Aluminum alloy foil for battery packaging

The aluminum alloy foil composition addresses issues of edge cracks and formability by optimizing Fe, Si, and Cu content, grain boundaries, and manufacturing processes, achieving high elongation and stable deformation for battery packaging applications.

JP7847567B2Active Publication Date: 2026-04-17MA ALUMINUM CORP
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Patent Information

Authority / Receiving Office
JP · JP
Patent Type
Patents
Current Assignee / Owner
MA ALUMINUM CORP
Filing Date
2023-06-22
Publication Date
2026-04-17

AI Technical Summary

Technical Problem

Existing aluminum alloy foils for battery packaging face issues with high Cu content leading to edge cracks during rolling, mixed grain boundaries affecting formability, and unstable elongation in multiple directions, especially when thickness is reduced.

Method used

An aluminum alloy foil composition with controlled Fe, Si, and Cu content, optimized grain boundary ratios, and intermetallic compound densities, along with specific manufacturing processes to achieve uniform grain size and texture for enhanced elongation and formability.

Benefits of technology

The solution results in an aluminum alloy foil with high elongation characteristics and improved formability, suitable for battery packaging, achieving stable deformation in multiple directions and reduced thickness without edge cracks.

✦ Generated by Eureka AI based on patent content.

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Abstract

To provide an aluminum alloy foil for battery packaging material having high elongation properties.SOLUTION: An aluminum alloy foil for battery packaging material according to the present invention contains Fe by 1.0 mass% or more and 1.8 mass% or less, Si by 0.01 mass% or more and 0.08 mass% or less, and Cu by 0.005 mass% or more and 0.05 mass% or less, regulates to Mn: 0.01 mass% or less, the balance has a composition consisting of Al and inevitable impurities, Cu orientation density is 40 or less and R orientation density is 30 or less as an aggregate structure, the density of an Al-Fe-based intermetallic compound having the particle diameter 1 μm or more and less than 3 μm is 1.2×104 / mm2 or more and, the density of an Al-Fe-based intermetallic compound having the particle diameter 0.1 μm or more and less than 1 μm is 2.1×105 / mm2 or more, the limit bulging height is 11.0 mm, and the thickness is 10 μm or more and 80 μm or less.SELECTED DRAWING: Figure 1
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Description

[Technical Field]

[0001] This invention relates to aluminum alloy foil for battery packaging. [Background technology]

[0002] Aluminum foil used in packaging for food products and batteries such as lithium-ion secondary batteries is subjected to significant deformation during press molding and other processes. Therefore, good formability has traditionally been required for aluminum foil used in packaging, and soft foils of 1000 series alloys such as 1N30 and 8000 series alloys such as 8079 and 8021 have been used. While elongation is an important parameter in the forming of aluminum alloy foil, the foil is not deformed in only one direction; rather, a process known as stretch forming is often used. Therefore, in aluminum alloy foil, high elongation is required not only in the direction parallel to the rolling direction, which is generally used as the material's elongation value, but also in other directions such as 45° and 90°. Furthermore, in recent years, there has been a trend towards reducing the thickness of aluminum alloy foil packaging materials, particularly in the battery packaging sector. [Prior art documents] [Patent Documents]

[0003] [Patent Document 1] International Publication No. 2014 / 021170 [Patent Document 2] International Publication No. 2014 / 034240 [Patent Document 3] Japanese Patent Publication No. 2004-27353 [Overview of the project] [Problems that the invention aims to solve]

[0004] However, there are concerns about the high amount of Cu added to the aluminum alloy foil described in Patent Document 1, which is up to 0.5 mass%. Since Cu is an element that reduces the rollability of aluminum alloy foil even in trace amounts, there is a risk that edge cracks will occur during rolling, causing the foil to break. In addition, the aluminum alloy foil described in Patent Document 1 has a large average grain size, which may make it difficult to maintain high formability when the foil thickness is reduced. The aluminum alloy foil described in Patent Document 2 specifies very fine grain size, but the grain boundaries are limited to those with an orientation difference of 5° or more. An orientation difference of 5° or more at the grain boundaries means that large-angle grain boundaries and small-angle grain boundaries are mixed together, and it is uncertain whether the grains surrounded by large-angle grain boundaries are fine. Unlike Patent Documents 1 and 2, Patent Document 3 describes a thin foil with a thickness of 10 μm or less, rather than a battery casing foil, and since it is manufactured without intermediate annealing, a texture develops. As a result, stable elongation cannot be obtained in the 0°, 45°, and 90° directions relative to the rolling direction. Furthermore, the average grain size is 10 μm or more, and high formability cannot be expected when the foil thickness is thin.

