WO2023233713A1 - Manufacturing method for high-strength aluminum alloy extruded material having excellent scc resistance - Google Patents
Manufacturing method for high-strength aluminum alloy extruded material having excellent scc resistance Download PDFInfo
- Publication number
- WO2023233713A1 WO2023233713A1 PCT/JP2023/004134 JP2023004134W WO2023233713A1 WO 2023233713 A1 WO2023233713 A1 WO 2023233713A1 JP 2023004134 W JP2023004134 W JP 2023004134W WO 2023233713 A1 WO2023233713 A1 WO 2023233713A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- extruded material
- aluminum alloy
- scc resistance
- billet
- cooled
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/002—Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
Definitions
- the present invention relates to a method for producing an extruded material using an Al-Zn-Mg-based aluminum alloy, and particularly to a method for producing an extruded material that has high strength and excellent SCC resistance.
- Patent Document 1 describes a technique in which a 7000-series aluminum alloy to which a relatively large amount of transition elements such as Mn, Cr, and Zr are added is subjected to restoring heat treatment. (SCC resistance) is insufficient.
- Patent Document 2 a high-strength material is obtained by adding transition elements such as Mn, Cr, and Zr and rolling or drawing after extrusion, but the SCC resistance is still poor, and it is difficult to achieve both high strength and SCC resistance. It is difficult to achieve this goal.
- An object of the present invention is to provide a method for manufacturing an aluminum alloy extrusion material that is effective in achieving high strength while ensuring excellent SCC resistance.
- the method for producing a high-strength aluminum alloy extruded material with excellent SCC resistance according to the present invention is as follows in mass %: Zn: 6.0 to 8.0%, Mg: 1.5 to 2.8%, Cu: 0.10 to 0.50%, Zr: 0.10 to 0.50%, Ti: 0.005 to 0.05%, Mn: 0.10 to 0.40%, Cr: 0.05% or less
- a billet is cast using an aluminum alloy in which the total of Mn+Cr+Zr is 0.10 to 0.50%, and the balance is Al and unavoidable impurities, and the billet obtained by the casting is heated at 470 to 560°C for 1 to 30 minutes.
- the billet After 14 hours of homogenization, the billet is cooled at a cooling rate of 50° C./hr or higher, extruded using the billet, immediately air cooled, and when the temperature of the extruded material reaches 300 to 480° C., the cooling rate is further increased to 150° C./hr. It is characterized by being cooled down to 200°C or less at a rate of 950°C/min, and then subjected to artificial aging treatment.
- the artificial aging treatment is performed at 80 to 130°C for 2 to 8 hours in the first stage, and 2 to 16 hours at 130 to 160°C in the second stage, and has a 0.2% yield strength of 460 MPa or more, and has excellent SCC resistance.
- the average crystal grain size of the extruded material is preferably 250 ⁇ m or less.
- the temperature of the extruded material immediately after extrusion is as high as 440 to 585° C. due to processing heat and the like. Therefore, quenching is possible by cooling immediately after extrusion, and this is called die end quenching.
- the present invention suppresses the amount of Cr added, adds Mn: 0.1 to 0.40% and Zr: 0.10 to 0.25%, which are relatively less sensitive to quenching, and increases the total amount of Mn + Cr + Zr.
- air cooling is performed at a cooling rate of 50 to 150 °C/min until the extruded material temperature reaches 300 to 480 °C from 500 to 585 °C immediately after extrusion, It is characterized by the fact that it is then rapidly cooled at a cooling rate of 150 to 950°C/min, thereby achieving high strength while suppressing a decrease in SCC resistance.
- ⁇ Zn, Mg> Zn and Mg components contribute to obtaining high strength.
- Zn can be added at a high concentration without comparably reducing extrudability, but if it is too large, the SCC resistance will decrease, so below, Zn is in the range of 6.0 to 8.0% by mass.
- Mg is in the range of 1.5 to 2.8%.
- ⁇ Cu> The Cu component is effective in achieving high strength due to its solid solution effect, but if it is too large, the extrudability and general corrosion resistance will decrease, so the Cu content is preferably in the range of 0.10 to 0.50%.
- Mn, Zr, Cr> Mn, Zr, and Cr are all transition elements, and can suppress the refinement of crystal grains and the depth of surface recrystallization during extrusion molding. While ensuring hardenability by cooling immediately after extrusion, considering air cooling in the high temperature range of the extruded material and rapid cooling from 300 to 480°C in the present invention, Mn: 0.10 to 0.40%, Zr: The content of Cr is preferably 0.10 to 0.25%, preferably at least 0.05%. Further, it is preferable to control the total amount of Mn+Cr+Zr within a range of 0.10 to 0.50%. ⁇ Ti> The Ti component is effective in refining crystal grains during billet casting.
- Ti is preferably in the range of 0.005 to 0.05%.
