TWI692531B - Aluminum alloy material and method for producing the same - Google Patents

Aluminum alloy material and method for producing the same Download PDF

Info

Publication number
TWI692531B
TWI692531B TW108119370A TW108119370A TWI692531B TW I692531 B TWI692531 B TW I692531B TW 108119370 A TW108119370 A TW 108119370A TW 108119370 A TW108119370 A TW 108119370A TW I692531 B TWI692531 B TW I692531B
Authority
TW
Taiwan
Prior art keywords
aluminum alloy
aluminum
alloy material
hot
manufacturing
Prior art date
Application number
TW108119370A
Other languages
Chinese (zh)
Other versions
TW202045743A (en
Inventor
庾忠義
石漢正
丁仕旋
Original Assignee
中國鋼鐵股份有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 中國鋼鐵股份有限公司 filed Critical 中國鋼鐵股份有限公司
Priority to TW108119370A priority Critical patent/TWI692531B/en
Application granted granted Critical
Publication of TWI692531B publication Critical patent/TWI692531B/en
Publication of TW202045743A publication Critical patent/TW202045743A/en

Links

Images

Landscapes

  • Metal Rolling (AREA)

Abstract

The present invention relates to an aluminum alloy material and a method for producing the same. An aluminum slab is firstly provided and subjected to a homogenizated process, thereby obtaining a homogenizated aluminum slab. Next, a cooling process including multiple cooling steps is performed to the homogenizated aluminum slab, so as to adjust a solid-solution amount of a cooled aluminum slab. Then, a hot rolling process and a cold rolling process are performed to the cooled aluminum slab, thereby producing the aluminum alloy material of the present invention. The aluminum alloy material has a suitable amount of pinning particles, thereby enhancing baking strength and pressure resistance of the aluminum alloy material.

Description

鋁合金材料及其製作方法 Aluminum alloy material and its manufacturing method

本發明係有關一種鋁合金,特別是提供一種具有良好耐壓性與烘烤強度之鋁合金材料及其製作方法。 The invention relates to an aluminum alloy, in particular to provide an aluminum alloy material with good pressure resistance and baking strength and a manufacturing method thereof.

罐裝飲料之市場競爭激烈,為了對陳出新,以提高銷量。部分業者於飲料中添加更多之二氧化碳(CO2),以提高飲品中之氣泡含量,而增加口感。然而,更多之二氧化碳亦大幅提升瓶內壓力,而使得飲料罐必須耐受更高壓力。再者,為了降低飲料罐之成本,製作罐身的鋁片厚度係被進一步減薄,而降低罐身強度。 The market for canned beverages is fiercely competitive, and in order to create new products to increase sales. Some businesses add more carbon dioxide (CO 2 ) to beverages to increase the content of bubbles in the beverage and increase the taste. However, more carbon dioxide also greatly increases the pressure inside the bottle, which makes the beverage cans have to withstand higher pressures. In addition, in order to reduce the cost of beverage cans, the thickness of the aluminum sheet for making the can body is further thinned to reduce the strength of the can body.

另外,為增添飲料罐之識別性,裝填飲品前須彩繪瓶身,故所製得之飲料罐須進一步進行烘烤製程,以烘乾漆料,並同時對罐身進行高溫殺菌。於此同時,烘烤製程之高溫易誘發材料中之差排組織的相消、重組與多邊形等回復(recovery)行為,而進一步降低飲料罐之強度。據此,為避免較薄之瓶身無法耐受更高之瓶內壓力,飲料罐之品質要求係越趨嚴格。 In addition, in order to increase the identification of the beverage can, the bottle body must be painted before filling the beverage. Therefore, the beverage can must be further baked to dry the paint and sterilize the can at the same time. At the same time, the high temperature of the baking process can easily induce the elimination, reorganization and recovery of polygons in the material, and further reduce the strength of the beverage can. Accordingly, in order to prevent thinner bottles from being able to withstand higher pressures in bottles, the quality requirements of beverage cans are becoming stricter.

一種習知方法係將鋁合金材料之析出顆粒的尺寸控制為大於1μm,並調整二次析出相之密度,惟其烘烤後之強度無法有效被提升,且具有較高之突耳率,而無法滿足後端應用之需求。另一種習知方法係額外添加Mg2Si與Al6Mn至鋁胚中,以降低所製得之鋁合金材料的突耳率,惟其烘烤後之強度降幅過大,而無法滿足應用之需求。 A conventional method is to control the size of the precipitated particles of the aluminum alloy material to be greater than 1 μm, and adjust the density of the secondary precipitated phase, but the strength after baking cannot be effectively improved, and has a higher lug rate, which cannot Meet the needs of back-end applications. Another conventional method is to add Mg 2 Si and Al 6 Mn to the aluminum embryo to reduce the lug ratio of the aluminum alloy material produced, but the strength drop after baking is too large to meet the needs of the application.

再一種習知方法係藉由調整熱處理之參數設定(例如:調高處理溫度、延長處理時間或加快淬火速度)及/或額外增設熱處理製程(例如:於冷軋製程前增設中間退火製程),來調整鋁合金材料之烘烤強度與耐壓性。然而,此些習知方法均未有效提升鋁合金材料烘烤後之強度。再者,額外增設之中間退火製程易大幅增加鋁合金材料的製作成本,而不符合經濟效益與節能之環保要求。 Another conventional method is by adjusting the heat treatment parameter settings (for example: increasing the treatment temperature, extending the treatment time or increasing the quenching speed) and/or additionally adding a heat treatment process (for example: adding an intermediate annealing process before the cold rolling process), To adjust the baking strength and pressure resistance of aluminum alloy materials. However, none of these conventional methods have effectively improved the strength of aluminum alloy materials after baking. In addition, the additional intermediate annealing process can easily increase the production cost of aluminum alloy materials, which does not meet the environmental protection requirements of economic efficiency and energy saving.

有鑑於此,亟須提供一種鋁合金材料及其製作方法,以改進習知鋁合金材料的缺陷。 In view of this, there is an urgent need to provide an aluminum alloy material and a manufacturing method thereof to improve the defects of conventional aluminum alloy materials.

因此,本發明之一態樣是在提供一種鋁合金材料的製作方法,其藉由均質化製程、分段冷卻與熱軋製程之特定參數,而可調整所製得之鋁合金材料的析出物之數量和尺寸,進而於烘烤製程時,可抑制次晶粒之粗化及差排之消散,因此提升鋁合金材料之烘烤強度與耐壓性。 Therefore, one aspect of the present invention is to provide a method for manufacturing an aluminum alloy material, which can adjust the precipitates of the aluminum alloy material obtained by the specific parameters of the homogenization process, the stage cooling and the hot rolling process The quantity and size, and furthermore, during the baking process, can suppress the coarsening of the secondary grains and the dissipation of the difference row, thus improving the baking strength and pressure resistance of the aluminum alloy material.