[0005] This invention was made against the backdrop of the above-mentioned problems, and one of its objectives is to provide an aluminum alloy foil for battery packaging that has good processability and high elongation characteristics. [Means for solving the problem]

[0006] (1) The aluminum alloy foil for battery packaging in this embodiment contains Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.08% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and unavoidable impurities. The texture has a Cu orientation density of 40 or less and an R orientation density of 30 or less, and the density of Al-Fe intermetallic compounds with a particle size of 1 μm to less than 3 μm is 1.2 × 10⁻⁶. 4 pieces / mm 2 The above results indicate that the density of Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm is 2.1 × 10⁻⁶.5 pieces / mm 2 That's all. , thick The thickness is between 10 μm and 80 μm. For a thickness of 10 μm, the limiting overhang height is 7.0 mm or more; for a thickness of 20 μm, it is 9.0 mm or more; for a thickness of 30 μm, it is 10.5 mm or more; for a thickness of 40 μm, it is 11.0 mm or more; for a thickness of 50 μm, it is 11.5 mm or more; for a thickness of 60 μm, it is 12.0 mm or more; for a thickness of 70 μm, it is 12.5 mm or more; and for a thickness of 80 μm, it is 13.0 mm or more. It is characterized by being such. (2) In the aluminum alloy foil for battery packaging of this embodiment, it is preferable that the elongation in the directions of 0°, 45°, and 90° with respect to the rolling direction is 28% or more. (3) In the aluminum alloy foil for battery packaging of this embodiment, it is preferable that the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is 6 μm or more and 15 μm or less, and that the ratio of the maximum grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more to the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is such that the relationship maximum grain size / average grain size ≤ 3.5.

[0007] (4) The aluminum alloy foil for battery packaging in this embodiment contains Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.08% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and unavoidable impurities, and the density of Al-Fe intermetallic compounds with a particle size of 1 μm to less than 3 μm is 1.2 × 10⁻¹⁴ 4 pieces / mm 2 The above results indicate that the density of Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm is 2.1 × 10⁻⁶. 5 pieces / mm 2 That's all. The thickness is between 10 μm and 80 μm, and the critical overhang height is 7.0 mm or more for a thickness of 10 μm, 9.0 mm or more for a thickness of 20 μm, 10.5 mm or more for a thickness of 30 μm, 11.0 mm or more for a thickness of 40 μm, 11.5 mm or more for a thickness of 50 μm, 12.0 mm or more for a thickness of 60 μm, 12.5 mm or more for a thickness of 70 μm, and 13.0 mm or more for a thickness of 80 μm. It is characterized by being such. (5) In the aluminum alloy foil for battery packaging of this embodiment, it is preferable that the elongation in the directions of 0°, 45°, and 90° with respect to the rolling direction is 28% or more. (6) In the aluminum alloy foil for battery packaging of this embodiment, it is preferable that the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is 6 μm or more and 15 μm or less, and that the ratio of the maximum grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more to the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is such that the relationship maximum grain size / average grain size ≤ 3.5. [Effects of the Invention]

[0008] According to the aluminum alloy foil of the present invention, an aluminum alloy foil having high elongation characteristics can be obtained.

Brief Description of the Drawings

[0009] [Figure 1] It is a figure which shows the planar shape of the square punch used by the limiting forming height test in the Example of this invention.

Modes for Carrying Out the Invention

[0010] Hereinafter, an example of an embodiment of the present invention will be described in detail based on the accompanying drawings. In addition, the drawings used in the following description may show, for the sake of clarity, the characteristic parts enlarged for convenience.

[0011] Hereinafter, the content defined by the aluminum alloy foil according to this embodiment will be described. The aluminum alloy foil according to this embodiment contains Fe: 1.0 mass% or more and 1.8 mass% or less, Si: 0.01 mass% or more and 0.08 mass% or less, Cu: 0.005 mass% or more and 0.05 mass% or less, is regulated to Mn: 0.01 mass% or less, and the balance consists of Al and unavoidable impurities.

[0012] In the aluminum alloy foil according to this embodiment, in the crystal orientation analysis per unit area by backscattered electron diffraction (EBSD), the ratio (HAGBs / LAGBs) of the length of high-angle grain boundaries (HAGBs) with an orientation difference of 15° or more and low-angle grain boundaries (LAGBs) with an orientation difference of 2° or more and less than 15° is more than 2.0, the Cu orientation density is 40 or less, and the R orientation density is 30 or less as an aggregate structure, and the difference (Ra 20 -Ra0) between the initial surface roughness Ra0 and the surface roughness Ra at the time of 20% strain in the tensile test is preferably 0.25 μm or less. 20 Moreover, in the aluminum alloy foil of this embodiment, it is preferable that the elongation in each direction of 0°, 45°, and 90° with respect to the rolling direction is 28% or more. ​Furthermore, in the aluminum alloy foil of this embodiment, it is preferable that the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is 6 μm or more and 15 μm or less, and that the maximum grain size / average grain size ≤ 3.5.