- ⁇ Fe, Si> Fe and Si components become impurities in the present invention, and it is preferable to suppress Fe to 0.4% or less and Si to 0.3% or less.
- the composition of the aluminum alloy used in the evaluation is shown.
- the manufacturing conditions of the billet and extruded material used in the evaluation are shown below.
- the evaluation results of extruded materials are shown.
- a molten metal having an aluminum alloy composition as shown in FIG. 1 was prepared, an 8-inch cylindrical billet was manufactured under the manufacturing conditions shown in FIG. 2, and after homogenization treatment, an extruded material was manufactured under the manufacturing conditions shown in FIG. Billets are cast using continuous casting methods such as hot top casting and insulated mold casting. At this time, when the casting speed is set to 50 mm/min or more, the billet's cast structure becomes a fine structure with an average crystal grain size of 250 ⁇ m or less.
- the average grain size indicates the average value of 3 ⁇ 3 points at the center of the cross section of the billet's tip, middle, and rear end, and an intermediate position between the periphery and the tip.
- Billet homogenization treatment is performed to eliminate micro-segregation that occurs during billet casting.
- the temperature is maintained at 470 to 560°C for 1 to 14 hours, and then the mixture is cooled at a cooling rate of 50°C/hr or more.
- the billet (BLT) is preheated to 400° C. or higher, preferably 440 to 500° C., and then filled into a container of an extruder and extruded.
- a direct extruder was used for extrusion processing.
- the temperature of the extruded material (extruded shape material) immediately after extrusion processing is 440°C or higher, preferably 480 to 510°C. Immediately after being extruded from the die, it is at a high temperature of 440° C. or higher, but it is air cooled at ambient temperature.
- the extruded material (extruded shape) is air cooled for at least about 0.1 min, and from the stage when the temperature of the extruded material (extruded shape) reaches 300 to 480°C, the temperature is kept at a rate of 150 to 950°C/min until the temperature reaches 200°C or less. It is characterized by water cooling or strong fan air cooling. In this way, in die end quenching during extrusion, a sufficient quenching effect can be obtained even if the extruded material is rapidly cooled at a rate of 150 to 950°C/min once the temperature of the extruded material reaches 300 to 480°C. Cooling strain is less likely to occur in the extruded material than die end quenching. This makes it possible to suppress deterioration in SCC resistance while maintaining high strength. This point will be discussed later by comparing Examples and Comparative Examples.
- the extruded material is subjected to artificial aging treatment at 80-130°C x 2-8 hr in the first stage and 2-8 hr at 130-160°C in the second stage, resulting in excellent SCC resistance and high strength extrusion. wood is obtained.
- the targets were T5 tensile strength of 480 MPa or more, 0.2% T5 yield strength of 460 MPa or more, and T5 elongation of 10% or more.
- the goal of SCC resistance stress corrosion cracking resistance
- the depth of the recrystallized layer formed on the surface of the extruded material was targeted to be 150 ⁇ m or less on average.
- Figures 1 to 3 show the manufacturing conditions of Examples 1 to 15 and Comparative Examples 1 to 4, and the evaluation results of the extruded materials obtained thereby.
- Examples 1 to 15 achieved the targets in all evaluation items, had high strength of 480 MPa or more in tensile strength and 460 MPa or more in 0.2% yield strength, and had excellent SCC resistance.
- Comparative Example 1 the quenching start temperature of the extruded material at 150 to 950°C/min was 500°C, which exceeded the upper limit of the specification of 480°C, so the SCC resistance did not reach the target.
- Comparative Example 2 Mn was 0.70%, which exceeded the upper limit of the standard 0.40%, and the quenching start temperature was high, so the SCC resistance did not reach the target. Moreover, the strength of Comparative Example 2 was lower than that of Comparative Example 1. In Comparative Example 3, the Cu component was 1.60%, which was higher than the upper limit of 0.50% of the specification, and even though it had high strength, the SCC resistance was significantly reduced. In Comparative Example 4, the Mg component was 1.21%, which was lower than the lower limit of the specification of 1.5%, so the strength did not reach the target.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Extrusion Of Metal (AREA)
Abstract
Description
本発明は、Al-Zn-Mg系のアルミニウム合金を用いた押出材の製造方法に関し、特に高強度でかつ耐SCC性に優れた押出材の製造方法に係る。 The present invention relates to a method for producing an extruded material using an Al-Zn-Mg-based aluminum alloy, and particularly to a method for producing an extruded material that has high strength and excellent SCC resistance.