本發明之另一態樣是在提供一種鋁合金材料,其係藉由前述之製作方法所製得。 Another aspect of the present invention is to provide an aluminum alloy material, which is manufactured by the foregoing manufacturing method.

根據本發明之一態樣,提出一種鋁合金材料之製作方法。鋁胚係先被提供,並進行均質化製程,以製得均質化鋁胚。其中,鋁胚之材料為3000系鋁合金,且均質化製程之溫度不小於615℃。然後,對均質化鋁胚進行冷卻製程,以製得冷卻鋁胚。冷卻製程包含第一冷卻步驟、第二冷卻步驟與第三冷卻步驟,其中第一冷卻步驟係於2小時至6小時內將均質化鋁胚冷卻至520℃,第二冷卻步驟係於3小時內由520℃冷卻至350℃,且第三冷卻步驟係由350℃水淬至室溫。接著,對冷卻鋁胚進行熱軋製程,以製得熱軋鋁捲,並對熱軋鋁捲進行冷軋製程,即可製得鋁合金材料。 According to one aspect of the present invention, a method for manufacturing an aluminum alloy material is proposed. The aluminum embryo system is provided first and undergoes a homogenization process to obtain a homogenized aluminum embryo. Among them, the material of the aluminum embryo is 3000 series aluminum alloy, and the temperature of the homogenization process is not less than 615°C. Then, the homogenized aluminum embryo is subjected to a cooling process to obtain a cooled aluminum embryo. The cooling process includes a first cooling step, a second cooling step, and a third cooling step, where the first cooling step is to cool the homogenized aluminum embryo to 520°C within 2 hours to 6 hours, and the second cooling step is within 3 hours It is cooled from 520°C to 350°C, and the third cooling step is quenched from 350°C water to room temperature. Next, a hot rolling process is performed on the cooled aluminum blank to obtain a hot rolled aluminum coil, and a cold rolling process is performed on the hot rolled aluminum coil to obtain an aluminum alloy material.

依據本發明之一實施例,前述鋁胚包含大於0.2重量百分比之銅與大於0.2重量百分比之鋅。 According to an embodiment of the invention, the aforementioned aluminum blank includes greater than 0.2 weight percent copper and greater than 0.2 weight percent zinc.

依據本發明之一實施例,前述均質化製程之溫度小於鋁胚之熔點。 According to an embodiment of the invention, the temperature of the aforementioned homogenization process is less than the melting point of the aluminum embryo.

依據本發明之一實施例,前述之均質化製程至少進行12小時。 According to an embodiment of the invention, the aforementioned homogenization process is performed for at least 12 hours.

依據本發明之一實施例,前述之熱軋製程包含熱粗軋步驟與熱精軋步驟,且熱粗軋步驟與熱精軋步驟之間隔時間不大於360秒。 According to an embodiment of the invention, the aforementioned hot rolling process includes a hot rough rolling step and a hot finishing rolling step, and the interval between the hot rough rolling step and the hot finishing rolling step is not more than 360 seconds.

依據本發明之一實施例,前述熱軋製程之完軋盤捲溫度大於350℃。 According to an embodiment of the present invention, the temperature of the finished coil in the aforementioned hot rolling process is greater than 350°C.

依據本發明之一實施例,前述熱軋鋁捲之冷卻速率每分鐘不大於1℃。 According to an embodiment of the present invention, the cooling rate of the aforementioned hot rolled aluminum coil is not greater than 1°C per minute.

依據本發明之一實施例,於進行前述之冷軋製程前,製作方法不進行中間退火製程。 According to an embodiment of the present invention, before the aforementioned cold rolling process, the manufacturing method does not perform an intermediate annealing process.

根據本發明之另一態樣,提出一種鋁合金材料,其係藉由前述之製作方法所製得。此鋁合金材料於每立方微米(μm3)之單位體積含有30至80個釘紮顆粒,且每一個釘紮顆粒之粒徑小於1μm。 According to another aspect of the present invention, an aluminum alloy material is proposed, which is manufactured by the aforementioned manufacturing method. This aluminum alloy material contains 30 to 80 pinned particles per cubic micrometer (μm 3 ) of unit volume, and the diameter of each pinned particle is less than 1 μm.

依據本發明之一實施例,經220℃之烘烤後,前述鋁合金材料之降伏強度係大於260MPa,且降伏強度的降幅不大於20MPa。 According to an embodiment of the present invention, after baking at 220° C., the yield strength of the aforementioned aluminum alloy material is greater than 260 MPa, and the decrease in yield strength is not greater than 20 MPa.

應用本發明之鋁合金材料及其製作方法,其藉由均質化製程、冷卻製程之分段冷卻與熱軋製程之特定參數,來調控鋁合金材料之析出顆粒的數量與尺寸,以提供適當之釘紮力,進而於後端應用之烘烤製程中,有效抑制鋁合金材料中次晶粒的粗化與差排的消散,因此提升鋁合金材料之烘烤強度與耐壓性。 The aluminum alloy material of the present invention and its manufacturing method are used to control the number and size of the precipitated particles of the aluminum alloy material through the specific parameters of the homogenization process, the staged cooling of the cooling process and the hot rolling process to provide appropriate The pinning force, in the baking process of the back-end application, effectively suppresses the coarsening of secondary grains and the dissipation of the differential rows in the aluminum alloy material, thus improving the baking strength and pressure resistance of the aluminum alloy material.

100‧‧‧方法 100‧‧‧Method

110/120/131/133/135/140/150/160‧‧‧操作 110/120/131/133/135/140/150/160‧‧‧Operation

130‧‧‧冷卻製程 130‧‧‧cooling process

為了對本發明之實施例及其優點有更完整之理解,現請參照以下之說明並配合相應之圖式。必須強調的是,各種特徵並非依比例描繪且僅係為了圖解目的。相關圖式內容說明如下:〔圖1〕係繪示依照本發明之一實施例之鋁合金材料的製作方法之流程圖。 In order to have a more complete understanding of the embodiments of the present invention and its advantages, please refer to the following description and cooperate with the corresponding drawings. It must be emphasized that the various features are not drawn to scale and are for illustration purposes only. The contents of the related drawings are explained as follows: [FIG. 1] is a flowchart showing a method for manufacturing an aluminum alloy material according to an embodiment of the present invention.