[0013] The following describes each element contained in the aluminum alloy that constitutes the aluminum alloy foil according to this embodiment. ·Fe: 1.0 mass% or more and 1.8 mass% or less Fe crystallizes as Al-Fe intermetallic compounds during casting, and if the size of these compounds is large, they act as recrystallization sites during annealing, resulting in the refinement of the recrystallized grains. If the Fe content falls below the lower limit (1.0 mass%), the distribution density of coarse intermetallic compounds decreases, reducing the refinement effect and resulting in a non-uniform final grain size distribution. If the Fe content exceeds the upper limit (1.8 mass%), the grain refinement effect saturates or even decreases, and the size of the Al-Fe compounds generated during casting becomes very large, reducing the elongation and rollability of the foil. Therefore, the Fe content is set within the above range. Furthermore, for the same reason, it is more preferable that the Fe content be between 1.0% by mass and 1.6% by mass.

[0014] ·Si: 0.01 mass% or more and 0.10 mass% or less Si forms intermetallic compounds with Fe, but high Si content leads to coarser compound size and reduced distribution density. If the Si content exceeds the upper limit (0.10 mass%), there is a concern that the rolling properties and elongation characteristics will decrease due to coarse precipitates, and furthermore, the uniformity of the recrystallized grain size distribution will decrease after final annealing. For these reasons, a lower Si content is preferable. However, if the Si content falls below the lower limit (0.01% by mass), it becomes necessary to use high-purity metal, which significantly increases manufacturing costs. Furthermore, if high-purity metal is used, trace components such as Cu will also be extremely low, raising concerns that excessive work softening may occur during cold rolling, resulting in reduced rollability. For these reasons, the Si content is set within the range of 0.01% by mass or more and 0.10% by mass or less. For similar reasons, it is preferable that the Si content be between 0.01% by mass and 0.05% by mass.

[0015] ·Cu: 0.005 mass% or more and 0.05 mass% or less Cu is an element that increases the strength of aluminum foil and decreases its elongation. On the other hand, it has the effect of suppressing excessive work softening during cold rolling. When the Cu content is less than 0.005 mass%, the effect of suppressing work softening is low, and when it exceeds 0.05 mass%, the elongation clearly decreases. For this reason, the Cu content is set within the above range. For similar reasons, it is more preferable that the Cu content be in the range of 0.005% by mass or more and 0.01% by mass or less.

[0016] ·Mn: 0.01 mass% or less Mn either dissolves in the aluminum matrix or forms very fine compounds, inhibiting the recrystallization of aluminum. While very small amounts of Mn can suppress work softening similarly to Cu, high amounts delay recrystallization during intermediate and final annealing, making it difficult to obtain fine, uniform crystal grains. Therefore, the Mn content is restricted to 0.01% by mass or less. Furthermore, for similar reasons, it is more preferable to have a Mn content of 0.005% by mass or less.

[0017] • "HAGBs / LAGBs>2.0" This is not limited to Al-Fe alloys, but the ratio of the length of large-angle grain boundaries (HAGBs) to the length of small-angle grain boundaries (LAGBs) (HAGBs / LAGBs) in the total grain boundaries changes depending on the recrystallization behavior during annealing. If the proportion of LAGBs is high after final annealing, even if the average grain size is fine, local deformation is more likely to occur and elongation will decrease if L1 / L2 ≤ 2.0. For this reason, it is desirable to set L1 / L2 > 2.0, and by satisfying this requirement, higher elongation can be expected. More preferably, the above ratio (HAGBs / LAGBs) should be 2.5 or higher. The lengths of large-angle and small-angle grain boundaries can be measured by SEM-EBSD, similar to grain size. L1 / L2 can be calculated from the total length of large-angle and small-angle grain boundaries in the area of ​​the observed field of view.

[0018] • "As a collective structure, the Cu azimuthal density is 40 or less, and the R azimuthal density is 30 or less." The texture significantly affects the elongation of the foil. When the Cu orientation density exceeds 40 and the R orientation density also exceeds 30, anisotropy occurs in the elongation values ​​at 0°, 45°, and 90°, and the elongation values ​​in the 0° and 90° directions decrease in particular. When anisotropy occurs in elongation, uniform deformation cannot be achieved during molding, and the moldability decreases. More preferably, the Cu orientation density is 30 or less and the R orientation density is 20 or less.

