High-Strength Aluminum-Lithium Alloy for Advanced Engineering

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Customization: Available
Application: 3c
Certification: RoHS, ISO9001, JIS, EN
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  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
  • High-Strength Aluminum-Lithium Alloy for Advanced Engineering
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Overview

Basic Info.

Technique
Hot Rolled
Grade
--
Temper
--
Surface Treatment
Mill Finish
Alloy
Alloy
Transport Package
Export Standard Wooden Pallet
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7606125900
Production Capacity
15000mt/Month

Product Description

High-strength aluminum-lithium alloy (fifth-generation aluminum alloy)

Aluminum-lithium alloys have excellent mechanical properties and processing properties, which can replace the current 2024, 2A12, 2A14, 7075, 7050, 7055 and other high-strength alloys. Under the premise of ensuring the same mechanical properties, the weight can be reduced by 5% to 20%, which is suitable for military use. The current urgent need for weight reduction in aircraft and civil electronic products has important economic and social benefits.

Aluminum-lithium alloy characteristics
1. The density is low, every time 1% of lithium is added, the density is reduced by 3%
2. High specific modulus, high specific strength, instead of conventional high-strength aluminum alloy, the modulus of elasticity is increased by 6%, and the stiffness is increased by 15%-20%
3. Excellent superplastic forming performance
4. Excellent corrosion resistance
5. Good casting, hot processing (rolling, forging, extrusion), welding
(Laser welding, friction stir welding), machining formability

Chemical composition of aluminum-lithium alloy

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

Aluminum-lithium alloy performance index

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 - -


Application characteristics of aluminum-lithium alloy materials
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.

Product supply specifications
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
Detailed Photos

 

High-Strength Aluminum-Lithium Alloy for Advanced EngineeringHigh-Strength Aluminum-Lithium Alloy for Advanced EngineeringHigh-Strength Aluminum-Lithium Alloy for Advanced EngineeringHigh-Strength Aluminum-Lithium Alloy for Advanced EngineeringHigh-Strength Aluminum-Lithium Alloy for Advanced EngineeringHigh-Strength Aluminum-Lithium Alloy for Advanced Engineering
 

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