Customization: | Available |
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Application: | Spaceflight |
Certification: | RoHS, ISO9001, JIS, EN |
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Alloy | Chemical composition/wt.% | Executive standard | |||||||
Al | Mn | Zn | Zr | Y | RE | Gd | Mg | ||
ZE61 | - | - | 5.5~6.5 | ≥0.3 | - | 1.5-2.5 | - | - | - |
MB22 | - | - | 1.2-1.6 | 0.45-0.8 | 2.9-3.5 | - | - | - | - |
MB25 | - | - | 5.5~6.5 | ≥0.45 | 0.7~1.7 | - | - | Margin | GJB 5154 |
MB26 | - | - | 5.5~6.5 | ≥0.3 | - | 0.6~1.4 | - | Margin | GJB 5154 |
AE80 | 7.5-8.5 | 0.1-0.4 | 0.2-0.8 | - | - | 0.2-0.5 | - | Margin | - |
WE43 | - | <0.03 | <0.2 | ≥0.4 | 3.7~4.3 | 2.4~4.4 | - | Margin | GB/T5153 |
WE54 | - | <0.03 | <0.06 | 0.4~1.0 | 4.7~5.5 | 3.4~5.4 | - | Margin | GB/T5153 |
VW63 | - | - | - | 0.3-1.0 | 2.5-3.7 | - | 5.0-6.4 | Margin | QJ 20708 |
VW94 | - | - | 0-2 | ≥0.4 | 3.0~7.0 | - | 7.0~12.0 | Margin | - |
Alloy |
Density/g•cm-3 | Test temperature /ºC |
Tensile strength Rm /MPa |
Yield Strength Rp0.2 /MPa |
Elongation after breaking A /% |
Elastic Modulus /GPa | Executive standard |
ZE61 | 1.84 | RT | 290-340 | 230-280 | 6-12 | About 45 | - |
MB22 |
1.79 |
RT | 245-275 | 155-220 | 7-10 | About 43 | - |
250 | 165-195 | 130-155 | 17-23 | - | |||
MB25 |
1.85 |
RT | 305-355 | 225-285 | 6-10 | About 44 | GJB 5154 |
150 | 185-205 | 135-155 | 35-45 | - | |||
200 | 105-155 | 90-105 | 40-60 | ||||
250 | 95-115 | 85-95 | 45-65 | ||||
MB26 |
1.84 |
RT | 325-345 | 240-280 | 6-10 | GJB 5154 |
|
250 | 100-125 | 80-100 | 20-45 | - | |||
AE80 |
1.82 |
RT | 340-370 | 250-270 | 6-10 | About 44 | - |
150 | 170-190 | 120-140 | 25-45 | - | - | ||
WE43 |
1.84 |
RT | 280-360 | 160-250 | 5-8 | About 44 | ASTM B80 ISO 3116 |
200 | 175-200 | 120-135 | 9-12 | - | |||
WE54 |
1.85 |
RT | 260-340 | 175-230 | 5-8 | About 45 | ASTM B80 ISO 3116 |
200 | 180-210 | 140-160 | 9-12 | - | |||
VW63 | 1.91 | RT | 230-340 | 170-260 | 5-12 | - | QJ 20708 |
VW94 |
1.95 |
RT | 290-400 | 180-270 | 4-7 | About 45 | - |
150 | 250-350 | 190-300 | 8-11 | - | |||
Note: The above properties without special instructions are the properties of rolled plates |
Alloy | Material type | Material characteristics and typical uses |
ZE61 | Plates, forgings,bar | Achieve high room temperature tensile strength and yield strength at a lower cost, and is suitable for occasions where there is an urgent need for weight reduction and higher strength requirements. |
MB22 | Plates | Mg-Y-Zn-Zr series of wrought magnesium alloys are mainly made into sheets, with good forming and welding properties, and no stress corrosion tendency. It is recommended to be used for short-term aerospace structural parts below 300ºC. |
MB25 | Forgings, bars | Plasticity, toughness and corrosion resistance are similar to those of MB15, with good cutting performance and poor welding performance. It can replace some medium-strength aluminum alloys for aircraft load-bearing components. |
MB26 | Plates, forgings,bar | This alloy replaces Y in MB25 with Y-rich mixed rare earths. The price is lower and the performance difference is not big. It can also be applied to aircraft parts. |
AE80 | Plates, forgings, bar | The alloy is improved based on AZ80M. By adding rare earth elements, the room temperature and high temperature properties of the alloy are improved, and it can be used to prepare aircraft engine parts. |
WE43 | Castings, plates | It has good tensile performance, creep resistance and fatigue resistance at room temperature and high temperature, and can be used in vibration, sand and dust, high temperature, etc. |
WE54 | Plates, forgings, Extrusion | Serve in a harsh environment. It can be applied to aircraft parts such as aircraft engine gearboxes and helicopter gearboxes. |
VW63 | Plates, forgings, Extrusion | Mg-Gd-Y is a heat-resistant magnesium alloy with good room temperature and high temperature performance, and has great application potential in aircraft. |
VW94 |
Plates, forgings, Extrusion | The high-strength heat-resistant magnesium rare earth alloy has a tensile strength of more than 200MPa at 300°C, and its heat resistance is far better than aviation aluminum alloy. It is mainly used in the aerospace and weaponry fields that have strong weight reduction requirements and must withstand changes in space temperature, including cockpit skeletons, nose covers, door frames, ribs, beams, missile pylons, missile cabins and other parts. |
Product type | Temper | Dimensions |
Plate (rolling) | F(R),O(M),H112(R),H18(Y),H24(Y2) | (≥0.4)×(≤1200)×L mm |
Plate (extruded) | F(R),T5(S) | (≤50)×(≤400)×L mm |
Bar (extruded) | H112(R),T5(S) | Ф≤200mm |
Forging | F(R),T5(S) | Customer request size |
Sand castings & precision castings | - | According to the technical requirements of the drawings |
Special size specifications can be customized according to customer needs |