Customization: | Available |
---|---|
Application: | 3c |
Certification: | RoHS, ISO9001, JIS, EN |
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Alloy |
Chemical composition/% | |||||||||||||
Cu |
Li |
Zn |
Mg |
Mn |
Zr |
Ti |
Ag |
Sc |
Fe |
Si |
Other | |||
Single | Merge | Al | ||||||||||||
5A90(1420) |
- |
1.9~2.3 |
- |
4.5~6.0 |
- |
0.08~0.15 |
0.10 |
- |
- |
0.20 |
0.15 |
0.05 |
0.15 |
Margin |
1421 |
- |
1.8~2.2 |
- |
4.5~5.3 |
- |
0.06~0.10 |
0.10 |
- |
0.15 |
0.200 |
0.2 |
0.05 |
0.15 |
Margin |
8090 | 1.0~1.6 | 2.2~2.7 | 0.25 | 0.6~1.3 | 0.10 | 0.04~0.16 | 0.10 | - | - | 0.2 | 0.3 | 0.05 | 0.15 | Margin |
2297 |
2.5~3.1 |
1.1~1.7 |
0.05 |
0.25 |
0.10~0.5 |
0.08~0.15 |
0.12 |
- |
- |
0.10 |
0.10 |
0.05 |
0.15 |
Margin |
2A97 |
3.65~3.96 |
1.35~1.55 |
0.4~0.6 |
0.35~0.55 |
0.2~0.4 |
0.1~0.2 |
0.02~0.06 |
0.01 |
- |
0.20 |
0.10 |
0.05 |
0.10 |
Margin |
2196 | 2.5-3.3 | 1.4-2.1 | 0.35 | 0.25-0.8 | 0.35 | 0.04-0.18 | 0.10 | 0.25-0.6 | - | 0.15 | 0.12 | 0.05 | 0.15 | Margin |
2195 |
3.7~4.3 |
0.8~1.2 |
0.25 |
0.25~0.8 |
0.25 |
0.08~0.16 |
0.10 |
0.25~0.6000 |
- |
0.12 |
0.15 |
0.05 |
0.15 |
Margin |
2198 |
2.9-3.5 |
0.8-1.1 |
0.35 |
0.25-0.8 |
0.5 |
0.04-0.18 |
0.10 |
0.10-0.50 |
- |
0.10 |
0.08 |
0.05 |
0.15 |
Margin |
2099 | 2.4-3.0 | 1.6-2.0 | 0.4-1.0 | 0.1-0.5 | 0.1-0.5 | 0.05-0.12 | 0.10 | 0.07 | 0.05 | 0.05 | 0.15 | Margin | ||
2055 |
3.20-4.20 |
1.0-1.30 |
0.30-0.70 |
0.20-0.60 |
0.10-0.50 |
0.05-0.15 |
0.10 |
0.20-0.7 |
- |
0.10 |
0.07 |
0.05 |
0.15 |
Margin |
2050 |
3.2-3.9 |
0.7-1.3 |
0.25 |
0.20-0.6 |
0.20-0.50 |
0.06-0.14 |
0.10 |
0.20-0.7 |
- |
0.10 |
0.08 |
0.05 |
0.15 |
Margin |
2060 | 3.4-4.5 | 0.6-0.9 | 0.30-0.50 | 0.6-1.1 | 0.10-0.500 | 0.05-0.15 | 0.10 | 0.05-0.50 | - | 0.07 | 0.07 | 0.05 | 0.15 | Margin |
2065 |
3.8-4.7 |
0.8-1.5 |
0.30 |
0.25-0.8 |
0.15-0.50 |
0.05-0.15 |
0.10 |
0.15-0.50 |
- |
0.10 |
0.10 |
0.05 |
0.15 |
Margin |
Alloy |
Density ρ/g cm-3 |
Temper |
Standard |
Tensile strengthRm/MPa |
Yield Strength Rpo2/MPa |
Elongation after breaking A/% | Fracture toughness KC/MPa | Elastic Modulus /GPa |
5A90 (1420) |
2.47 |
Forging T6 Vertical |
GJB8506-2015 |
≥405 | ≥205 | ≥7.0 | 25 |
73.8 |
Sheet T6 Horizontal |
GJB8504-2015 |
≥410 | ≥255 | ≥8.0 | ||||
8090 | 2.55 | T8 | Q/QYHJ-A-8090-2018 | ≥460 | ≥380 | ≥4 | 26 | 77.0 |
2196 | 2.63 | T8 | Q/QYHJ-A-2196-2018 | ≥520 | ≥470 | ≥6 | - | 76.5 |
2297 | 2.65 | T8 | Q/QYHJ-A-2297-2018 | ≥440 | ≥400 | ≥10 | 30 | 77.3 |
2A97 | 2.70 | T8 | Q/QYHJ-A-2A97-2018 | ≥510 | ≥450 | ≥8 | 27 | 75.0 |
2195 |
2.72 |
T8 | Q/QYHJ-A-2195-2018 |
≥560 | ≥500 | ≥6 | 31 | 76.0 |
O | <200 | <150 | >15 | |||||
2198 | 2.7 | T8 | Q/QYHJ-A-2198-2018 | ≥450 | ≥400 | ≥4 | - | 76.5 |
2099 | 2.63 | T8 | Q/QYHJ-A-2099-2018 | 520 | 470 | 9 | 30 | 78 |
2050 | 2.70 | T8 | Q/QYHJ-A-2050-2018 | ≥490 | ≥455 | ≥6.0 | - | 76.5 |
2065 | 2.7 | T8 | Q/QYHJ-A-2065-2018 | ≥580 | ≥550 | ≥6.0 | - | - |
Cast aluminum lithium alloy |
2.55 | T6 | - | ≥400 | ≥300 | ≥6 | - | - |
5A90 (1420) | Thick plates, thin plates,profiles, forgings |