Al-Zn-Mg系(7000系)アルミニウム合金は、高強度の押出材が得られることで、車両,産業機械等のいろいろな分野にて使用されている。
この種のアルミニウム合金は、ビレットの鋳造,均質化処理条件,押出条件や熱処理条件等によって、押出材の品質が大きく変化する。
例えば特許文献1には、Mn,Cr,Zr等の遷移元素を比較的多く添加した7000系のアルミニウム合金を用いて、復元熱処理を施した技術が記載されているが、そのままでは対応力腐食割れ性(耐SCC性)が不充分である。
特許文献2には、Mn,Cr,Zrの遷移元素の添加と、押出後の圧延又は引き抜き加工により高強度材を得ているが、やはり耐SCC性に劣り、高強度と耐SCC性の両立を図るのが困難である。
BACKGROUND ART Al-Zn-Mg (7000 series) aluminum alloys are used in various fields such as vehicles and industrial machinery because they produce high-strength extruded materials.
The quality of the extruded material of this type of aluminum alloy varies greatly depending on the billet casting, homogenization treatment conditions, extrusion conditions, heat treatment conditions, etc.
For example,
In
本発明は、優れた耐SCC性を確保しつつ、高強度化を図るのに有効なアルミニウム合金押出材の製造方法の提供を目的とする。 An object of the present invention is to provide a method for manufacturing an aluminum alloy extrusion material that is effective in achieving high strength while ensuring excellent SCC resistance.
本発明に係る耐SCC性に優れる高強度アルミニウム合金押出材の製造方法は、以下質量%にて、Zn:6.0~8.0%,Mg:1.5~2.8%,Cu:0.10~0.50%,Zr:0.10~0.50%,Ti:0.005~0.05%,Mn:0.10~0.40%,Cr:0.05%以下でMn+Cr+Zrの合計が0.10~0.50%であり、残部がAlと不可避的不純物からなるアルミニウム合金を用いてビレットを鋳造し、前記鋳造して得られたビレットを470~560℃,1~14時間の均質化処理後に冷却速度50℃/hr以上で冷却し、前記ビレットを用いて押出加工し、その直後に空冷し、押出材の温度が300~480℃になったらさらに冷却速度150~950℃/minの範囲にて200℃以下まで冷却し、その後に人工時効処理することを特徴とする。
ここで、人工時効処理は1段目80~130℃,2~8時間、2段目130~160℃,2~16時間であり、0.2%耐力460MPa以上を有し、耐SCC性に優れているのが好ましく、押出材の平均結晶粒径は250μm以下になっている。
The method for producing a high-strength aluminum alloy extruded material with excellent SCC resistance according to the present invention is as follows in mass %: Zn: 6.0 to 8.0%, Mg: 1.5 to 2.8%, Cu: 0.10 to 0.50%, Zr: 0.10 to 0.50%, Ti: 0.005 to 0.05%, Mn: 0.10 to 0.40%, Cr: 0.05% or less A billet is cast using an aluminum alloy in which the total of Mn+Cr+Zr is 0.10 to 0.50%, and the balance is Al and unavoidable impurities, and the billet obtained by the casting is heated at 470 to 560°C for 1 to 30 minutes. After 14 hours of homogenization, the billet is cooled at a cooling rate of 50° C./hr or higher, extruded using the billet, immediately air cooled, and when the temperature of the extruded material reaches 300 to 480° C., the cooling rate is further increased to 150° C./hr. It is characterized by being cooled down to 200°C or less at a rate of 950°C/min, and then subjected to artificial aging treatment.
Here, the artificial aging treatment is performed at 80 to 130°C for 2 to 8 hours in the first stage, and 2 to 16 hours at 130 to 160°C in the second stage, and has a 0.2% yield strength of 460 MPa or more, and has excellent SCC resistance. The average crystal grain size of the extruded material is preferably 250 μm or less.
Al-Zn-Mg系のアルミニウム合金を用いて、ビレットを鋳造し、このビレットを用いて押出加工すると、加工熱等により押出直後の押出材の温度は440~585℃の高温になっている。
したがって、押出直後に冷却することで焼入れが可能であり、これをダイス端焼入れと称されている。
When a billet is cast using an Al-Zn-Mg-based aluminum alloy and extruded using this billet, the temperature of the extruded material immediately after extrusion is as high as 440 to 585° C. due to processing heat and the like.
Therefore, quenching is possible by cooling immediately after extrusion, and this is called die end quenching.
このダイス端焼入れには、ファン等により空冷する方法と、水等により水冷する方法が知られている。
この場合に、アルミニウム合金中のMn,Cr,Zr等の遷移元素の添加により、結晶粒の微細化とともに焼入れ性を向上させている。
しかし、文献1や2に開示するように、Crの添加量が多くなると焼入れ感受性が鋭くなり、水冷レベルの急冷でないと充分な焼入れ効果が得られない。
しかし、押出加工直後の高温状態の押出材を水冷すると、押出材に冷却歪みが発生し、押出材の形状品質を確保するのが困難であるとともに、耐応力腐食割れ性(耐SCC性)が低下する技術的課題があった。
For this die end hardening, two methods are known: air cooling using a fan or the like, and water cooling using water or the like.