以下仔細討論本發明實施例之製造和使用。然而,可以理解的是,實施例提供許多可應用的發明概念,其可實施於各式各樣的特定內容中。所討論之特定實施例僅供說明,並非用以限定本發明之範圍。 The manufacture and use of embodiments of the present invention are discussed in detail below. However, it can be understood that the embodiments provide many applicable inventive concepts that can be implemented in a variety of specific contents. The specific embodiments discussed are for illustration only and are not intended to limit the scope of the invention.

請參照圖1,其係繪示依照本發明之一實施例之鋁合金材料的製作方法之流程圖。方法100係先提供鋁胚,如操作110所示。鋁胚之材料可為3000系鋁合金。在一些實施例中,鋁胚可為3104鋁合金、3004鋁合金、其他適當之鋁合金材料,或上述材料之任意混合。在此些實施例中,鋁胚可包含大於0.2重量百分比之銅與大於0.2重量百分比之鋅。其中,銅與鋅之含量不超過規範含量(即3000系鋁合金之規範含量)。若銅或鋅之含量小於0.2重量百分比時,所製得之鋁合金材料具有較差之耐壓性,而無法滿足後端之應用需求。若銅或鋅之含量大於規範含量時,所製得之鋁合金材料無法滿足規定之規格,且過多之銅或鋅易降低鋁合金材料之耐腐蝕性,而使鋁合金材料具有易被腐蝕之缺陷。 Please refer to FIG. 1, which is a flowchart illustrating a method of manufacturing an aluminum alloy material according to an embodiment of the present invention. The method 100 first provides an aluminum blank, as shown in operation 110. The material of aluminum embryo can be 3000 series aluminum alloy. In some embodiments, the aluminum blank may be 3104 aluminum alloy, 3004 aluminum alloy, other suitable aluminum alloy materials, or any mixture of the foregoing materials. In such embodiments, the aluminum blank may include greater than 0.2 weight percent copper and greater than 0.2 weight percent zinc. Among them, the content of copper and zinc does not exceed the standard content (that is, the standard content of 3000 series aluminum alloy). If the content of copper or zinc is less than 0.2 weight percent, the aluminum alloy material obtained has poor pressure resistance, and cannot meet the application requirements of the back end. If the content of copper or zinc is greater than the standard content, the aluminum alloy material prepared cannot meet the specified specifications, and too much copper or zinc is easy to reduce the corrosion resistance of the aluminum alloy material, so that the aluminum alloy material is easy to be corroded defect.

然後,對鋁胚進行均質化製程,如操作120所示。當進行均質化製程時,鋁胚中之組成物可均勻地擴散分佈,而利於後續析出物之形成,進而可提升所製得鋁合金材料之烘烤強度與耐壓性。其次,於鑄造鋁胚時,部分組成物易形成尺寸較大之析出顆粒。於進行均質化製程時,此些析出顆粒可進一步被細化縮小。均質化製程之溫度不小於615℃。在一些實施例中,均質化製程之溫度係小於鋁胚之熔 點。若均質化製程之溫度小於615℃時,鋁胚中之組成物無法均勻擴散,而不利於後續析出物之形成,因此降低所製得之鋁合金材料之烘烤強度與耐壓性。在一些實施例中,均質化製程至少進行12小時。 Then, the aluminum embryo is subjected to a homogenization process, as shown in operation 120. When the homogenization process is performed, the components in the aluminum embryo can be evenly distributed and distributed, which is beneficial to the formation of subsequent precipitates, which can further improve the baking strength and pressure resistance of the aluminum alloy material obtained. Secondly, when casting aluminum embryos, part of the composition tends to form precipitated particles of larger size. During the homogenization process, these precipitated particles can be further refined and reduced. The temperature of the homogenization process is not less than 615℃. In some embodiments, the temperature of the homogenization process is less than the melting of the aluminum embryo point. If the temperature of the homogenization process is less than 615°C, the components in the aluminum embryo cannot be uniformly diffused, which is not conducive to the formation of subsequent precipitates, thus reducing the baking strength and pressure resistance of the aluminum alloy material obtained. In some embodiments, the homogenization process is performed for at least 12 hours.

於進行操作120後,對均質化製程所製得之均質化鋁胚進行冷卻製程130。其中,冷卻製程130包含多階段之冷卻步驟(如圖1所示之操作131至操作135),以調整所製得鋁合金材料之析出物數量、尺寸與分佈。首先,第一冷卻步驟係先進行,以控制析出物之尺寸。在一些實施例中,第一冷卻步驟係將均質化鋁胚由均質化製程之溫度緩慢冷卻至520℃。在一些實施例中,第一冷卻步驟係於2小時至6小時內將均質化鋁胚冷卻至520℃。若第一冷卻步驟係冷卻至小於520℃時,析出物之數量將過多且過密,而降低所製得鋁合金材料之烘烤強度與耐壓性。 After operation 120 is performed, a cooling process 130 is performed on the homogenized aluminum embryo produced by the homogenization process. The cooling process 130 includes a multi-stage cooling step (operation 131 to operation 135 shown in FIG. 1) to adjust the number, size and distribution of the precipitates of the aluminum alloy material. First, the first cooling step is performed first to control the size of the precipitate. In some embodiments, the first cooling step is to slowly cool the homogenized aluminum embryo from the temperature of the homogenization process to 520°C. In some embodiments, the first cooling step is to cool the homogenized aluminum embryo to 520°C within 2 hours to 6 hours. If the first cooling step is to cool to less than 520°C, the amount of precipitates will be too much and too dense, which will reduce the baking strength and pressure resistance of the aluminum alloy material produced.

於進行第一冷卻步驟後,進行第二冷卻步驟,以進一步降低鋁胚之溫度。於第二冷卻步驟中,為避免析出物大量析出,鋁胚須快速降溫至設定溫度(即低於易形成析出物的溫度範圍之溫度),以控制後續所形成之釘紮顆粒的密度,而使所製得之鋁合金材料滿足應用之需求。在一些實施例中,第二鋁卻步驟係於3小時內,將經第一冷卻步驟冷卻後之鋁胚冷卻至350℃或更低之溫度。換言之,於本發明之冷卻製程130中,鋁胚中之析出物主要係於第一冷卻步驟時析出。 After the first cooling step, the second cooling step is performed to further reduce the temperature of the aluminum blank. In the second cooling step, in order to avoid a large amount of precipitates, the aluminum embryo must be quickly cooled to a set temperature (that is, a temperature lower than the temperature range where precipitates are likely to form) to control the density of the subsequent pinned particles, and The prepared aluminum alloy material can meet the application requirements. In some embodiments, the second aluminum cooling step is within 3 hours, and the aluminum embryo cooled by the first cooling step is cooled to a temperature of 350°C or lower. In other words, in the cooling process 130 of the present invention, the precipitates in the aluminum embryo are mainly precipitated during the first cooling step.