It is a medium-strength, weldable, low-density, high-modulus, high-corrosion-resistant aluminum-lithium alloy, used to manufacture aerospace structural parts, etc., with obvious weight reduction effects. |
8090 |
Thick plates,thin plates,profiles, forgings |
It can replace aluminum alloys such as 2014, 2024, 7010, 7075, and is widely used in floor mountings, brackets, stiffeners, frames, spars, stringers, longitudinal beams, ribs, partitions, and tail spine skins; flight control systems And avionics floor structure, nose, cabin top frame; flight control structure, skin siding (lower fuselage), cabin top frame, flat cover; brackets, door rails, seat rails, etc. |
2297 |
Thick plates |
Compared with 2124-T851 alloy, it has higher fatigue damage resistance, and its fatigue life is 3-5 times higher than other aviation aluminum alloys. Compared with other conventional alloys, while the strength is improved, the density is reduced by 5% and the elastic modulus is increased by 8%. Mainly used for aircraft fuselage frames, wing spars, bulkhead partitions, etc. |
2A97 |
Thin plate, thick plate |
It is a new research material of aluminum-lithium alloy with completely independent intellectual property rights in my country, which is stronger than the 7050-T7451 thick plate.The toughness is equivalent, the density is 5% lower, and the modulus of elasticity is 7% higher. It can replace 7050 for the manufacture of aircraft main bearing structural parts, and the weight reduction effect is outstanding. |
2195 |
Thick plates,thin plates,profiles, forgings |
Weldable aluminum-lithium alloy with high strength and high modulus of elasticity has excellent low temperature performance. The density of the alloy is 5% lighter than that of 2219 alloy, and its strength is 30% higher than the latter. It can replace 2219 alloy for aerospace cryogenic storage tank materials , Obvious weight loss effect has been achieved. |
Cast aluminum-lithium alloy | Metal and membrane shell precision castings | As an alloy with low density, high elastic modulus, high specific strength and high specific rigidity, and good fluidity, cast aluminum-lithium alloy has very broad application prospects in the aerospace field where weight reduction is urgent. Mainly used in missile compartments, missile barrels, fairings, inlet lip, hatch, fuel tank, precision instrument shells, instrument mounting frames, structural cabins with complex shapes, etc. |
Alloy | Dimensions | |
Size |
Round ingot slab ingot | Ф100×240mm,Ф240×400mm,Ф400×800mm,800×600×200mm,300×700×950mm , and other customized specifications |
Extruded sheet | 60×5mm,80×7mm,105×4mm,220×26mm,250×40mm, and other customized specifications | |
Extrude rod | Φ9.5mm,Φ12mm,Φ22mm,Φ30mm,Φ60mm,Φ100mm, and other customized specifications | |
Forged plate | 100×600×1500mm,120×600×1200mm,150×600×1000mm, and other customized specifications | |
Forged rod | Ф30mm-Ф400mm | |
Plate | Plate(0.5-50mm)Thick×1200mm Wide×4000mm Long | |
Casting | Metal and membrane shell precision-cast parts with a single weight of 0.2kg~150kg |