[0019] • Initial surface roughness Ra0 and surface roughness Ra at 20% strain in tensile testing 20 Difference (Ra 20 —Ra0) is 0.25 μm or less. The inventors have observed that the surface of aluminum foil becomes rougher as the molding process progresses, and it is hypothesized that good formability can be obtained when this surface roughness during molding is minimal. Factors influencing the surface roughness of aluminum foil during deformation include grain size, texture, and the distribution of intermetallic compounds, and these interact in a complex manner, with the full picture still not being clear. The inventors define the initial surface roughness of aluminum foil as Ra0, and the surface roughness of aluminum alloy foil at 20% strain during tensile deformation as Ra 20 In that case, the increase in surface roughness (Ra 20 We found that by suppressing the Ra0 value to 0.25 μm or less, it is possible to obtain a foil with good moldability. From this perspective, it is more preferable that the increase in surface roughness during the molding of the aluminum foil be 0.20 μm or less.

[0020] • "For crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more, the average grain size is between 6 μm and 15 μm, and the ratio of maximum grain size to average grain size is ≤ 3.5." Soft aluminum foil, with its fine grain structure, can suppress surface roughness during deformation, resulting in high elongation and consequently high formability. One factor influencing this surface roughness is grain size. To achieve high elongation and high formability, it is desirable that the average grain size of grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more be 15 μm or less. Furthermore, if the average grain size is less than 6 μm, formability decreases due to an increase in yield strength. Moreover, such fine grain structures tend to have a higher rate of continuous recrystallization during recrystallization, increasing the Cu orientation density in the texture and again posing a risk of reduced formability. Even with the same average grain size, if the grain size distribution is non-uniform, localized deformation is more likely to occur, reducing elongation. Therefore, high elongation can be obtained not only by setting the average grain size between 6 μm and 15 μm, but also by setting the maximum grain size / average grain size ≤ 3.5. Furthermore, the inventors have found that when the grain size exceeds 15 μm, surface roughness during molding becomes significant, indicating that controlling the grain structure is also important for suppressing surface roughness. Furthermore, the average grain size is preferably 5 μm or more and 10 μm or less, and the ratio is more preferably 2.5 or less. By analyzing the crystal orientation per unit area using backscatter electron diffraction (EBSD), a large-angle grain boundary map with an orientation difference of 15° or more can be obtained.

[0021] • "When the foil thickness is 40 μm, the elongation in the 0°, 45°, and 90° directions relative to the rolling direction is 28% or more." High formability depends on the elongation of the foil, and it is especially important that the elongation is high in the directions parallel to the rolling direction (0°), 45°, and 90° (normal to the rolling direction). The elongation value of the foil is greatly affected by the thickness of the foil, but high formability can be expected if the elongation is 28% or more at a thickness of 40 μm. As a guideline for thin foils, high formability can be expected if the elongation is 12% or more for a thickness of 10 μm, 16% or more for a thickness of 20 μm, and 22% or more for a thickness of 30 μm. As a guideline for thick foils, high formability can be expected if the elongation is 30% or more for a thickness of 50 μm, 32% or more for a thickness of 60 μm, 34% or more for a thickness of 70 μm, and 36% or more for a thickness of 80 μm.

[0022] • Density of Al-Fe intermetallic compounds with particle size between 1 μm and 3 μm: 1 × 10 4 pieces / mm 2 That's all." A particle size of 1 μm or larger is generally considered to be the size at which nucleation sites occur during recrystallization. The high density distribution of such intermetallic compounds makes it easier to obtain fine recrystallized grains during annealing. Particle size less than 1 μm, or density of 1 × 10⁻⁶ 4 pieces / mm 2 If the particle size is less than 3 μm, it is less likely to function effectively as a nucleation site during recrystallization, and if it exceeds 3 μm, it is more likely to lead to pinholes and reduced elongation during rolling. For this reason, it is desirable that the density of Al-Fe intermetallic compounds with a particle size of 1 μm or more and less than 3 μm be within the above range.

[0023] • Density of Al-Fe intermetallic compounds with particle size between 0.1 μm and 1 μm: 2 × 10 5 pieces / mm 2 That's all." Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm are generally considered to be a size that does not easily form nucleation sites during recrystallization. However, the present inventors have obtained results that suggest that they have a significant influence on grain refinement and recrystallization behavior. Although the overall mechanism is not yet clear, we have confirmed that the presence of high density of fine compounds smaller than 1 μm, in addition to coarse intermetallic compounds with a particle size of 1-3 μm, leads to recrystallization grain refinement after final annealing and suppression of the decrease in HAGBs length / LAGBs length. This may also promote grain subdivision during cold rolling. Therefore, it is desirable that the density of Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm be within the above range.

