2124 Aerospace Aluminum Sheet Plate
What is 2124 aluminum?
2124 aluminum is a high-strength aluminum alloy that belongs to the aluminum-copper alloy series, featuring good strength and corrosion resistance.
After heat treatment, 2124 alloy exhibits high strength and hardness, making it suitable for manufacturing aircraft structures, spacecraft components, and other applications that require high strength and low weight.
2124 aluminum alloy is a high-purity variant of 2024 alloy. This alloy is typically supplied in the T851 temper, exhibiting excellent strength retention and creep resistance at temperatures up to 350°F (approximately 177°C).
The fracture toughness of 2124-T851 aluminum plate is significantly higher than that of 2024-T851, making it suitable for applications that require higher short transverse ductility, high strength, and excellent machinability. This alloy also offers outstanding resistance to exfoliation corrosion, and its fatigue performance is similar to that of 2024-T851. It is widely used in high-performance structural components in the aerospace industry.
Characteristics of 2124 Aerospace Aluminum Plate
- High strength: Compared to other aluminum alloys, 2124 excels in strength, making it suitable for structures that bear significant loads.
- Good machinability: With appropriate heat treatment, 2124 aluminum has good machinability and can undergo various machining processes.
- Corrosion resistance: Although aluminum-copper alloys have relatively low corrosion resistance, proper surface treatments can enhance their corrosion performance.
- Heat treatment: 2124 aluminum typically requires heat treatment to achieve optimal performance, with common processes including quenching and aging.
Specification of 2124 aerospace grade aluminum plate
| Temper | O, H112, T3, T4, T6, T351, T851, etc. |
| Thickness | 0.5mm-300mm |
| Width | 500-2650mm |
| Length | 500-12000mm |
| Standard | GB/T3880, GJB1541, GJB2662, ASTMB209, EN485, QQ-A-250/29, AMS 4101, etc. |
Popular 2124 Aluminum
Aluminum Sheet Plate 2124 T851
2124 T851 alloy plate is commonly used in the manufacture of aircraft structures, particularly in parts requiring high strength and excellent machinability. These applications include wing spars, fuselage frames, landing gear structures, and more, and it is widely used in aerospace applications where high-temperature and fatigue resistance are essential.
Aircraft Structures AA2124 T351 Aluminum Plate
AA2124 alloy in the T351 temper has a high yield strength and good corrosion resistance, making it suitable for manufacturing structural components that need to withstand high pressure and stress. Compared to other common aluminum alloys, AA2124 T351 has better short transverse ductility, making it ideal for applications that require complex machining.
Chemical composition of 2124 aerospace grade aluminium plate
| Element | Composition(%) |
| Si | 0.2 |
| Fe | 0.3 |
| Cu | 3.8-4.9 |
| Mn | 0.3-0.9 |
| Mg | 1.2-1.8 |
| Cr | 0.10 |
| Zn | 0.25 |
| Ti | 0.15 |
| Other | 0.2 |
| Al | Remainder |
Advantages of 2124 Aluminum
- High strength-to-weight ratio
- Good machinability
- Excellent corrosion resistance
Limitations of 2124 Aluminum
- Relatively high cost
- Difficult to machine, especially after heat treatment
2124 Aluminum Typical Mechanical Properties
| Thickness | Tensile Strength | Yield Strength | Elongation |
| In. | KSI | KSI | % |
| 1.001-2.00 | 66 | 57 | 5 |
| 5.001-6.00 | 63 | 54 | 4 |
2124 Aluminum Physical properties
| Coefficient of thermal expansion from 20 to 100°C | 22.9 K⁻¹10⁻⁶ |
| Coefficient of thermal expansion from 20 to 200°C | 23.8 K⁻¹10⁻⁶ |
| Coefficient of thermal expansion from 20 to 300°C | 24.7 K⁻¹10⁻⁶ |
| Coefficient of thermal expansion from -50 to 20°C | 21.1 K⁻¹10⁻⁶ |
| Density | 2.78 g/cm³ |
| Modulus of elasticity | 73 GPa |
| Shear modulus | 27 GPa |
| Specific heat | 882 J/(kg·K) |
| Thermal conductivity max. | 190 W/m*K |
| Thermal conductivity min. | 150 W/m*K |
Applications of 2124 Aircraft Aluminum Plate
2124 aluminum plate is primarily used for aircraft structural components, wings, fuselage, and other load-bearing parts.