於進行第二冷卻步驟後,進行第三冷卻步驟。由於鋁胚於第二冷卻步驟之溫度已低於易形成析出物之溫度,故第三冷卻步驟之冷卻速率沒有特別之限制。在一些實施例中,為縮短冷卻製程之時間,第三冷卻步驟可於鋁胚不變形之條件下,直接水淬至室溫。 After the second cooling step, the third cooling step is performed. Since the temperature of the aluminum embryo in the second cooling step is already lower than the temperature at which precipitates are easily formed, the cooling rate of the third cooling step is not particularly limited. In some embodiments, in order to shorten the time of the cooling process, the third cooling step can be directly water quenched to room temperature without the aluminum embryo deforming.

於進行冷卻製程130後,對所製得之冷卻鋁胚進行熱軋製程,以製得熱軋鋁捲,如操作140所示。在一些實施例中,熱軋製程包含熱粗軋步驟與熱精軋步驟。一般而言,於進行熱粗軋步驟之後,由於設備之限制,故經熱粗軋之熱軋鋁片須經一停留時間才可輸送至熱精軋機,以進行接續之熱精軋步驟(可理解的是,此停留時間即為熱粗軋步驟與熱精軋步驟之間隔時間)。惟,熱軋製程係於高溫下進行,故為避免過長之停留時間導致鋁片中之析出物再次析出,停留時間係不大於360秒。其次,為避免經熱粗軋步驟所製得之鋁合金片的溫度降低過多,而須重新加熱,故停留時間係不大於360秒。 After the cooling process 130 is performed, a hot rolling process is performed on the obtained cooled aluminum blank to obtain a hot rolled aluminum coil, as shown in operation 140. In some embodiments, the hot rolling process includes a hot rough rolling step and a hot finish rolling step. Generally speaking, after the hot rough rolling step, due to the limitations of the equipment, the hot rolled aluminum sheet after the hot rough rolling must be transported to the hot finishing mill after a residence time for the subsequent hot finish rolling step (may It is understood that this residence time is the interval time between the hot rough rolling step and the hot finish rolling step). However, the hot rolling process is carried out at a high temperature, so in order to avoid excessive residence time causing the precipitation in the aluminum sheet to precipitate again, the residence time is not more than 360 seconds. Secondly, in order to avoid the temperature of the aluminum alloy sheet produced by the hot rough rolling step decreasing too much, it needs to be reheated, so the residence time is not more than 360 seconds.

在一些實施例中,熱軋製程之完軋盤捲溫度可大於350℃,且熱軋製程所製得之熱軋鋁捲的冷卻速率不大於1℃/分鐘,以維持所需之固溶量。 In some embodiments, the temperature of the finished coil in the hot rolling process may be greater than 350°C, and the cooling rate of the hot rolled aluminum coil produced in the hot rolling process is not greater than 1°C/min to maintain the required amount of solution .

於進行操作140後,對熱軋鋁捲進行冷軋製程,即可製得本發明之鋁合金材料,如操作150與操作160所示。在一些實施例中,冷軋製程之冷軋量可為85%至90%。於所製得之鋁合金材料中,藉由前述之均質化製程、冷卻製程與熱軋製程,鋁合金材料具有粒徑小於1μm之釘 紮顆粒(即析出物)。在一些具體例中,釘紮顆粒於鋁合金材料之顆粒密度為30個/μm3至80個/μm3After operation 140, the hot-rolled aluminum coil is cold-rolled to obtain the aluminum alloy material of the present invention, as shown in operations 150 and 160. In some embodiments, the cold rolling volume of the cold rolling process may be 85% to 90%. In the prepared aluminum alloy material, through the aforementioned homogenization process, cooling process and hot rolling process, the aluminum alloy material has pinned particles (ie, precipitates) with a particle size of less than 1 μm. In some specific examples, the particle density of the pinned particles on the aluminum alloy material is 30 particles/μm 3 to 80 particles/μm 3 .

於後端應用時,所製得之鋁合金材料經220℃之烘烤後,鋁合金材料之降伏強度係大於260MPa,且降伏強度的降幅不大於20MPa。據此,本發明所製得之鋁合金材料具有良好之烘烤強度。其次,由於釘紮顆粒係分佈於鋁合金材料中,故釘紮顆粒可提供釘紮力,而可有效抑制晶界與差排(dislocation)之移動。因此,經高溫烘烤後,鋁合金材料於橫方向(即垂直於軋延方向)上的次晶粒之平均尺寸係不大於1.5μm,且次晶粒並無明顯粗化。另外,於烘烤時,釘紮顆粒可有效抑制差排的移動,而可降低差排之消散速度,進而抑制差排密度減少(即抑制回復速度)的程度。在一些具體例中,於烘烤後,鋁合金材料之差排密度不小於1012cm/cm3In the back-end application, after the baked aluminum alloy material is baked at 220°C, the yield strength of the aluminum alloy material is greater than 260 MPa, and the reduction in yield strength is not greater than 20 MPa. Accordingly, the aluminum alloy material prepared by the present invention has good baking strength. Secondly, since the pinned particles are distributed in the aluminum alloy material, the pinned particles can provide the pinning force, and can effectively suppress the movement of grain boundaries and dislocations. Therefore, after baking at high temperature, the average size of the secondary grains of the aluminum alloy material in the lateral direction (that is, perpendicular to the rolling direction) is not greater than 1.5 μm, and the secondary grains are not significantly coarsened. In addition, during baking, the pinned particles can effectively suppress the movement of the differential row, and can reduce the dissipation speed of the differential row, thereby suppressing the degree of reduction of the differential row density (ie, the suppression of the recovery speed). In some specific examples, after baking, the difference in row density of the aluminum alloy material is not less than 10 12 cm/cm 3 .

由於本發明之鋁合金材料具有適當數量之釘紮顆粒,故所製得鋁合金材料之耐壓性係不小於6.4Kg/cm2,而可滿足後端應用之需求。 Since the aluminum alloy material of the present invention has an appropriate number of pinned particles, the pressure resistance of the prepared aluminum alloy material is not less than 6.4Kg/cm 2 , which can meet the requirements of back-end applications.