In this case, by adding transition elements such as Mn, Cr, and Zr to the aluminum alloy, grain size is refined and hardenability is improved.
However, as disclosed in
However, when extruded materials are cooled in a high-temperature state immediately after extrusion processing, cooling distortion occurs in the extruded materials, making it difficult to ensure the shape quality of the extruded materials and reducing stress corrosion cracking resistance (SCC resistance). There were declining technical challenges.
そこで本発明は、Crの添加量を抑え、相対的に焼入れ感受性が鋭くないMn:0.1~0.40%,Zr:0.10~0.25%の添加と、Mn+Cr+Zrの合計量を0.10~0.50%の範囲に制御することで、押出直後の押出材温度500~585℃から300~480℃になるまでは、冷却速度50~150℃/minレベルの空冷を施し、その後に冷却速度150~950℃/minの急冷を施すことで耐SCC性の低下を抑えつつ、高強度化を図った点に特徴がある。 Therefore, the present invention suppresses the amount of Cr added, adds Mn: 0.1 to 0.40% and Zr: 0.10 to 0.25%, which are relatively less sensitive to quenching, and increases the total amount of Mn + Cr + Zr. By controlling the temperature within the range of 0.10 to 0.50%, air cooling is performed at a cooling rate of 50 to 150 °C/min until the extruded material temperature reaches 300 to 480 °C from 500 to 585 °C immediately after extrusion, It is characterized by the fact that it is then rapidly cooled at a cooling rate of 150 to 950°C/min, thereby achieving high strength while suppressing a decrease in SCC resistance.
本発明におけるアルミニウム合金の組成の選定理由を以下説明する。
<Zn,Mg>
Zn及びMg成分は、高強度を得るのに寄与する。
その中でもZnは、比較的に押出性を低下させずに高濃度に添加できるが、多すぎると耐SCC性が低下するので、以下質量%でZn:6.0~8.0%の範囲が好ましく、Mgは1.5~2.8%の範囲とした。
<Cu>
Cu成分は、固溶効果により高強度化を図るのに有効であるが、多すぎると押出性の低下、一般耐食性が低下するので、Cu:0.10~0.50%の範囲が好ましい。
<Mn,Zr,Cr>
Mn,Zr,Crは、いずれも遷移元素であり、押出成形時における結晶粒の微細化と表面の再結晶深さを抑制できる。
押出直後の冷却にて焼入れ性を確保しつつ、本発明において押出材の高温度域における空冷と、300~480℃からの急冷を考慮すると、Mn:0.10~0.40%,Zr:0.10~0.25%,Crはできるだけ少なくし、少なくとも0.05%以下にするのが好ましい。
また、Mn+Cr+Zrの合計で、0.10~0.50%の範囲に制御するのが好ましい。
<Ti>
Ti成分は、ビレットの鋳造時の結晶粒の微細化に有効である。
Tiの溶解量を考慮して、Ti:0.005~0.05%範囲が好ましい。
<Fe,Si>
Fe,Si成分は、本発明において不純物となり、Fe:0.4%以下,Si:0.3%以下に抑えるのが好ましい。
The reason for selecting the composition of the aluminum alloy in the present invention will be explained below.
<Zn, Mg>
Zn and Mg components contribute to obtaining high strength.
Among them, Zn can be added at a high concentration without comparably reducing extrudability, but if it is too large, the SCC resistance will decrease, so below, Zn is in the range of 6.0 to 8.0% by mass. Preferably, Mg is in the range of 1.5 to 2.8%.
<Cu>
The Cu component is effective in achieving high strength due to its solid solution effect, but if it is too large, the extrudability and general corrosion resistance will decrease, so the Cu content is preferably in the range of 0.10 to 0.50%.
<Mn, Zr, Cr>
Mn, Zr, and Cr are all transition elements, and can suppress the refinement of crystal grains and the depth of surface recrystallization during extrusion molding.
While ensuring hardenability by cooling immediately after extrusion, considering air cooling in the high temperature range of the extruded material and rapid cooling from 300 to 480°C in the present invention, Mn: 0.10 to 0.40%, Zr: The content of Cr is preferably 0.10 to 0.25%, preferably at least 0.05%.
Further, it is preferable to control the total amount of Mn+Cr+Zr within a range of 0.10 to 0.50%.
<Ti>
The Ti component is effective in refining crystal grains during billet casting.
Considering the amount of dissolved Ti, Ti is preferably in the range of 0.005 to 0.05%.
<Fe, Si>
Fe and Si components become impurities in the present invention, and it is preferable to suppress Fe to 0.4% or less and Si to 0.3% or less.
本発明においては、押出成形直後の焼入れを押出温度が300~480℃までは空冷し、その後に冷却速度150~950℃/minの急冷をしても冷却歪みを抑え、耐SCC性の低下を抑えることができ、高強度との両立を図ることができる。 In the present invention, even if the quenching immediately after extrusion is air-cooled until the extrusion temperature reaches 300 to 480°C, and then rapid cooling is performed at a cooling rate of 150 to 950°C/min, cooling distortion can be suppressed and SCC resistance can be prevented from decreasing. Therefore, it is possible to achieve both high strength and high strength.
