JP2004323952A5 - - Google Patents

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JP2004323952A5
JP2004323952A5 JP2003123395A JP2003123395A JP2004323952A5 JP 2004323952 A5 JP2004323952 A5 JP 2004323952A5 JP 2003123395 A JP2003123395 A JP 2003123395A JP 2003123395 A JP2003123395 A JP 2003123395A JP 2004323952 A5 JP2004323952 A5 JP 2004323952A5
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range
grain boundaries
cooling
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sum
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JP4807484B2 (en
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【請求項3】 請求項2に記載の成形加工用アルミニウム合金板の製造方法において、
前記安定化処理の後、さらに100℃/min以上の加熱速度で170〜280℃の範囲内の温度に加熱してその範囲内の温度で5分以下保持した後、100℃/min以上の冷却速度で冷却する最終熱処理を施すことを特徴とする、曲げ加工その他の成形性および焼付硬化性に優れかつ伸びと曲げ異方性の少ない成形加工用アルミニウム合金板の製造方法。
3. The method for producing an aluminum alloy sheet for forming according to claim 2,
After the stabilization treatment, the mixture is further heated to a temperature in the range of 170 to 280 ° C. at a heating rate of 100 ° C./min or more and maintained at a temperature in the range for 5 minutes or less , and then cooled at a rate of 100 ° C./min or more. A method for producing an aluminum alloy sheet for forming, which is excellent in bending and other formability and bake hardenability and has low elongation and bending anisotropy, characterized by performing a final heat treatment of cooling at a high speed.

またさらに請求項3の発明の成形加工用アルミニウム合金板の製造方法は、請求項2に記載の成形加工用アルミニウム合金板の製造方法において、前記安定化処理の後、さらに100℃/min以上の加熱速度で170〜280℃の範囲内の温度に加熱してその範囲内の温度で5分以下保持した後、100℃/min以上の冷却速度で冷却する最終熱処理を施すことを特徴とするものである。 The method for producing an aluminum alloy sheet for forming according to the third aspect of the present invention is the method for producing an aluminum alloy sheet for forming according to the second aspect, wherein after the stabilizing treatment, the temperature is further increased to 100 ° C./min or more. After heating to a temperature in the range of 170 to 280 ° C. at a heating rate and maintaining the temperature within the range for 5 minutes or less , a final heat treatment of cooling at a cooling rate of 100 ° C./min or more is performed. It is.

さらにこの発明では、結晶組織における小角粒界の長さの和、すなわち回転角が5〜15°の範囲内にある粒界の長さの和が、回転角5°以上の全ての粒界の長さの総和に対し〜90%の範囲内にある必要がある。すなわち、5°以上15°以下の小角粒界の長さの和が、5°以上の全ての粒界長さの総和に対して一定の範囲内であることによって、粒界に沿うような曲げ割れを緩和する効果が得られる。そしてこの割合が2%未満では、良好な曲げ性が得られなくなるおそれがあり、一方90%を越えれば、成形加工時に肌荒れが生じて、板表面品質の低下を招くおそれがある。そこででこの発明では、良好な曲げ性を得ると同時に良好な板表面品質を得るため、上述のように小角粒界の割合を規定した。 Further, in the present invention, the sum of the lengths of the small-angle grain boundaries in the crystal structure, that is, the sum of the lengths of the grain boundaries having a rotation angle in the range of 5 to 15 °, is the sum of the lengths of all the grain boundaries having a rotation angle of 5 ° or more. It should fall within the range of 2-90% relative to the sum of the length. That is, since the sum of the lengths of the small-angle grain boundaries of 5 ° or more and 15 ° or less is within a certain range with respect to the sum of the lengths of all the grain boundaries of 5 ° or more, the bending along the grain boundaries is performed. The effect of alleviating cracks is obtained. If this ratio is less than 2%, good bendability may not be obtained. On the other hand, if it exceeds 90%, the surface may be roughened at the time of molding and the surface quality of the sheet may be degraded. Therefore, in the present invention, the ratio of the small-angle grain boundaries is specified as described above in order to obtain good bending properties and good sheet surface quality.

溶体化処理後には、100℃/min以上の冷却速度で、50℃以上、150℃未満の温度域まで冷却(焼入れ)する。ここで、溶体化処理後の冷却速度が100℃/min未満では、冷却中にMgSiあるいは単体Siが粒界に多量に析出してしまい、成形性、特にヘム曲げ性が低下すると同時に、焼付硬化性が低下して塗装焼付時の充分な強度向上が望めなくなる。 After the solution treatment, cooling (quenching) is performed at a cooling rate of 100 ° C / min or more to a temperature range of 50 ° C or more and less than 150 ° C. Here, if the cooling rate after the solution treatment is less than 100 ° C./min, a large amount of Mg 2 Si or elemental Si precipitates at the grain boundaries during cooling, and the moldability, particularly the hem bending property, decreases, and at the same time, The bake hardenability is reduced, and it is no longer possible to expect a sufficient improvement in the strength during baking.

前述のように安定化処理を行なった後には、これをそのまま製品板として、自動車ボディーシート等のための成形加工に供しても良いが、塗装焼付硬化性とヘム曲げ性をさらに向上させるためには、さらに最終熱処理を行なっても良い。この最終熱処理は、170〜280℃の温度範囲内に100℃以上の加熱速度で加熱して5分以下保持し、100℃/min以上の冷却速度で冷却する条件とする必要がある。 After performing the stabilization treatment as described above, it may be used as it is as a product plate, and may be subjected to a forming process for an automobile body sheet or the like, but in order to further improve paint baking hardenability and hem bending property. May be further subjected to a final heat treatment. The final heat treatment is heated to equity 5 minutes or less coercive at a heating rate of 100 ° C. or more within a temperature range of 170 to 280 ° C., it is necessary to make the conditions for cooling at 100 ° C. / min or higher cooling rate.

JP2003123395A 2003-04-28 2003-04-28 Aluminum alloy plate for forming and method for producing the same Expired - Fee Related JP4807484B2 (en)

Priority Applications (1)

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JP2003123395A JP4807484B2 (en) 2003-04-28 2003-04-28 Aluminum alloy plate for forming and method for producing the same

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Application Number Priority Date Filing Date Title
JP2003123395A JP4807484B2 (en) 2003-04-28 2003-04-28 Aluminum alloy plate for forming and method for producing the same

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JP2004323952A JP2004323952A (en) 2004-11-18
JP2004323952A5 true JP2004323952A5 (en) 2006-06-15
JP4807484B2 JP4807484B2 (en) 2011-11-02

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Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5148930B2 (en) * 2007-06-11 2013-02-20 住友軽金属工業株式会社 Method for producing Al-Mg-Si aluminum alloy plate for press forming, and Al-Mg-Si aluminum alloy plate for press forming
DE102013221710A1 (en) * 2013-10-25 2015-04-30 Sms Siemag Aktiengesellschaft Aluminum hot strip rolling mill and method for hot rolling an aluminum hot strip
CN103911533A (en) * 2014-04-26 2014-07-09 广东兴发铝业有限公司 Formula of 6061 aluminum alloy extrusion section for refrigerated container
JP6345016B2 (en) * 2014-07-24 2018-06-20 株式会社Uacj Aluminum alloy plate for hot forming and manufacturing method thereof
CN110714147B (en) * 2019-11-05 2021-06-01 郑州明泰实业有限公司 6082 aluminum alloy plate for aviation and preparation process thereof

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