在一些實施例中,於進行冷軋製程前,本發明之製作方法100不須進行中間退火製程。故,本發明之製作方法100可有效降低能量之損耗,並縮短製程時間。 In some embodiments, before the cold rolling process, the manufacturing method 100 of the present invention does not require an intermediate annealing process. Therefore, the manufacturing method 100 of the present invention can effectively reduce energy loss and shorten process time.

在一應用例中,本發明之鋁合金材料具有適當數量之析出物,而可有效釘紮晶界與差排於烘烤時之移動,進而可抑制鋁合金材料經烘烤時之次晶粒粗化程度與差排 之消散速度。因此,所製得之鋁合金材料具有良好之烘烤強度與耐壓性。 In an application example, the aluminum alloy material of the present invention has an appropriate amount of precipitates, which can effectively pin the grain boundaries and the movement of the differential row during baking, thereby suppressing secondary grains of the aluminum alloy material after baking Coarseness and difference The speed of dissipation. Therefore, the prepared aluminum alloy material has good baking strength and pressure resistance.

以下利用實施例以說明本發明之應用,然其並非用以限定本發明,任何熟習此技藝者,在不脫離本發明之精神和範圍內,當可作各種之更動與潤飾。 The following examples are used to illustrate the application of the present invention, but it is not intended to limit the present invention. Anyone who is familiar with this art can make various changes and modifications without departing from the spirit and scope of the present invention.

製備鋁合金材料Preparation of aluminum alloy materials

以下係根據第1表製備實施例1至實施例4與比較例1至比較例7之鋁合金材料。 The aluminum alloy materials of Examples 1 to 4 and Comparative Examples 1 to 7 are prepared according to Table 1 below.

實施例1Example 1

首先,對滿足3104鋁合金之規範的鋁合金原料進行澆鑄製程,以製得實施例1之鋁胚。其中,銅與鋅之含量分別為0.23重量百分比。然後,以大於615℃之溫度對鋁胚進行均質化製程。經過12小時後,對鋁胚進行冷卻製程,其中冷卻製程係區分為三個階段。於第一冷卻步驟中,鋁胚係於3.8小時內由均質化溫度冷卻至520℃。然後,進行第二冷卻步驟,以於2.14小時內由520℃冷卻至350℃。接著,以水淬之方式直接將鋁胚冷卻至室溫。 First, the aluminum alloy raw material that meets the specifications of the 3104 aluminum alloy is subjected to a casting process to obtain the aluminum blank of Example 1. Among them, the contents of copper and zinc are 0.23% by weight. Then, the aluminum embryo is homogenized at a temperature greater than 615°C. After 12 hours, the aluminum blank was cooled, and the cooling process was divided into three stages. In the first cooling step, the aluminum embryo was cooled from the homogenization temperature to 520°C within 3.8 hours. Then, a second cooling step was performed to cool from 520°C to 350°C in 2.14 hours. Next, the aluminum blank was directly cooled to room temperature by water quenching.

進行冷卻製程後,對鋁胚進行熱軋製程。其中,熱粗軋步驟所製得之鋁合金片經196秒之停留時間後,進行熱精軋步驟。熱精軋步驟所製得之熱軋鋁捲的完軋盤捲溫度為362℃,且冷卻速率為0.62℃/min。熱軋製程所製得之鋁捲係進一步進行冷軋量為85%至90%之冷軋製程,以製得 實施例1之鋁合金材料,並以下述之評價方式進行評價,其結果如第1表所示。 After the cooling process, the aluminum blank is hot rolled. Among them, the aluminum alloy sheet produced by the hot rough rolling step undergoes a hot finish rolling step after a residence time of 196 seconds. The temperature of the finished coil of the hot-rolled aluminum coil produced in the hot finish rolling step is 362°C, and the cooling rate is 0.62°C/min. The aluminum coil produced by the hot rolling process is further subjected to a cold rolling process with a cold rolling amount of 85% to 90% to obtain The aluminum alloy material of Example 1 was evaluated by the following evaluation method, and the results are shown in Table 1.

實施例2至實施例4與比較例1至比較例6Examples 2 to 4 and Comparative Examples 1 to 6

實施例2至實施例4與比較例1至比較例6係使用與實施例1之鋁合金材料相同之製造方法,不同之處在於實施例2至實施例4及比較例1至比較例6係改變鋁胚中之銅與鋅的含量,以及冷卻製程、熱軋製程與冷軋製程等之參數設定。其條件及評價結果如第1表所示,在此不另贅述。 Examples 2 to 4 and Comparative Examples 1 to 6 use the same manufacturing method as the aluminum alloy material of Example 1, except that Examples 2 to 4 and Comparative Examples 1 to 6 Change the content of copper and zinc in the aluminum embryo, as well as the parameter settings of the cooling process, hot rolling process and cold rolling process. The conditions and evaluation results are shown in Table 1, and are not repeated here.

比較例7Comparative Example 7

比較例7係使用與實施例1之鋁合金材料相同之製造方法,不同之處在於比較例7係改變鋁胚中之銅與鋅的含量,且於進行均質化製程後,以特定之設備於5小時內將鋁胚由均質化溫度緩冷至480℃至520℃,並於同一設備中直接進行熱軋製程。經熱軋製程與冷軋製程後,即可製得比較例7之鋁合金材料。所得之鋁合金原料以下述之評價方式進行評價,其結果如第1表所示。 Comparative Example 7 uses the same manufacturing method as the aluminum alloy material of Example 1, except that Comparative Example 7 changes the content of copper and zinc in the aluminum embryo, and after performing the homogenization process, using specific equipment in Within 5 hours, the aluminum embryo was slowly cooled from the homogenization temperature to 480°C to 520°C, and the hot rolling process was directly performed in the same equipment. After the hot rolling process and the cold rolling process, the aluminum alloy material of Comparative Example 7 can be produced. The obtained aluminum alloy raw material was evaluated by the following evaluation method, and the results are shown in Table 1.

評價項目Evaluation project 1.顆粒密度1. Particle density

實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料的顆粒密度係以穿透式電子顯微鏡(Transmission electron microscope;TEM)來量測。 The particle density of the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 was measured with a transmission electron microscope (TEM).

2.突耳率2. Lug rate

實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料的突耳率係以本發明所屬技術領域具有通常知識者所熟知之方法量測,並以下述之基準進行評價: The lug ratio of the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 is measured by a method well known to those of ordinary skill in the technical field to which the present invention pertains, and is performed according to the following criteria Evaluation:

◎:突耳率約為1%。 ◎: The lug rate is about 1%.