[0024] The following describes an example of a method for manufacturing aluminum alloy foil according to this embodiment. An aluminum alloy ingot was manufactured by preparing an aluminum alloy containing Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.10% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and other unavoidable impurities. The method of manufacturing the ingot is not particularly limited and can be carried out by conventional methods such as semi-continuous casting. The obtained ingot was subjected to a homogenization treatment by holding it at 480-550°C for 6 hours or more.

[0025] After homogenization, hot rolling is performed, setting the finished rolling temperature to 230°C or higher and less than 280°C. Then, cold rolling is performed, with intermediate annealing carried out during the cold rolling process. The temperature for intermediate annealing should be 300°C to 400°C. The intermediate annealing time is preferably 3 hours or more and less than 10 hours. If the annealing temperature is low, the material may not soften sufficiently, and long annealing times of 10 hours or more are not economically desirable. The cold rolling during the intermediate annealing stage corresponds to the final cold rolling, with a final cold rolling ratio of 92% or more. The final annealing is then carried out under conditions of holding the material at 250-350°C for 10 hours or more. The foil thickness is not particularly limited, but can be, for example, 10 μm to 80 μm. Alternatively, the foil thickness can be 10 μm to 70 μm, or 20 μm to 70 μm.

[0026] • "Homogenization treatment: Hold at 480-550°C for 6 hours or more." The homogenization process here aims to eliminate microsegregation within the ingot and adjust the distribution of intermetallic compounds, and is a crucial process for ultimately obtaining a fine and uniform grain structure. In the homogenization process, at temperatures below 480°C, while microsegregation within the ingot can be eliminated, Fe precipitation is insufficient, resulting in a high solid solution amount of Fe and a decrease in the density of coarse intermetallic compounds with a particle size of 1 μm to less than 3 μm, which serve as nucleation sites for recrystallization. As a result, the grain size tends to become coarser. Therefore, these factors can lead to the development of surface roughness. Furthermore, to precipitate fine intermetallic compounds with a particle size of 0.1 μm to less than 1 μm at high density, homogenization at the lowest possible temperature is effective, as the density of these fine intermetallic compounds decreases above 550°C. In the homogenization process, long heat treatment is necessary to precipitate intermetallic compounds at high density, and a minimum of 6 hours is required. If the homogenization process time is less than 6 hours, precipitation is insufficient, and the density of fine intermetallic compounds decreases.

[0027] • "Finished rolling temperature for hot rolling: 230°C or higher and less than 280°C" Hot rolling is performed after homogenization treatment. In hot rolling, it is desirable to keep the finishing temperature below 280°C to suppress recrystallization. By keeping the hot rolling finishing temperature below 280°C, the hot-rolled sheet will have a uniform fiber structure. By suppressing recrystallization after hot rolling in this way, the amount of strain accumulated up to the intermediate annealing thickness increases, and a fine recrystallized grain structure can be obtained during intermediate annealing. This leads to finer final grains and contributes to suppressing surface roughness. If the temperature exceeds 280°C, recrystallization will occur in some parts of the hot-rolled sheet, resulting in a mixture of fiber structure and recrystallized grain structure, which leads to non-uniformity of the recrystallized grain size during intermediate annealing, and this directly leads to non-uniformity of the final grain size. Finishing below 230°C requires extremely low temperatures during hot rolling, raising concerns that cracks may occur on the sides of the sheet, significantly reducing productivity.

[0028] • Intermediate annealing: 300℃~400℃ Intermediate annealing softens the material hardened by repeated cold rolling, restoring its rollability and promoting Fe precipitation, thereby reducing the amount of Fe in solid solution. If the intermediate annealing temperature is below 300°C, recrystallization will not be completed, resulting in a non-uniform grain structure and a risk of significant development of Cu orientation. Furthermore, at temperatures exceeding 400°C, recrystallized grains become coarser, and the final grain size also increases. At even higher temperatures, the amount of Fe precipitation decreases, and the amount of Fe in solid solution increases. A high amount of Fe in solid solution suppresses recrystallization during final annealing, and the proportion of small-angle grain boundaries increases, which is a factor in the decrease of HAGB / LAGB.

