ASTM B209 Aluminum and Aluminum-Alloy Sheet and Plate
Grade:1060、1100、1230、2014、2024、2124、2219、3003、3004、3005、3105、5005、5005、5010、5050,5052, 5059,5083,5086,5154,5252,5254,5454,5456,5457,5657,5754,6003,6013,6061,7072,7075
Condition:O, H12, H22, H14, H24, H16, H26, H18, H28, H112, F, H32, H34, H36, H38, H19, H25, H27, H111, H241, H25, T3, T4, T451, T42, T6, T62, T651, T351, T361, T72, T81, T851, T861, T87, T31, T37, T7351, T7651
Plate & Sheet Size:THK:0.15mm-500mm,宽度:100mm-200mm,腿:1000mm-9000mm
线圈尺寸:THK:0.05-15mm宽度:15-2000mm
1xxx系列
等级:1060, 1100, 1230
1XXX系列合金 - (万博体育全能版下载不加热 - 最终拉伸强度为10至27 ksi)该系列通常称为纯铝系列,因为它必须具有最小铝的99.0%。它们是可焊接的。但是,由于它们的熔化范围狭窄,因此需要某些考虑才能产生可接受的焊接程序。当考虑制造时,这些合金主要是用于其优质耐腐蚀性(例如在专用的化学罐和管道中)的万博体育全能版下载优质耐腐蚀性,或者是为了像在总线杆应用中一样出色的电导率。这些合金具有万博体育全能版下载相对较差的机械性能,对于一般结构应用,很少会考虑。这些基本合金通常用匹配万博体育全能版下载的填充材料或依赖于应用和性能要求的4xxx填充合金焊接。
2xxx系列
Grade:2014,2024,2124,2219
2XXX系列合金 - (万博体育全能版下载可热处理 - 终极拉伸强度为27至62 kSi)它们是铝 /铜合金(铜添加量为0.7至6.8%),是高强度,高强度,高性能合金,通常用于航空航天和航空航天和航空航天和高性能合金飞机应用。它们在广泛的温度范围内具有出色的强度。这些合金中的一些因电弧焊接过万博体育全能版下载程而被认为是不可划分的,因为它们对热开裂和应力腐蚀开裂的敏感性;但是,通过正确的焊接程序可以非常成功地焊接其他弧线。这些基本材料通常用高强度2XXX系列填充合金焊接旨在符合其性能,但有时可以用含有硅或硅和铜的4xxx系列填充剂焊接,取决于应用和服务要求。万博体育全能版下载
3xxx系列
等级:3003,3004,3005,3105
3xxx系列Alloys – (non-heat treatable – with ultimate tensile strength of 16 to 41 ksi) These are the aluminum / manganese alloys (manganese additions ranging from 0.05 to 1.8%) and are of moderate strength, have good corrosion resistance, good formability and are suited for use at elevated temperatures. One of their first uses was pots and pans, and they are the major component today for heat exchangers in vehicles and power plants. Their moderate strength, however, often precludes their consideration for structural applications. These base alloys are welded with 1xxx, 4xxx and 5xxx series filler alloys, dependent on their specific chemistry and particular application and service requirements.
5xxx系列
Grade:5005、5010、5050,5052, 5059,5083,5086,5154,5252,5254,5454,5456,5457,5657,5754
5xxx系列Alloys – (non-heat treatable – with ultimate tensile strength of 18 to 51 ksi) These are the aluminum / magnesium alloys (magnesium additions ranging from 0.2 to 6.2%) and have the highest strength of the non-heat treatable alloys. In addition, this alloy series is readily weldable, and for these reasons they are used for a wide variety of applications such as shipbuilding, transportation, pressure vessels, bridges and buildings. The magnesium base alloys are often welded with filler alloys, which are selected after consideration of the magnesium content of the base material, and the application and service conditions of the welded component. Alloys in this series with more than 3.0% magnesium are not recommended for elevated temperature service above 150 deg F because of their potential for sensitization and subsequent susceptibility to stress corrosion cracking. Base alloys with less than approximately 2.5% magnesium are often welded successfully with the 5xxx or 4xxx series filler alloys. The base alloy 5052 is generally recognized as the maximum magnesium content base alloy that can be welded with a 4xxx series filler alloy. Because of problems associated with eutectic melting and associated poor as-welded mechanical properties, it is not recommended to weld material in this alloy series, which contain higher amounts of magnesium with the 4xxx series fillers. The higher magnesium base materials are only welded with 5xxx filler alloys, which generally match the base alloy composition.
6xxx系列
等级:6003,6013,6061
6 xxx系列合金(热处万博体育全能版下载理——天涯te tensile strength of 18 to 58 ksi) These are the aluminum / magnesium - silicon alloys (magnesium and silicon additions of around 1.0%) and are found widely throughout the welding fabrication industry, used predominantly in the form of extrusions, and incorporated in many structural components. The addition of magnesium and silicon to aluminum produces a compound of magnesium-silicide, which provides this material its ability to become solution heat treated for improved strength. These alloys are naturally solidification crack sensitive, and for this reason, they should not be arc welded autogenously (without filler material). The addition of adequate amounts of filler material during the arc welding process is essential in order to provide dilution of the base material, thereby preventing the hot cracking problem. They are welded with both 4xxx and 5xxx filler materials, dependent on the application and service requirements.
7xxx Series
Grade:7072,7075
7xxx系列合金 - (万博体育全能版下载可热处理 - 最终拉伸强度为32至88 ksi)这些是铝 /锌合金(锌添加范围为0.8至12.0%),并包含一些最高强度的铝合金。这些合金通常万博体育全能版下载用于飞机,航空航天和竞争性运动设备等高性能应用中。像2XXX系列合金一样,该系列融合了合金,这些合万博体育全能版下载金被认为是不适合用于电弧焊接的候选者,而其他合金通常是成功焊接的。本系列中常见的合金,例如7005,主要用万博体育全能版下载5xXX系列填充合金焊接。