Customization: | Available |
---|---|
Application: | Transportation Tools, Spaceflight |
Certification: | RoHS, ISO9001, JIS, EN |
Still deciding? Get samples of US$ 0/Piece
Request Sample
|
Suppliers with verified business licenses
Audited by an independent third-party inspection agency
Alloy |
Chemical composition (mass fraction)/% | |||||||||
Al | Mn | Zn | Zr | RE | Cu | Fe | Ni | Si | Mg | |
ZK61M (MB15) |
≤0.05 |
≤0.10 |
5.0-6.0 |
0.30-0.90 |
- |
≤0.05 |
≤0.05 |
≤0.05 |
≤0.05 |
Margin |
AZ31B | 2.5-3.5 | 0.20-1.0 | 0.60-1.40 | - | - | ≤0.01 | ≤0.005 | ≤0.001 | ≤0.08 | Margin |
AZ40M (MB2) |
3.0-4.0 |
0.15-0.5 |
0.20-0.80 |
- |
- |
≤0.05 |
≤0.05 |
≤0.005 |
≤0.10 |
Margin |
ME20M (MB8) |
≤0.20 |
1.3-2.2 |
≤0.3 |
- |
0.15-0.35 |
≤0.05 |
≤0.05 |
≤0.01 |
≤0.15 |
Margin |
AZ80M | 7.8-9.2 | 0.15-0.50 | 0.20-0.8 | - | - | ≤0.05 | ≤0.05 | ≤0.005 | ≤0.10 | Margin |
Alloy |
Temper |
Plate thick/mm |
Tensile strength Rm/MPa | Yield Strength Rp0.2/MPa |
Elongation after breaking A/% |
Remark |
ZK61M (MB15) |
H112 |
8.00~12.50 | ≥290 | ≥190 | ≥12.0 | Finished product flaw detection reaches GJB1580A- in 2004 Class A standard |
>12.50~20.00 | ≥285 | ≥190 | ≥12.0 | |||
>20.00~32.00 | ≥280 | ≥185 | ≥10.0 | |||
>32.00~70.00 | ≥275 | ≥180 | ≥10.0 | |||
T5 |
8.00~12.50 | ≥295 | ≥200 | ≥8.0 | ||
>12.50~20.00 | ≥290 | ≥195 | ≥8.0 | |||
>20.00~32.00 | ≥285 | ≥195 | ≥7.0 | |||
>32.00~70.00 | ≥280 | ≥195 | ≥7.0 | |||
AZ31B |
O |
0.4~3.0 | ≥240 | ≥150 | ≥12.0 | Finished product flaw detection reaches GJB1580A- in 2004 Class A standard |
>3.0~12.5 | ≥230 | ≥140 | ≥12.0 | |||
>12.5~70 | ≥230 | ≥140 | ≥10.0 | |||
H24 |
0.4~8.0 | ≥270 | ≥200 | ≥6.0 | ||
>8.0~12.5 | ≥255 | ≥165 | ≥8.0 | |||
>12.5~20 | ≥250 | ≥150 | ≥8.0 | |||
>20~70 | ≥235 | ≥125 | ≥8.0 | |||
H26 |
8~10 | ≥270 | ≥186 | ≥6.0 | ||
>10~12.5 | ≥265 | ≥180 | ≥6.0 | |||
>12.5~25 | ≥255 | ≥160 | ≥6.0 | |||
>25~50 | ≥240 | ≥150 | ≥5.0 | |||
H112 |
8~12.5 | ≥230 | ≥140 | ≥10.0 | ||
>12.5~20 | ≥230 | ≥140 | ≥8.0 |
>20~32 | ≥230 | ≥140 | ≥8.0 | |||
>32~70 | ≥230 | ≥130 | ≥8.0 | |||
AZ40M |
O |
0.8~3.0 | ≥240 | ≥130 | ≥12.0 | Finished product flaw detection reaches GJB1580A- in 2004 Class A standard |
>3.0~10.0 | ≥230 | ≥120 | ≥12.0 | |||
H112 |
8~12.5 | ≥230 | ≥140 | ≥10.0 | ||
>12.5~20.0 | ≥230 | ≥140 | ≥8.0 | |||
>20.0~70.0 | ≥230 | ≥140 | ≥8.0 | |||
ME20M |
H18 | 0.40~0.80 | 260 | - | ≥2.0 | Finished product flaw detection reaches GJB1580A- in 2004 Class A standard |
H24 |
>0.80~3.00 | 250 | ≥160 | ≥8.0 | ||
>3.00~5.00 | 240 | ≥140 | ≥7.0 | |||
>5.00~10.00 | 240 | ≥140 | ≥6.0 | |||
O |
0.40~3.00 | 230 | ≥120 | ≥12.0 | ||
>3.00~10.00 | 220 | ≥110 | ≥10.0 | |||
H112 |
8.00~12.50 | 220 | ≥110 | ≥10.0 | ||
>12.50~20.00 | 210 | ≥110 | ≥10.0 | |||
>20.00~32.00 | 210 | ≥110 | ≥7.0 | |||
>32.00~70.00 | 200 | ≥90 | ≥6.0 | |||
AZ80M |
H112 | 25-40 |
≥280 | ≥175 | ≥10.0 | |
T5 | ≥340 | ≥210 | ≥5.0 |
Alloy | Material type | Material characteristics and typical uses |