1. Aircraft Structural Components
2124 aluminum alloy is commonly used in the manufacturing of primary structural components for aircraft, such as frames, support beams, and other load-bearing structures. These parts need to withstand high loads and fatigue, making the strength and rigidity of 2124 aluminum alloy an ideal choice.
2. Wings
Wings are critical components of an aircraft, and 2124 aluminum alloy is often used in the primary load-bearing structures of wings, such as wing beams and ribs. Its high strength and fatigue resistance allow wings to effectively bear aerodynamic loads during flight.
3. Fuselage
In the design of aircraft fuselage, 2124 aluminum alloy is used to manufacture important load-bearing components, such as cross beams and longitudinal beams. These parts need to provide sufficient strength and stability to ensure the overall structural integrity of the aircraft.
4. Other Load-Bearing Components
In addition to wings and fuselage, 2124 aluminum alloy is also used in other load-bearing components, such as landing gear brackets, connectors, and other structural elements. These parts must withstand significant impacts and loads during flight and landing.
5. Military and Aerospace Applications
In military aviation and aerospace applications, 2124 aluminum alloy is widely used due to its excellent performance, particularly in components requiring high strength and low weight.
What is the difference between 2024 and 2124 aluminum?
2024 aluminum is commonly used in aircraft structural components, transport vehicles, and other applications requiring high strength.
2124 aluminum, with its superior high-temperature performance and corrosion resistance, is often used in high-performance components in the aerospace field, such as wing beams and fuselage structures.
Haomei Aluminum 2124 plate is available in the following sizes (all dimensions in inches)
Why choose Haomei 2124 aerospace grade aluminum plate?
Haomei Aluminum offers a wide range of aluminum aircraft sheet and plate products to meet various aerospace application needs. Our products include a variety of standards such as AMS 4041, AMS 4037, AMS 4035, AMS 4049, AMS 4050, AMS 4048, AMS 4045, AMS 4044, AMS 4027, AMS 4026, AMS 4025, AMS 4347, and AMS 4202. In addition, we supply high-performance aluminum alloys such as 2219, 2124, 7175, 7475, 2024-Hi-Form, 7075T73, and 7075T76 to meet the needs of customers in the aerospace and aviation industries.
| Grade | Temper | Surface | Specification |
| 2024 |
0, T3, T81, T351, T851 0, T3, T81, T351, T851 0, T3 |
BARE ALCLAD Clad 1 Side |
AMS-QQA250/4, AMS4035, AMS4037 AMS-QQA250/5, AMS4040, AMS4041, BMS7-305, AMS4036-AMS4077 |
| 2124 |
0, T3, T6, T351 T651 |
BARE ALCLAD |
AMS4029, AMS4028 AMS-QQA250/3 |
| 2219 |
0, T3, T81, T37 T87, T351, T851 |
BARE ALCLAD |
AMS-QQA250/30, AMS4031 AMS4095, AMS4096, AMS4094, DMS1719, BMS-7-110 |
| 2124 | T351, T851 | BARE | AMS-QQA250/29, GM2007, MMS-149, FMS-3002 |
| 6061 | 0, T6, T4, T651 | BARE | AMS-QQA250/11, AMS4025, AMS4026, AMS4027 |
| 6013 | T4 | BARE | AMS4347 |
| 7075 |
0, T6, T73, T76 T651, T7351 |
BARE ALCLAD |
AMS-QQA250/12, AMS-QQA250/24, AMS4044, AMS4045, AMS4078, AMS4315, MMS159 AMS-QQA250/13, AMS-QQA250/25, AMS4048, AMS4049, AMS4316, BMS7-302 |
| 7475 |
0, T6, T761, T7351 T7651 0, T61, T761 |
BARE BARE ALCLAD |
DMS2281, AMS4084, AMS4085, AMS4089, AMS4202F MS3004, CMS516-02 DMS2234, AMS4100, AMS4207 |
| 7050 | 0, T7451, T7651 | BARE | AMS4050, AMS4201, MMS1420, DMS2234, BMS7-323, CMS513-01/03 |
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