○:突耳率約為2%。 ○: The lug rate is about 2%.

×:突耳率約為3%。 ×: The lug rate is about 3%.

3.烘烤後次晶粒尺寸3. Secondary grain size after baking

首先,分別對實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料放置於220℃之環境中,以進行烘烤製程。然後,以穿透式電子顯微鏡來量測鋁合金材料中之次晶粒的尺寸。其中,次晶粒尺寸係指於橫方向(即垂直於軋延方向)上之次晶粒所對應的等效橢圓之長軸。 First, the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 are placed in an environment of 220° C. to perform a baking process. Then, the size of the secondary grains in the aluminum alloy material is measured with a transmission electron microscope. The secondary grain size refers to the long axis of the equivalent ellipse corresponding to the secondary grain in the lateral direction (that is, perpendicular to the rolling direction).

4.烘烤後差排密度4. Poor row density after baking

首先,分別對實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料放置於220℃之環境中,以進行烘烤製程。然後,以穿透式電子顯微鏡來量測鋁合金材料中之差排密度。 First, the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 are placed in an environment of 220° C. to perform a baking process. Then, a transmission electron microscope is used to measure the differential row density in the aluminum alloy material.

5.烘烤後降伏強度5. Yield strength after baking

首先,以本發明所屬技術領域具有通常知識者所熟知之方法與儀器來量測實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料的降伏強度。 First, the yield strength of the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 is measured by methods and instruments well known to those skilled in the art.

然後,分別將鋁合金材料放置於220℃之環境中,以進行烘烤製程。待進行烘烤製程後,以本發明所屬技術領域具有通常知識者所熟知之方法與儀器來量測烘烤後 之鋁合金材料的降伏強度,並計算烘烤前後,鋁合金材料之降伏強度的降幅。 Then, the aluminum alloy materials were placed in an environment of 220°C for the baking process. After the baking process is performed, the methods and instruments well-known to those skilled in the art of the present invention are used to measure the baking The yield strength of the aluminum alloy material, and calculate the reduction of the yield strength of the aluminum alloy material before and after baking.

6.耐壓性6. Pressure resistance

首先,分別對實施例1至實施例4與比較例1至比較例7所製得之鋁合金材料放置於220℃之環境中,以進行烘烤製程。然後,以本發明所屬技術領域具有通常知識者所熟知之方法與儀器來量測烘烤後之鋁合金材料的耐壓性。 First, the aluminum alloy materials prepared in Examples 1 to 4 and Comparative Examples 1 to 7 are placed in an environment of 220° C. to perform a baking process. Then, the pressure resistance of the baked aluminum alloy material is measured by methods and instruments well known to those of ordinary skill in the technical field to which the present invention belongs.

請參照第1表。於實施例1至實施例4中,由於所製得之鋁合金材料具有適當數量之釘紮顆粒(每立方微米之鋁合金材料具有30個至80個釘紮顆粒),故於進行烘烤製程時,此些釘紮顆粒可提供足夠之釘紮力,以限制次晶粒與差排之移動,而可抑制次晶粒之粗化與差排消散的程度,進而確保鋁合金材料於烘烤後仍具有良好之降伏強度,並降低鋁合金材料於烘烤後之降伏強度的降幅。據此,實施例1至實施例4所製得之鋁合金材料具有良好之烘烤強度。另外,由於烘烤後之鋁合金材料具有良好之降伏強度,故其亦具有良好之耐壓性。 Please refer to table 1. In Examples 1 to 4, since the prepared aluminum alloy material has an appropriate number of pinning particles (30 to 80 pinning particles per cubic micrometer of aluminum alloy material), the baking process is performed At this time, these pinning particles can provide sufficient pinning force to limit the movement of secondary grains and differential rows, and can inhibit the coarsening of secondary grains and the degree of differential row dissipation, thereby ensuring the baking of aluminum alloy materials It still has good yield strength, and reduces the drop of yield strength of aluminum alloy materials after baking. Accordingly, the aluminum alloy materials prepared in Examples 1 to 4 have good baking strength. In addition, since the baked aluminum alloy material has good yield strength, it also has good pressure resistance.

於比較例1中,由於第一冷卻步驟之時間過長,而使得冷卻速率過於緩慢,進而導致所析出之釘紮顆粒粗化,故於烘烤時,釘紮顆粒對於晶粒粗化之抑制效果與差排消散的限制效果係被減弱。據此,於烘烤製程後,比較例1所製得之鋁合金材料具有較大之強度降幅,而具有較差之降伏強度。於比較例2中,由於第二冷卻步驟之時間過長,而 使得第二冷卻步驟之冷卻速率過慢,而大幅增加析出物之析出量,進而、降低鋁合金材料中之固溶量,因此減少其中之強化相。據此,於烘烤製程後,所製得之鋁合金材料具有較差之烘烤強度,且此鋁合金材料具有較差之突耳率,而降低鋁合金材料之成品性質。 In Comparative Example 1, because the time of the first cooling step is too long, the cooling rate is too slow, which leads to coarsening of the pinned particles precipitated, so during baking, the pinning particles inhibit the grain coarsening The effect and the limiting effect of the dissipation of the difference are reduced. According to this, after the baking process, the aluminum alloy material prepared in Comparative Example 1 has a larger strength drop and has a lower yield strength. In Comparative Example 2, since the time of the second cooling step is too long, and The cooling rate of the second cooling step is too slow, and the precipitation amount of the precipitates is greatly increased, thereby further reducing the amount of solid solution in the aluminum alloy material, and thus reducing the strengthening phase therein. Accordingly, after the baking process, the manufactured aluminum alloy material has poor baking strength, and the aluminum alloy material has poor lug ratio, which reduces the finished properties of the aluminum alloy material.

顯然,本發明之鋁合金材料藉由多段冷卻來調控釘紮顆粒之析出數量與尺寸,藉以提升其所提供之釘紮力,而可提升所製得鋁合金材料的烘烤強度與耐壓性,進而滿足後端應用之需求。 Obviously, the aluminum alloy material of the present invention controls the precipitation amount and size of the pinning particles through multiple stages of cooling, so as to increase the pinning force provided by it, and can improve the baking strength and pressure resistance of the aluminum alloy material produced. To meet the needs of back-end applications.