[0029] • "Final cold rolling ratio: 92% or higher" The higher the final cold rolling ratio from intermediate annealing to the final thickness, the greater the amount of strain accumulated in the material, resulting in finer recrystallized grains after final annealing. Furthermore, grain refinement occurs during the cold rolling process (grain subduction), so a higher final cold rolling ratio is desirable for this reason as well. Specifically, a final cold rolling ratio of 92% or higher is desirable. Below 92%, the amount of accumulated strain and grain refinement during rolling are insufficient, resulting in larger grain sizes after final annealing and worsening surface roughness. Additionally, the proportion of in-situ recrystallization increases, leading to an increase in LAGBs (Layered Grain Blocks) with orientation differences of less than 15° and a decrease in HAGBs / LAGBs. While there are no material-related disadvantages to exceeding the upper limit, manufacturing thin foils with cold rolling exceeding 99.9% can lead to reduced rollability and an increased risk of fracture due to side cracks. • Final annealing: Hold at 250-350°C for 10 hours or more. After the final cold rolling, the foil is annealed to completely soften it. Regarding the conditions for final annealing, temperatures below 250°C or holding times below 10 hours may result in insufficient softening, while temperatures above 350°C can lead to foil deformation and reduced economic efficiency. From an economic standpoint, the upper limit for the holding time during final annealing is preferably less than 100 hours.

[0030] The aluminum alloy foil obtained by the manufacturing method described above has excellent elongation properties. For example, when the thickness is 40 μm, the elongation in the 0°, 45°, and 90° directions relative to the rolling direction is 28% or more. Furthermore, in crystal orientation analysis per unit area by backscattered electron diffraction (EBSD) of the obtained aluminum alloy foil, the average grain size of the crystal grains surrounded by large-angle grain boundaries (grain boundaries with an orientation difference of 15° or more) is between 6 μm and 15 μm, and the maximum grain size / average grain size is ≤ 3.5, indicating that the crystal grains are of an appropriate size. Therefore, surface roughness when deformed can be suppressed. Furthermore, in the crystal orientation analysis per unit area using backscattered electron diffraction (EBSD), grain boundaries with an orientation difference of 15° or more are defined as small-angle grain boundaries, and grain boundaries with an orientation difference of 2° or more but less than 15° are defined as small-angle grain boundaries. When the length of the large-angle grain boundary is L1 and the length of the small-angle grain boundary is L2, L1 / L2 > 2.0 (HAGBs / LAGBs > 2.0). This results in higher elongation.

[0031] The resulting aluminum alloy foil can be deformed by press molding or other methods and can be suitably used as packaging material for food products or lithium-ion batteries. However, the uses of the aluminum alloy foil in this embodiment are not limited to those described above, and it can be used for any appropriate application. [Examples]

[0032] Aluminum alloy ingots having the compositions shown in Table 1 were produced by a semi-continuous casting method. Subsequently, the obtained ingots underwent homogenization, hot rolling, cold rolling, intermediate annealing, and further cold rolling according to the manufacturing conditions (homogenization treatment conditions, hot rolling finish temperature, intermediate annealing thickness, intermediate annealing conditions, and final cold rolling ratio) shown in Table 1, followed by batch-type final annealing at 290°C for 20 hours to produce aluminum alloy foil.

[0033] The following measurements and evaluations were performed on the obtained aluminum alloy foil. ·“Crystal grain size” After electropolishing the surface of aluminum alloy foil, crystal orientation analysis was performed using SEM (Scanning Electron Microscope)-EBSD. Grain boundaries with an orientation difference of 15° or more were defined as HAGBs (High-Angle Grain Boundaries), and the size of the grains enclosed by HAGBs was measured. Three fields of view with a magnification of ×1000 and a field size of 45 × 90 μm were measured, and the average grain size and the ratio of maximum grain size to average grain size were calculated. The grain size of each individual grain was calculated using the equivalent diameter of a circle, and the EBSD Area method (Average by Area Fraction Method) was used to calculate the average grain size. TSL Solutions' OIM Analysis was used for the analysis.

[0034] • "HAGBs / LAGBs" After electropolishing the surface of aluminum alloy foil, crystal orientation analysis was performed using SEM-EBSD to observe large-angle grain boundaries (HAGBs) with an orientation difference of 15° or more between crystal grains, and small-angle grain boundaries (LAGBs) with an orientation difference of 2° or more and less than 15°. Three fields of view were measured at a magnification of ×1000 with a field size of 45 × 90 μm, and the lengths of HAGBs and LAGBs within the field of view were determined, and their ratio was calculated. • "Crystal orientation" The Cu direction is {112}. <111> The R direction is {123} <634> The following directions were designated as representative directions. The orientation densities for each direction were measured using X-ray diffraction to obtain incomplete pole figures for {111}, {200}, and {220}. The results were then used to calculate and evaluate the three-dimensional orientation distribution function (ODF).