ZK61M |
Plates,bars,forgings |
ZK61M magnesium alloy belongs to the Mg-Zn-Zr series of magnesium alloys. It has the advantages of high specific strength, easy cutting, good vibration damping, and good electromagnetic shielding. It is now mainly used in the aviation industry to manufacture parts with heavy loads. , Such as wings, stringers, wing ribs and rocker arms, etc., With the breakthrough in the production technology of large-scale rolled plate products, the application prospect of this brand of magnesium alloy products is very broad. |
AZ31B |
Plates, bars, forgings |
AZ31B alloy belongs to Mg-Al-Zn series magnesium alloy, which is not strengthened by heat treatment.It has the characteristics of moderate strength, good welding performance and good machining performance. It is the most widely used magnesium alloy grade. After surface treatment, it can be used to manufacture aerospace components that can withstand medium loads and use at room temperature, as well as high-speed rail The structure of seat brackets, notebook or mobile phone shells in the fields of aerospace, transportation, electronic communications, etc. There are many applications in terms of software. |
AZ40M |
Plates, bars, forgings |
AZ40M alloy belongs to the magnesium-aluminum-zinc series non-heat-treatable deformed magnesium alloy. The alloy has poor process plasticity at room temperature and good plasticity at high temperature, so the pressure processing process of the alloy must be carried out under heating. The alloy has good cutting performance and welding performance, and has a low stress corrosion tendency, but it has better performance. The alloy can be processed into plates, bars, profiles and forgings and die forgings with complex shapes, and the manufactured parts can work for a long time below 150°C. |
ME20M |
Plates, bars, forgings |
ME20M alloy belongs to the Mg-Mn series magnesium alloy. Its corrosion resistance is the best among magnesium alloys. It has good welding performance and cutting performance. It is a heat-treated non-reinforceable alloy with moderate strength. It is often used for manufacturing and has little bearing capacity, but it requires Parts with good weldability and corrosion resistance, sheet products are often used in the manufacture of aircraft skins, siding and internal parts. |
AZ80M |
Plates, bars, forgings |
AZ80M alloy belongs to the magnesium-aluminum-zinc series magnesium alloy, which is not heat-strengthened alloy. High specific strength, large elastic modulus, good shock absorption, greater impact load capacity than aluminum alloy, and good resistance to organics and alkali corrosion. AZ80M magnesium board is mainly used in transportation applications, such as automobiles, trains, ships, etc. |
Product type | Temper | Dimensions |
Plate and strip | F,O,H112,H18,H24 | (0.4~70)×≤1200× ≤3000mm |
Forging | F,T5 | customer needs |
Extruded bar | T5 | customer needs |