於比較例3至比較例5中,由於熱軋製程之停留時間被延長(即比較例3),故鋁合金材料中之析出物於此階段大幅析出,而降低鋁合金材料之固溶量,進而降低烘烤後之降伏強度與耐壓性。其次,過低之完軋盤捲溫度與過快之冷卻速率均減少鋁合金材料中之固溶量,而降低鋁合金材料之烘烤強度與耐壓性。 In Comparative Examples 3 to 5, since the residence time of the hot rolling process is extended (ie Comparative Example 3), the precipitates in the aluminum alloy material are greatly precipitated at this stage, and the solid solution amount of the aluminum alloy material is reduced, Furthermore, the yield strength and pressure resistance after baking are reduced. Secondly, too low the temperature of the finished coil and too fast cooling rate both reduce the amount of solid solution in the aluminum alloy material, and reduce the baking strength and pressure resistance of the aluminum alloy material.

據此,本發明之鋁合金材料的製作方法藉由適當之熱軋製程,而可調整所製得之熱軋鋁捲的固溶量,進而有效補強鋁合金材料,故本發明之鋁合金材料可具有良好之烘烤強度與耐壓性。 According to this, the method for manufacturing the aluminum alloy material of the present invention can adjust the solid solution amount of the hot rolled aluminum coil produced by an appropriate hot rolling process, and thus effectively reinforce the aluminum alloy material, so the aluminum alloy material of the present invention Can have good baking strength and pressure resistance.

另外,於比較例6中,鋁胚含有過少之銅與鋅,而降低所製得鋁合金材料之耐壓性,故無法滿足後端應用之需求。於比較例7中,由於鋁合金材料係以特定設備製作,故其設備成本較高昂。再者,由於比較例7之鋁合金材料於緩冷至設定溫度(480℃至520℃)後,即直接進行熱軋製 程,故比較例7之鋁合金材料缺乏本發明前述之第二冷卻步驟。因此,比較例7之鋁合金材料具有過多之析出顆粒,而具有較高之強度降幅,故具有較差之耐壓性。 In addition, in Comparative Example 6, the aluminum blank contains too little copper and zinc, which reduces the pressure resistance of the aluminum alloy material produced, so it cannot meet the needs of back-end applications. In Comparative Example 7, since the aluminum alloy material is manufactured with specific equipment, the equipment cost is relatively high. Furthermore, since the aluminum alloy material of Comparative Example 7 is slowly cooled to the set temperature (480°C to 520°C), it is directly hot rolled Therefore, the aluminum alloy material of Comparative Example 7 lacks the aforementioned second cooling step of the present invention. Therefore, the aluminum alloy material of Comparative Example 7 has too many precipitated particles and has a higher strength drop, so it has poorer pressure resistance.

依據前述之說明可知,本發明之鋁合金材料的製作方法藉由均質化製程、分段冷卻與具有特定參數之熱軋製程,調整鋁合金材料中所析出之釘紮顆粒的數量與尺寸,而可提供適當之釘紮力,進而提升鋁合金材料之烘烤強度與耐壓性。 According to the foregoing description, it can be seen that the manufacturing method of the aluminum alloy material of the present invention adjusts the number and size of the pinned particles precipitated in the aluminum alloy material through a homogenization process, a staged cooling and a hot rolling process with specific parameters, and It can provide proper pinning force, thereby improving the baking strength and pressure resistance of aluminum alloy materials.

雖然本發明已以實施方式揭露如上,然其並非用以限定本發明,在本發明所屬技術領域中任何具有通常知識者,在不脫離本發明之精神和範圍內,當可作各種之更動與潤飾,因此本發明之保護範圍當視後附之申請專利範圍所界定者為準。 Although the present invention has been disclosed as above in the embodiments, it is not intended to limit the present invention. Anyone with ordinary knowledge in the technical field to which the present invention belongs can make various modifications and changes without departing from the spirit and scope of the present invention. Retouching, therefore, the protection scope of the present invention shall be subject to the scope defined in the appended patent application.

Figure 108119370-A0101-12-0015-1
Figure 108119370-A0101-12-0015-1

100‧‧‧方法 100‧‧‧Method

110/120/131/133/135/140/150/160‧‧‧操作 110/120/131/133/135/140/150/160‧‧‧Operation

130‧‧‧冷卻製程 130‧‧‧cooling process

Claims (10)

