Aluminum Tube
Metal Tube for Aircraft, Aluminum Alloy for Space Craft, Metal Tube for Fuel Tank, Aluminum Machining Plant
We produce Aluminum tube according to the alloy type, specification, heat treatment condition, and other details clients have provided. Please contact to tell us your requirements.
For commonly used Aluminum and Aluminum alloy please click here:
Processing Equipment & Specification| Equipment | Products | Outer diameter | Inner diameter |
| 100MN double-action direct extruder | seamless pipe | 225-507mm | 195-435mm |
| 55MN double-action indirect extruder | seamless pipe | 70-265mm | 50-254mm |
| 28MN double-action indirect extruder | seamless pipe | 70-137mm | 35-125 |
| 1880UST double-action direct extruder | seamless pipe | 28-88mm | 14-78mm |
| 1100UST double-action direct extruder | seamless pipe | 25-64mm | 3-55mm |
Recommended Alloy & Applications
2024: for aircraft frame, rivet, missile components, truck wheel hub, propeller components, aircraft skin, construction and transport structures, and other structural elements
| Alloy | Major alloying element (mass fraction) (%) | ||||||||
| Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Al | |
| 2024 | 0.5 | 0.5 | 3.8~4.9 | 0.3~0.9 | 1.2~1.8 | 0.1 | 0.25 | 0.15 | the rest part |
| Alloy | Mechanical and physical properties | ||||
| tensile strength (25°C) (MPa) | yield strength (25°c) (MPa) | hardness 500kg 10mm | elongation 1.6mm(1/16in) thickness | max shear stress (MPa) | |
| 2024-T351 | 470 | 325 | 120 | 10 | 285 |
| weldability | machinability | corrosion resistance | electricity conductivity 20℃(68℉) (％IACS) | density (20℃) (g/cm3) | |
| limited | great | poor | 30～40 | 2.78 | |
2014: for occasions with high strength and hardness (high temperature) requirements, like aircraft, forgings, thick metal plates and extruded materials, wheels and structural elements, the first fuel tank of multistage rocket, truck frame, suspension parts
2219: oxidizer tank in space racket, supersonic aircraft skin and structural elements. 2210 shows good welding performance and high fracture toughness. Under T8 state, its resistance to stress corrosion cracking is perfect. Working temperature: -270~300℃
2618: for die forgings and free forgings, piston and aero engine parts
2A50: for complex shaped medium-strength spare parts
2A70F: aircraft skin, aircraft engine, pistons, guide wheels, roulette
| Alloy | Major alloying element (mass fraction) (%) | ||||||||
| Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Al | |
| 2024 | 0.5 | 0.5 | 3.8~4.9 | 0.3~0.9 | 1.2~1.8 | 0.1 | 0.25 | 0.15 | the rest part |
| 2014 | 0.5~1.2 | 0.7 | 3.9~5.0 | 0.4~1.2 | 0.2~0.8 | 0.1 | 0.25 | 0.15 | the rest part |
| 2219 | 0.2 | 0.3 | 5.8~6.8 | 0.2~0.4 | 0.2 | --- | 0.1 | 0.1~0.25 | the rest part |
| 2618 | 0.1~0.25 | 0.9~1.3 | 1.9~2.7 | --- | 1.3~1.8 | --- | 0.1 | 0.04~0.1 | the rest part |
| 2A50 | 0.7~1.2 | 0.7 | 1.8~2.6 | 0.4~0.8 | 0.4~0.8 | --- | 0.3 | 0.15 | the rest part |
| 2A70 | 0.35 | 0.9~1.5 | 1.9~2.5 | 0.2 | 1.4~1.8 | --- | 0.3 | 0.02~0.1 | the rest part |
| 2011 | 0.4 | 0.7 | 5.0~6.0 | --- | --- | --- | 0.3 | --- | the rest part |
| 2017 | 0.2~0.8 | 0.7 | 3.5~4.5 | 0.4~0.1 | 0.4~0.8 | 0.1 | 0.25 | 0.15 | the rest part |
| 2036 | 0.5 | 0.5 | 2.2~3.0 | 0.1~0.4 | 0.3~0.6 | 0.1 | 0.25 | 0.15 | the rest part |
| 2124 | 0.2 | 0.3 | 3.8~4.9 | 0.3~0.9 | 1.2~1.8 | 0.1 | 0.25 | 0.15 | the rest part |
| 2218 | 0.9 | 1 | 3.5~4.5 | 0.2 | 1.2~1.8 | 0.1 | 0.25 | --- | the rest part |
| 2319 | 0.2 | 0.3 | 5.8~6.8 | 0.2~0.4 | 0.02 | --- | 0.1 | 0.1~0.2 | the rest part |
| 2A01 | 0.5 | 0.5 | 2.2~3.0 | 0.2 | 0.2~0.5 | --- | 0.1 | 0.15 | the rest part |
| 2A02 | 0.3 | 0.3 | 2.3~3.2 | 0.45~0.7 | 2~2.4 | --- | 0.1 | 0.15 | the rest part |
| 2A06 | 0.5 | 0.5 | 3.8~4.3 | 0.5~1.0 | 1.7~2.3 | --- | 0.1 | 0.03~0.15 | the rest part |
| 2A10 | 0.25 | 0.2 | 3.9~4.5 | 0.3~0.5 | 0.15~0.3 | --- | 0.1 | 0.15 | the rest part |
| 2A11 | 0.7 | 0.7 | 3.8~4.8 | 0.4~0.8 | 0.4~0.8 | --- | 0.3 | 0.15 | the rest part |
| 2A14 | 0.6~1.2 | 0.7 | 3.9~4.8 | 0.4~1.0 | 0.4~0.8 | --- | 0.3 | 0.15 | the rest part |
| 2A16 | 0.3 | 0.3 | 6.0~7.0 | 0.4~0.8 | 0.05 | --- | 0.1 | 0.1~0.2 | the rest part |
| 2A17 | 0.3 | 0.3 | 6.0~7.0 | 0.4~0.8 | 0.25~0.45 | --- | 0.1 | 0.1~0.2 | the rest part |
| 2A80 | 0.5~1.2 | 1.0~1.6 | 1.9~2.5 | 0.2 | 1.4~1.8 | --- | 0.3 | 0.15 | the rest part |
| 2A90 | 0.5~1.0 | 0.5~1.0 | 3.5~4.5 | 0.2 | 0.4~0.8 | --- | 0.3 | 0.15 | the rest part |