図1に示すようなアルミニウム合金組成の溶湯を調整し、図2に示す製造条件にて8インチ円柱ビレットを製作し、均質化処理後に図2に示した製造条件にて押出材を製造した。
ビレットの鋳造はホットトップ鋳造法、断熱鋳型式鋳造法等の連続鋳造法にて製造する。
この際に鋳造速度を50mm/min以上にすると、ビレットの鋳造組織は結晶平均粒径が250μm以下の微細な組織になる。
平均結晶粒径はビレットの先端部、中間部、後端部の断面中心、周縁部との中間位置の3×3点の平均値を示す。
ビレットの均質化処理(HOMO)は、ビレット鋳造時に生じたミクロ偏析を解消するために行われる。
均質化処理は470~560℃にて1~14時間保持した後に冷却速度50℃/hr以上にて冷却する。
A molten metal having an aluminum alloy composition as shown in FIG. 1 was prepared, an 8-inch cylindrical billet was manufactured under the manufacturing conditions shown in FIG. 2, and after homogenization treatment, an extruded material was manufactured under the manufacturing conditions shown in FIG.
Billets are cast using continuous casting methods such as hot top casting and insulated mold casting.
At this time, when the casting speed is set to 50 mm/min or more, the billet's cast structure becomes a fine structure with an average crystal grain size of 250 μm or less.
The average grain size indicates the average value of 3×3 points at the center of the cross section of the billet's tip, middle, and rear end, and an intermediate position between the periphery and the tip.
Billet homogenization treatment (HOMO) is performed to eliminate micro-segregation that occurs during billet casting.
In the homogenization treatment, the temperature is maintained at 470 to 560°C for 1 to 14 hours, and then the mixture is cooled at a cooling rate of 50°C/hr or more.
次に、ビレット(BLT)を400℃以上、好ましくは440~500℃に余熱した後に押出機のコンテナに充填し押出成形する。
押出加工は直接押出機を用いた。
押出加工直後の押出材(押出形材)の温度は440℃以上になっていて、好ましくは480~510℃になっているのがよい。
ダイスから押し出された直後は440℃以上の高温になっているが、雰囲気温度にて空冷される。
本発明においては、押出直後は約0.1min以上空冷され、押出材(押出形材)の温度が300~480℃になった段階から150~950℃/minの速度で200℃以下になるまで水冷あるいは強いファン空冷を実施した点に特徴がある。
このように押出成形持のダイス端焼入れにおいて、押出材の温度が300~480℃になった時点で150~950℃/minの速度で急冷しても充分に焼入れ効果が得られ、従来の水冷によるダイス端焼入れよりも押出材に冷却ひずみが生じにくい。
これにより高強度でありながら耐SCC性の低下を抑えることができる。
この点については実施例と比較例とにて比較し、後述する。
Next, the billet (BLT) is preheated to 400° C. or higher, preferably 440 to 500° C., and then filled into a container of an extruder and extruded.
A direct extruder was used for extrusion processing.
The temperature of the extruded material (extruded shape material) immediately after extrusion processing is 440°C or higher, preferably 480 to 510°C.
Immediately after being extruded from the die, it is at a high temperature of 440° C. or higher, but it is air cooled at ambient temperature.
In the present invention, immediately after extrusion, the extruded material (extruded shape) is air cooled for at least about 0.1 min, and from the stage when the temperature of the extruded material (extruded shape) reaches 300 to 480°C, the temperature is kept at a rate of 150 to 950°C/min until the temperature reaches 200°C or less. It is characterized by water cooling or strong fan air cooling.
In this way, in die end quenching during extrusion, a sufficient quenching effect can be obtained even if the extruded material is rapidly cooled at a rate of 150 to 950°C/min once the temperature of the extruded material reaches 300 to 480°C. Cooling strain is less likely to occur in the extruded material than die end quenching.
This makes it possible to suppress deterioration in SCC resistance while maintaining high strength.
This point will be discussed later by comparing Examples and Comparative Examples.
次に押出材は、1段目:80~130℃×2~8hr,2段目:130~160℃×2~8hrの人工時効処理を実施することで耐SCC性に優れ、高強度の押出材が得られる。
本発明においては、T5引張強さ480MPa以上,0.2%T5耐力460MPa以上,T5伸び10%以上を目標とした。
耐SCC性(耐応力腐食割れ性)は後述する試料条件にて、720サイクル以上割れが発生しないことを目標とした。
また、押出材の表面に形成される再結晶層の深さは平均で150μm以下を目標とした。
Next, the extruded material is subjected to artificial aging treatment at 80-130°C x 2-8 hr in the first stage and 2-8 hr at 130-160°C in the second stage, resulting in excellent SCC resistance and high strength extrusion. wood is obtained.
