(28) TABLE-US-00001 TABLE 1 0.2% Tensile Proof Elongation strength stress at break Si Cu Mn Mg Zn Ni Co Ti Al (MPa) (MPa) (%) First Example 1.62 1.75 1.53 1.40 0.15 — — — Balance 513 462 10 Second Example 1.59 0.65 0.65 1.44 0.21 — — — Balance 496 417 12 Third Example 0.93 0.56 1.55 0.91 0.23 — — — Balance 499 429 12 Fourth Example 0.89 1.81 0.56 0.82 0.20 — — — Balance 503 443 10 Fifth Example 1.04 0.72 0.78 0.89 0.22 0.09 — — Balance 481 420 10 Sixth Example 1.02 0.72 0.76 0.88 0.34 — 0.11 — Balance 478 408 11 Seventh Example 1.05 0.71 0.77 0.88 0.31 — — 0.16 Balance 488 405 10 Eighth Example 1.06 0.70 0.76 0.84 0.35 0.06 — 0.19 Balance 506 449 10 Ninth Example 1.03 0.72 0.78 0.86 0.23 — 0.08 0.18 Balance 497 436 12 Tenth Example 0.99 0.74 0.72 0.87 0.33 0.10 0.11 — Balance 482 409 11 First 0.91 0.67 0.60 0.51 0.28 — — — Balance 421 350 14 Comparative Example Second 0.62 0.65 0.55 0.78 0.15 — — — Balance 415 348 14 Comparative Example Third 0.90 0.43 0.56 0.77 0.15 — — — Balance 423 347 14 Comparative Example Fourth 0.90 0.69 0.32 0.86 0.17 — — — Balance 430 368 15 Comparative Example Fifth 0.84 0.72 0.73 0.77 0.02 — — — Balance 457 389 13 Comparative Example

First to Fourth Examples

(29) The first to the fourth examples are aluminum alloys containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance aluminum (Al) with inevitable impurities.

Fifth to Tenth Examples

(30) The fifth to the tenth examples are aluminum alloys containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, and 0.1% to 0.7% of Zn and containing at least one selected from the group consisting of 0.05% to 0.15% of nickel (Ni), 0.05% to 0.15% of cobalt (Co), and 0.05% to 0.3% of titanium (Ti) and the balance aluminum (Al) with inevitable impurities.

First to Fifth Comparative Examples

(31) The first to the fifth comparative examples are, relative to the aluminum alloy containing 0.7% to 1.8% of Si, 0.5% to 2.1% of Cu, 0.4% to 1.8% of Mn, 0.6% to 1.6% of Mg, 0.1% to 0.7% of Zn, and the balance aluminum (Al) with inevitable impurities, out of the ranges in terms of any of the elements. Specifically, the first comparative example contains 0.51% of Mg, which is out of the range. The second comparative example contains 0.62% of Si, which is out of the range. The third comparative example contains 0.43% of Cu, which is out of the range. The fourth comparative example contains 0.32% of Mn, which is out of the range. The fifth comparative example contains 0.02% of Zn, which is out of the range.

(32) As to tensile strength, from Table 1, the first to the tenth examples each show 470 MPa or higher, whereas the first to the fifth comparative examples each show less than 470 MPa; it is revealed that the first to the tenth examples satisfy the strength described above and are thus higher in strength. As to 0.2% proof stress and elongation at break, from Table 1, the first to the tenth examples each show a 0.2% proof stress of 400 MPa or higher and an elongation at break of 12% or less, whereas the first to the fifth comparative examples each show a 0.2% proof stress of lower than 400 MPa and an elongation at break of 13% or more; it is revealed that the first to the tenth examples satisfy the strength described above and also have improved toughness.

INDUSTRIAL APPLICABILITY

(33) As described above, the aluminum alloy and the fastening member according to the present invention are suitable for providing a fastening member having improved strength and toughness.

REFERENCE SIGNS LIST

(34) 1, 5, 6 Fastening member 2, 7 Shaft 3, 8 Head 4, 9 Neck 21, 52 Screw thread 22 Screw part 51 Hole