Aluminum Tube

Send Message Request a Quote

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) (%)
Alloy	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
Alloy	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

Available Alloys and Major Alloying Element

Alloy	Major alloying element (mass fraction) (%)
Alloy	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

Scan QR to Read
Links：https://globefindpro.com/products/35771.html