In the present invention, the targets were T5 tensile strength of 480 MPa or more, 0.2% T5 yield strength of 460 MPa or more, and T5 elongation of 10% or more.
The goal of SCC resistance (stress corrosion cracking resistance) was that no cracking occurred for 720 cycles or more under the sample conditions described below.
Furthermore, the depth of the recrystallized layer formed on the surface of the extruded material was targeted to be 150 μm or less on average.
押出材の評価方法を以下に説明する。
(1)機械的特性はJIS-Z2241に基づいて押出材の押出方向に沿ってJIS-5号引張試験片を作成し、JIS規格に準拠した引張試験機にて測定した。
(2)押出材の表面に形成される再結晶層の深さは、押出材より切り出したサンプルの断面を鏡面研磨仕上げを施し、3%NaOHの水酸化ナトリウム水溶液でエッチングを実施した。
次に光学顕微鏡観察により、金属組織の100倍画像から再結晶層の平均深さを測定した。
耐SCC性は試験片に耐力の80%の応力を負荷した状態で次の条件を1サイクルとし、割れ発生が720サイクル以上であったものを目標達成とした。
<1サイクル>
3.5%NaCl水溶液中に25℃,10min浸漬し、その後に25℃,湿度40%中に50min放置し、次に自然乾燥する。
The evaluation method for extruded materials will be explained below.
(1) Mechanical properties were measured by preparing a JIS-5 tensile test piece along the extrusion direction of the extruded material based on JIS-Z2241 and using a tensile tester compliant with JIS standards.
(2) The depth of the recrystallized layer formed on the surface of the extruded material was determined by mirror-polishing the cross section of the sample cut out from the extruded material and etching it with a 3% NaOH aqueous sodium hydroxide solution.
Next, the average depth of the recrystallized layer was measured from a 100x image of the metal structure by optical microscopic observation.
For SCC resistance, the following conditions were set as one cycle with a stress of 80% of the proof stress being applied to the test piece, and the target was achieved if cracking occurred for 720 cycles or more.
<1 cycle>
It is immersed in a 3.5% NaCl aqueous solution at 25°C for 10 minutes, then left at 25°C and 40% humidity for 50 minutes, and then air-dried.
(評価結果)
図1~3に実施例1~15と比較例1~4の製造条件と、それにより得られた押出材の評価結果を示す。
実施例1~15は全ての評価項目において目標を達成していて、引張強さ480MPa以上,0.2%耐力460MPa以上の高強度で、かつ、耐SCC性に優れていた。
これに対して比較例1は押出材の150~950℃/minの急冷開始温度が500℃と規格の上限480℃を超えていたので、耐SCC性が目標未達であった。
比較例2は、Mn:0.70%と規格の上限0.40%を超えていたのと、急冷開始温度が高く耐SCC性が目標未達であった。
また、比較例2は比較例1よりも強度が低かった。
比較例3は、Cu成分が1.60%と規格の上限0.50%よりも多いこともあり、高強度であっても、耐SCC性が著しく低下していた。
比較例4はMg成分が1.21%と規格下限1.5%よりも低いので、強度が目標未達であった。
(Evaluation results)
Figures 1 to 3 show the manufacturing conditions of Examples 1 to 15 and Comparative Examples 1 to 4, and the evaluation results of the extruded materials obtained thereby.
Examples 1 to 15 achieved the targets in all evaluation items, had high strength of 480 MPa or more in tensile strength and 460 MPa or more in 0.2% yield strength, and had excellent SCC resistance.
On the other hand, in Comparative Example 1, the quenching start temperature of the extruded material at 150 to 950°C/min was 500°C, which exceeded the upper limit of the specification of 480°C, so the SCC resistance did not reach the target.
In Comparative Example 2, Mn was 0.70%, which exceeded the upper limit of the standard 0.40%, and the quenching start temperature was high, so the SCC resistance did not reach the target.
Moreover, the strength of Comparative Example 2 was lower than that of Comparative Example 1.
In Comparative Example 3, the Cu component was 1.60%, which was higher than the upper limit of 0.50% of the specification, and even though it had high strength, the SCC resistance was significantly reduced.
In Comparative Example 4, the Mg component was 1.21%, which was lower than the lower limit of the specification of 1.5%, so the strength did not reach the target.
本発明に係るアルミニウム合金押出材の製造方法を用いると、耐SCC性に優れた高強度の押出材が得られるので、車両や産業機械等における各種構造部材に利用できる。 By using the method for producing an aluminum alloy extruded material according to the present invention, a high-strength extruded material with excellent SCC resistance can be obtained, so it can be used for various structural members in vehicles, industrial machinery, etc.