[0035] • "Tensile strength, elongation" All measurements were performed using tensile testing. In accordance with JIS Z2241, JIS No. 5 test specimens were taken from the sample to measure elongation in directions of 0°, 45°, and 90° relative to the rolling direction, and the tests were performed on a universal tensile testing machine (Shimadzu Corporation AGS-X 10kN) at a tensile speed of 2 mm / min. The calculation of elongation was as follows: First, before the test, two lines were marked perpendicular to the length of the specimen at a distance of 50 mm from the center of the specimen. After the test, the fracture surfaces of the aluminum alloy foil were joined together and the distance between the marks was measured. The elongation (mm), obtained by subtracting the gauge length (50 mm) from this distance, was divided by the distance between the gauge points (50 mm) to obtain the elongation (%).

[0036] • "Density of intermetallic compounds" Intermetallic compounds were observed by cutting the parallel cross-section (RD-ND plane) of aluminum alloy foil with a cross-section polisher (CP) and observing it with a field emission scanning electron microscope (FE-SEM: Carl Zeiss NVision40). For Al-Fe intermetallic compounds with particle sizes between 1 μm and 3 μm, the density was calculated by image analysis of 5 fields observed at a magnification of 2000x. For Al-Fe intermetallic compounds with particle sizes between 0.1 μm and 1 μm, the density was calculated by image analysis of 10 fields observed at a magnification of 10000x. The calculation results are shown in Table 1.

[0037] • "Maximum molding height" The limiting forming height was evaluated using a rectangular tube forming test. The test was conducted using a universal thin sheet forming tester (ERICHSEN Model 142 / 20), and a rectangular punch (side length L=37mm, corner chamfer diameter R=4.5mm) with the shape shown in Figure 1 was used for aluminum foil. The test conditions were a wrinkle-suppressing force of 10kN, a punch rising speed (forming speed) scale of 1, and mineral oil applied as a lubricant to one side of the foil (the side that the punch strikes). The punch rising from the bottom of the device struck the foil, forming the foil. The maximum punch rising height at which the foil could be formed without cracks or pinholes after three consecutive formings was defined as the limiting forming height (mm) for that material. The punch height was varied in 0.5mm increments. Here, for a foil thickness of 40μm, an overhang height of 11.0mm or more was considered good formability and judged as ○, and an overhang height of less than 11.0mm was judged as ×. The molding height, like elongation, is affected by the foil thickness; the thinner the foil, the lower the molding height. When testing with thin foil, the limiting overhang height was judged as good moldability (○) if it was 7.0 mm or more for a thickness of 10 μm, 9.0 mm or more for a thickness of 20 μm, and 10.5 mm or more for a thickness of 30 μm, while anything below the above boundary values ​​for each thickness was judged as ×. When testing with thick foil, the limiting overhang height was judged as good moldability (○) if it was 11.5 mm or more for a thickness of 50 μm, 12.0 mm or more for a thickness of 60 μm, 12.5 mm or more for a thickness of 70 μm, and 13.0 mm or more for a thickness of 80 μm or more, while anything below the above boundary values ​​for each thickness was judged as ×.

[0038] • Initial surface roughness Ra0 and surface roughness Ra at 20% strain in tensile testing 20 Difference (Ra 20 -Ra0)" Surface roughness Ra at 20% strain deformation in tensile testing 20 Measurements were performed using a laser microscope (Keyence VK-X100). Measurements were taken at the center of the width and length of the specimen, and measurements were performed on both the specimen before the tensile test and after deformation by 20% strain. The surface roughness Ra0 before the test and the surface roughness Ra0 after deformation by 20% strain were measured. 20 The increase in surface roughness (Ra) is calculated. 20 -Ra0) was calculated.

[0039] [Table 1]

[0040] [Table 2]

[0041] As shown in Tables 1 and 2, the composition contains Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.08% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and unavoidable impurities. In crystal orientation analysis per unit area by backscattered electron diffraction (EBSD), the ratio of the length of large-angle grain boundaries (HAGBs) with an orientation difference of 15° or more to the length of small-angle grain boundaries (LAGBs) with an orientation difference of 2° or more to less than 15° (HAGBs / LAGBs) is greater than 2.0. The texture has a Cu orientation density of 40 or less and an R orientation density of 30 or less. The initial surface roughness Ra0 and the surface roughness Ra at 20% strain in the tensile test are... 20 Difference (Ra 20 Examples 1 to 11, with a Ra0 of 0.25 μm or less and a foil thickness of 10 to 80 μm, all showed excellent values ​​for 0° elongation, 45° elongation, and 90° elongation, demonstrating well-balanced elongation. Furthermore, these examples demonstrated excellent limit molding height.