一種鋁合金材料的製作方法,包含:提供一鋁胚,其中該鋁胚之材料為3000系鋁合金;對該鋁合金胚料進行一均質化製程,以製得一均質化鋁胚,其中該均質化製程之一溫度不小於615℃;對該均質化鋁胚進行一冷卻製程,以製得一冷卻鋁胚,其中該冷卻製程包含:進行一第一冷卻步驟,其中該第一冷卻步驟係於2小時至6小時內將該均質化鋁胚由該均質化製程之該溫度冷卻至520℃;進行一第二冷卻步驟,其中該第二冷卻步驟係於3小時內由520℃冷卻至350℃;以及進行一第三冷卻步驟,其中該第三冷卻步驟係由350℃水淬至室溫;對該冷卻鋁胚進行一熱軋製程,以製得一熱軋鋁捲;以及對該熱軋鋁捲進行一冷軋製程,即可製得該鋁合金材料。 An aluminum alloy material manufacturing method includes: providing an aluminum embryo, wherein the material of the aluminum embryo is 3000 series aluminum alloy; performing a homogenization process on the aluminum alloy blank to obtain a homogenized aluminum embryo, wherein the One of the temperatures of the homogenization process is not less than 615°C; a cooling process is performed on the homogenized aluminum embryo to obtain a cooled aluminum embryo, wherein the cooling process includes: performing a first cooling step, wherein the first cooling step is Cooling the homogenized aluminum blank from the temperature of the homogenization process to 520°C within 2 hours to 6 hours; performing a second cooling step, wherein the second cooling step is cooling from 520°C to 350 within 3 hours ℃; and a third cooling step, wherein the third cooling step is quenched from 350 ℃ water to room temperature; a hot rolling process is performed on the cooled aluminum blank to produce a hot rolled aluminum coil; and the hot The aluminum alloy material can be prepared by rolling an aluminum coil through a cold rolling process. 如申請專利範圍第1項所述之鋁合金材料的製作方法,其中該鋁胚包含大於0.2重量百分比之銅與大於0.2重量百分比之鋅。 The method for manufacturing an aluminum alloy material as described in item 1 of the patent application scope, wherein the aluminum blank contains greater than 0.2 weight percent copper and greater than 0.2 weight percent zinc. 如申請專利範圍第1項所述之鋁合金材料的製作方法,其中該均質化製程之該溫度小於該鋁胚之一熔點。 The method for manufacturing an aluminum alloy material as described in item 1 of the patent application range, wherein the temperature of the homogenization process is less than one melting point of the aluminum embryo. 如申請專利範圍第3項所述之鋁合金材料的製作方法,其中該均質化製程至少進行12小時。 The method for manufacturing an aluminum alloy material as described in item 3 of the patent application scope, wherein the homogenization process is performed for at least 12 hours. 如申請專利範圍第1項所述之鋁合金材料的製作方法,其中該熱軋製程包含一熱粗軋步驟與一熱精軋步驟,且該熱粗軋步驟與該熱精軋步驟之一間隔時間不大於360秒。 The method for manufacturing an aluminum alloy material as described in item 1 of the patent scope, wherein the hot rolling process includes a hot rough rolling step and a hot finish rolling step, and the hot rough rolling step is separated from the hot finish rolling step by one The time is not greater than 360 seconds. 如申請專利範圍第1項所述之鋁合金材料的製作方法,其中該熱軋製程之一完軋盤捲溫度大於350℃。 The method for manufacturing an aluminum alloy material as described in item 1 of the patent application scope, wherein the temperature of one of the finished coils in the hot rolling process is greater than 350°C. 如申請專利範圍第6項所述之鋁合金材料的製作方法,其中該熱軋鋁捲之一冷卻速率每分鐘不大於1℃。 The method for manufacturing an aluminum alloy material as described in item 6 of the patent application range, wherein the cooling rate of one of the hot-rolled aluminum coils is not more than 1°C per minute. 如申請專利範圍第1項所述之鋁合金材料的製作方法,於進行該冷軋製程前,該製作方法不進行中間退火製程。 For the manufacturing method of the aluminum alloy material as described in item 1 of the patent application scope, before the cold rolling process, the manufacturing method does not perform the intermediate annealing process. 一種鋁合金材料,係藉由如申請專利範圍第1至8項中之任一項所述之製作方法所製得,其中該鋁合金材料於每立方微米(μm3)之單位體積含有30至80個釘紮顆粒,且每一該些釘紮顆粒之粒徑小於1μm。 An aluminum alloy material produced by the manufacturing method as described in any one of claims 1 to 8, wherein the aluminum alloy material contains 30 to 30 micrometers per cubic micrometer (μm 3 ) 80 pinned particles, and the particle size of each pinned particle is less than 1 μm. 如申請專利範圍第9項所述之鋁合金材料,其中經220℃之一烘烤製程後,該鋁合金材料之一降伏強度係大於260MPa,且該降伏強度的降幅不大於20MPa。 The aluminum alloy material as described in item 9 of the patent application scope, wherein after a baking process at 220°C, one of the aluminum alloy materials has a yield strength greater than 260 MPa, and the reduction in yield strength is not greater than 20 MPa.
TW108119370A 2019-06-04 2019-06-04 Aluminum alloy material and method for producing the same TWI692531B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW108119370A TWI692531B (en) 2019-06-04 2019-06-04 Aluminum alloy material and method for producing the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW108119370A TWI692531B (en) 2019-06-04 2019-06-04 Aluminum alloy material and method for producing the same

Publications (2)

Publication Number Publication Date
TWI692531B true TWI692531B (en) 2020-05-01
TW202045743A TW202045743A (en) 2020-12-16

Family

ID=71895848

Family Applications (1)

Application Number Title Priority Date Filing Date
TW108119370A TWI692531B (en) 2019-06-04 2019-06-04 Aluminum alloy material and method for producing the same

Country Status (1)

Country Link
TW (1) TWI692531B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113201703A (en) * 2021-04-19 2021-08-03 龙口市丛林铝材有限公司 Aluminum alloy ingot casting homogenizing annealing stepped cooling process

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI752893B (en) * 2021-07-01 2022-01-11 中國鋼鐵股份有限公司 Method for fabricating aluminum alloy sheet with rapid heat treatment

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW201333228A (en) * 2012-02-15 2013-08-16 China Steel Corp Method of manufacturing high formability aluminum alloy

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW201333228A (en) * 2012-02-15 2013-08-16 China Steel Corp Method of manufacturing high formability aluminum alloy

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113201703A (en) * 2021-04-19 2021-08-03 龙口市丛林铝材有限公司 Aluminum alloy ingot casting homogenizing annealing stepped cooling process
CN113201703B (en) * 2021-04-19 2022-07-08 龙口市丛林铝材有限公司 Aluminum alloy ingot casting homogenizing annealing stepped cooling process

Also Published As

Publication number Publication date
TW202045743A (en) 2020-12-16

Similar Documents

Publication Publication Date Title
TWI692531B (en) Aluminum alloy material and method for producing the same
AU2017261184B2 (en) Aluminum alloys with enhanced formability and associated methods
CN105755333A (en) Preparation method of aluminum alloy plate for thin cover of zip-top can
CN111974919A (en) Forging method for improving anisotropy of 7XXX aluminum alloy forging
CN113881877A (en) Aluminum alloy strip and preparation method and application thereof
TWI674324B (en) Method for manufacturing aluminum-manganese alloy
CN107779705B (en) A kind of aluminium lithium alloy and milling method
TWI640639B (en) Dual phase steel and method of forming the same
JP3897926B2 (en) Method for producing aluminum alloy sheet with excellent formability
US4163665A (en) Aluminum alloy containing manganese and copper and products made therefrom
TWI683906B (en) Method of manufacturing medium carbon steel
TWI551702B (en) Aluminum-magnesium alloy plate and method of producing thereof
CN108838206B (en) Method for improving performance of aluminum stainless steel composite board and aluminum stainless steel composite board
TW202010851A (en) Aluminum magnesium alloy and method for producing the same
JPS61288056A (en) Manufacture of aluminum alloy sheet for deep drawing
CN114645209B (en) Steel plate for medium-high temperature pressure vessel and preparation method thereof
TWI683016B (en) Method for manufacturing aluminum alloy sheet
TW202016320A (en) Non-oriented electrical steel coil and method of forming the same
JPH10330897A (en) Production of aluminum base alloy sheet for deep drawing
JPS60145348A (en) High-strength thin al alloy plate having superior formability and corrosion resistance and its manufacture
JP2956038B2 (en) Al alloy plate for drawing cups excellent in suppressing distortion pattern and method for producing the same
TWI629118B (en) Method for manufacturing aluminum can sheet
TWI695895B (en) Method of fabricating aluminum-magnesium-silicon alloy sheet with high bendability
CN115740500B (en) Method for manufacturing high-strength titanium alloy containing easily segregated elements through 3D printing
CN114752874B (en) Multi-scale structure for synergistically optimizing strong plasticity of TA19 titanium alloy and preparation method thereof