Claims (2)
前記鋳造して得られたビレットを470~560℃,1~14時間の均質化処理後に冷却速度50℃/hr以上で冷却し、
前記ビレットを用いて押出加工し、その直後に空冷し、押出材の温度が300~480℃になったらさらに冷却速度150~950℃/minの範囲にて200℃以下まで冷却し、その後に人工時効処理することを特徴とする耐SCC性に優れる高強度アルミニウム合金押出材の製造方法。 The following mass % is Zn: 6.0 to 8.0%, Mg: 1.5 to 2.8%, Cu: 0.10 to 0.50%, Zr: 0.10 to 0.50%, Ti: 0.005 to 0.05%, Mn: 0.10 to 0.40%, Cr: 0.05% or less, the total of Mn + Cr + Zr is 0.10 to 0.50%, and the balance is unavoidable as Al. A billet is cast using an aluminum alloy consisting of impurities,
The billet obtained by the casting is homogenized at 470 to 560°C for 1 to 14 hours, and then cooled at a cooling rate of 50°C/hr or more,
The billet is extruded and immediately cooled in the air, and when the temperature of the extruded material reaches 300 to 480°C, it is further cooled to 200°C or less at a cooling rate of 150 to 950°C/min, and then artificially processed. A method for producing a high-strength aluminum alloy extruded material with excellent SCC resistance, which comprises aging treatment.
0.2%耐力460MPa以上を有し、耐SCC性に優れることを特徴とする請求項1記載の耐SCC性に優れる高強度アルミニウム合金押出材の製造方法。 The artificial aging treatment is performed at 80 to 130 °C for 2 to 8 hours in the first stage, and 130 to 160 °C for 2 to 16 hours in the second stage,
The method for producing a high-strength aluminum alloy extruded material with excellent SCC resistance according to claim 1, characterized in that it has a 0.2% yield strength of 460 MPa or more and is excellent in SCC resistance.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE112023002454.5T DE112023002454T5 (en) | 2022-05-30 | 2023-02-08 | METHOD FOR PRODUCING HIGH STRENGTH EXTRUDED ALUMINUM ALLOY MATERIAL WITH HIGH SCC RESISTANCE |
| CN202380039181.6A CN119137306A (en) | 2022-05-30 | 2023-02-08 | Method for producing high-strength aluminum alloy extrusion material with excellent SCC resistance |
| JP2024524167A JPWO2023233713A1 (en) | 2022-05-30 | 2023-02-08 | |
| US18/940,989 US20250066895A1 (en) | 2022-05-30 | 2024-11-08 | Method For Producing High Strength Aluminum Alloy Extruded Material With High SCC Resistance |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2022087936 | 2022-05-30 | ||
| JP2022-087936 | 2022-05-30 |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US18/940,989 Continuation US20250066895A1 (en) | 2022-05-30 | 2024-11-08 | Method For Producing High Strength Aluminum Alloy Extruded Material With High SCC Resistance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2023233713A1 true WO2023233713A1 (en) | 2023-12-07 |
Family
ID=89026001
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2023/004134 Ceased WO2023233713A1 (en) | 2022-05-30 | 2023-02-08 | Manufacturing method for high-strength aluminum alloy extruded material having excellent scc resistance |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20250066895A1 (en) |
| JP (1) | JPWO2023233713A1 (en) |
| CN (1) | CN119137306A (en) |
| DE (1) | DE112023002454T5 (en) |
| WO (1) | WO2023233713A1 (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015137376A (en) * | 2014-01-21 | 2015-07-30 | 株式会社Uacj押出加工 | Under bracket for motorcycle and tricycle and method for manufacturing the same |
| JP2015137377A (en) * | 2014-01-21 | 2015-07-30 | 株式会社Uacj押出加工 | Under bracket for motorcycle and tricycle and method for manufacturing the same |
| JP2019206748A (en) * | 2018-05-23 | 2019-12-05 | アイシン軽金属株式会社 | Manufacturing method of high strength aluminum alloy extrusion material |
| JP2021110042A (en) * | 2020-01-15 | 2021-08-02 | アイシン軽金属株式会社 | Method for manufacturing high-strength aluminum alloy extruded material with excellent toughness and corrosion resistance |
| JP2021123798A (en) * | 2020-02-04 | 2021-08-30 | アイシン軽金属株式会社 | Method for producing high-strength aluminum alloy extruded material |
| WO2022181306A1 (en) * | 2021-02-25 | 2022-09-01 | アイシン軽金属株式会社 | Method for manufacturing aluminum alloy extruded material having high strength and excellent scc resistance and quenchability |
| WO2022181307A1 (en) * | 2021-02-25 | 2022-09-01 | アイシン軽金属株式会社 | Method for manufacturing aluminum alloy extruded material |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2928445B2 (en) | 1993-08-31 | 1999-08-03 | 株式会社神戸製鋼所 | High-strength aluminum alloy extruded material and method for producing the same |
| JP6195448B2 (en) | 2013-01-30 | 2017-09-13 | 株式会社神戸製鋼所 | Method for producing 7000 series aluminum alloy member excellent in stress corrosion cracking resistance |
-
2023