[0042] Compared to these examples, Comparative Examples 12-17 have Si content, Fe content, Cu content, or Mn content that falls outside the desired range. Therefore, the average particle size, particle size ratio, (HAGBs / LAGBs) value, Cu orientation or R orientation indicating the texture state, number of intermetallic compounds in the 1.0-3.0 μm or 0.1-1.0 μm range, (Ra 20 If any of the values ​​of (Ra0) fall outside the desired range, the elongation in one of the directions becomes insufficient, resulting in reduced moldability. Comparative Examples 18 and 19 show that the homogenization treatment temperature is either lower or higher than the desired range, (Ra 20 A larger value of -Ra0, or a larger particle size ratio and a smaller value of (HAGBs / LAGBs), resulted in decreased moldability. Comparative Example 20 had a high hot-finishing temperature, resulting in a large particle size ratio, a small (HAGBs / LAGBs) value, and reduced moldability. In Comparative Examples 21 and 22, the intermediate annealing temperature was either lower or higher than the desired range, resulting in a large grain size ratio and failure to meet the requirements for both Cu orientation density and R orientation density in the texture. This resulted in a poor texture or a small (HAGBs / LAGBs) value, leading to reduced moldability in both cases. Comparative Example 23 has a final cold rolling ratio of less than 92%, so the value of (HAGBs / LAGBs) is small, and (Ra 20 The value of -Ra0) increased, resulting in decreased moldability. [Explanation of symbols]

[0043] 1... Punch.

Claims

1. It has a composition containing Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.08% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and unavoidable impurities. The texture is such that the Cu orientation density is 40 or less and the R orientation density is 30 or less, and the density of Al-Fe intermetallic compounds with a particle size of 1 μm or more and less than 3 μm is 1.2 × 10⁻¹⁴. 4 pieces / mm 2 The above results indicate that the density of Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm is 2.1 × 10⁻⁶. 5 pieces / mm 2 The above conditions apply, and the thickness is between 10 μm and 80 μm. Aluminum alloy foil for battery packaging, characterized in that the maximum overhang height is 7.0 mm or more if the thickness is 10 μm, 9.0 mm or more if the thickness is 20 μm, 10.5 mm or more if the thickness is 30 μm, 11.0 mm or more if the thickness is 40 μm, 11.5 mm or more if the thickness is 50 μm, 12.0 mm or more if the thickness is 60 μm, 12.5 mm or more if the thickness is 70 μm, and 13.0 mm or more if the thickness is 80 μm.

2. The aluminum alloy foil for battery packaging according to claim 1, characterized in that the elongation in each direction of 0°, 45°, and 90° with respect to the rolling direction is 28% or more.

3. The aluminum alloy foil for battery packaging according to claim 1 or 2, characterized in that the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is 6 μm or more and 15 μm or less, and the ratio of the maximum grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more to the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is such that the relationship maximum grain size / average grain size ≤ 3.

5.

4. It has a composition containing Fe: 1.0% to 1.8% by mass, Si: 0.01% to 0.08% by mass, Cu: 0.005% to 0.05% by mass, Mn: restricted to 0.01% by mass or less, with the remainder being Al and unavoidable impurities. The density of Al-Fe intermetallic compounds with a particle size of 1 μm or more and less than 3 μm is 1.2 × 10⁻⁶ 4 pieces / mm 2 The above results indicate that the density of Al-Fe intermetallic compounds with a particle size of 0.1 μm or more and less than 1 μm is 2.1 × 10⁻⁶. 5 pieces / mm 2 The above conditions apply, and the thickness is between 10 μm and 80 μm. Aluminum alloy foil for battery packaging, characterized in that the maximum overhang height is 7.0 mm or more if the thickness is 10 μm, 9.0 mm or more if the thickness is 20 μm, 10.5 mm or more if the thickness is 30 μm, 11.0 mm or more if the thickness is 40 μm, 11.5 mm or more if the thickness is 50 μm, 12.0 mm or more if the thickness is 60 μm, 12.5 mm or more if the thickness is 70 μm, and 13.0 mm or more if the thickness is 80 μm.

5. The aluminum alloy foil for battery packaging according to claim 4, characterized in that the elongation in each direction of 0°, 45°, and 90° with respect to the rolling direction is 28% or more.

6. The aluminum alloy foil for battery packaging according to claim 4 or 5, characterized in that the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is 6 μm or more and 15 μm or less, and the ratio of the maximum grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more to the average grain size of the crystal grains surrounded by large-angle grain boundaries with an orientation difference of 15° or more is such that the relationship maximum grain size / average grain size ≤ 3.5.

Citation Information

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