- 2023-02-08 WO PCT/JP2023/004134 patent/WO2023233713A1/en not_active Ceased
- 2023-02-08 DE DE112023002454.5T patent/DE112023002454T5/en active Pending
- 2023-02-08 CN CN202380039181.6A patent/CN119137306A/en active Pending
- 2023-02-08 JP JP2024524167A patent/JPWO2023233713A1/ja active Pending
-
2024
- 2024-11-08 US US18/940,989 patent/US20250066895A1/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015137376A (en) * | 2014-01-21 | 2015-07-30 | 株式会社Uacj押出加工 | Under bracket for motorcycle and tricycle and method for manufacturing the same |
| JP2015137377A (en) * | 2014-01-21 | 2015-07-30 | 株式会社Uacj押出加工 | Under bracket for motorcycle and tricycle and method for manufacturing the same |
| JP2019206748A (en) * | 2018-05-23 | 2019-12-05 | アイシン軽金属株式会社 | Manufacturing method of high strength aluminum alloy extrusion material |
| JP2021110042A (en) * | 2020-01-15 | 2021-08-02 | アイシン軽金属株式会社 | Method for manufacturing high-strength aluminum alloy extruded material with excellent toughness and corrosion resistance |
| JP2021123798A (en) * | 2020-02-04 | 2021-08-30 | アイシン軽金属株式会社 | Method for producing high-strength aluminum alloy extruded material |
| WO2022181306A1 (en) * | 2021-02-25 | 2022-09-01 | アイシン軽金属株式会社 | Method for manufacturing aluminum alloy extruded material having high strength and excellent scc resistance and quenchability |
| WO2022181307A1 (en) * | 2021-02-25 | 2022-09-01 | アイシン軽金属株式会社 | Method for manufacturing aluminum alloy extruded material |
Also Published As
| Publication number | Publication date |
|---|---|
| CN119137306A (en) | 2024-12-13 |
| DE112023002454T5 (en) | 2025-03-06 |
| JPWO2023233713A1 (en) | 2023-12-07 |
| US20250066895A1 (en) | 2025-02-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP5345056B2 (en) | Heat-treatable high-strength aluminum alloy | |
| JP6955483B2 (en) | High-strength aluminum alloy extruded material with excellent corrosion resistance and good hardenability and its manufacturing method | |
| JP3194742B2 (en) | Improved lithium aluminum alloy system | |
| US10087508B2 (en) | Aluminum alloy and method of manufacturing extrusion using same | |
| JP7018274B2 (en) | Aluminum alloy for extrusion molding and method for manufacturing extruded material using it | |
| JP7698953B2 (en) | Manufacturing method for high-strength aluminum alloy extrusion material with excellent toughness and corrosion resistance | |
| JP2007119904A (en) | High-strength aluminum alloy extruded product with excellent impact absorption and stress corrosion cracking resistance and method of manufacturing the same | |
| US10900108B2 (en) | Method for manufacturing bent article using aluminum alloy | |
| US20220364213A1 (en) | Method for Producing Aluminum Alloy Extrusion | |
| JP7479854B2 (en) | Manufacturing method of aluminum alloy extrusion material | |
| AU2017367371B2 (en) | Aluminum alloy for extruded material, extruded material using the same, and method for producing extruded material | |
| TWI434939B (en) | Aluminium alloy and process of preparation thereof | |
| US20230357902A1 (en) | Method For Manufacturing Aluminum Alloy Extruded Material With High Strength And Excellent In SCC Resistance And Hardenability | |
| US20230357889A1 (en) | Method For Manufacturing Aluminum Alloy Extruded Material | |
| US11827967B2 (en) | Method for producing aluminum alloy extruded material | |
| WO2023233713A1 (en) | Manufacturing method for high-strength aluminum alloy extruded material having excellent scc resistance | |
| JP2024139746A (en) | Manufacturing method for high-strength aluminum alloy extrusion material with excellent SCC resistance and aluminum alloy used therein | |
| JP2023126137A (en) | Production method of aluminum alloy extrusion material having excellent hardenability, high toughness and high strength |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 23815477 Country of ref document: EP Kind code of ref document: A1 |
|
| ENP | Entry into the national phase |
Ref document number: 2024524167 Country of ref document: JP Kind code of ref document: A |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 202380039181.6 Country of ref document: CN |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 112023002454 Country of ref document: DE |
|
| WWP | Wipo information: published in national office |
Ref document number: 112023002454 Country of ref document: DE |
|
| 122 | Ep: pct application non-entry in european phase |
Ref document number: 23815477 Country of ref document: EP Kind code of ref document: A1 |