2A01 Aircraft Aerospace Aluminum Alloy

• Color: Silver
• Application: Transportation Tools, Door & Window, Decorations
• Certification: ISO9001, ASTM, JIS, GB, EN
• Technique: Extruded
• Grade: 2000 Series
• Temper: O - H112
• Model NO.: 2A01
• Surface Treatment: Powder Coating
• Alloy: Alloy
• Elongation: More Than 10%
• Transport Package: Export Standard Wooden Pallet
• Specification: According to Customer Requirement
• Trademark: Chalco Aluminum
• Origin: Henan China
• HS Code: 7606125900
• Production Capacity: 20000mt/Month

Product Description

2A01 aircraft aerospace aluminum alloy
 

2A01

0.50

0.50

2.2~3.0

0.2

0.2~0.5

-

-

0.10

0.15

-

0.05

0.15

Remainder

2A01 alloy aircraft aerospace aluminum alloy wire is used for making medium strength aircraft rivet with a working temperature less than 100 degrees, and it is not restricted by parking time after solid solution treatment and natural aging. The corrosion resistance of the alloy is low, and the rivet must be anodized by the sulfuric acid solution, and the hole is sealed with potassium dichromate. The diameter of the supply wire is 1.6-10mm. This is an old alloy, which is rarely used in new machines, but is still in use on small civil aircraft. 2A01 alloy is a professional alloy for aeronautical rivet.

Alloy	Alloy Series	Main Features of 2A01 Alloy Aircraft Aerospace Aluminum Alloy Wire
2A01	Al-Cu-Mg	2A01 alloy aircraft aerospace aluminum alloy wire is used for making medium strength aircraft rivet with a working temperature less than 100 degrees, and it is not restricted by parking time after solid solution treatment and natural aging. The corrosion resistance of the alloy is low, and the rivet must be anodized by the sulfuric acid solution, and the hole is sealed with potassium dichromate. The diameter of the supply wire is 1.6-10mm. This is an old alloy, which is rarely used in new machines, but is still in use on small civil aircraft. 2A01 alloy is a professional alloy for aeronautical rivet.

 

Typical Mechanical Properties of 2A01 Alloy Wire in Room Temperature
Temper	Tension Strength Rm/MPa	Yield Strength Rp0.2/MPa	Elongation A10/%
T4	294	167	24
O	157	59	24

High Temperature Tensile Strength Rm of 2A01 Alloy Aircraft Aerospace Aluminum Alloy Wire
Temper	d/mm	Rm/MPa
		Min.	Max.	Average
T4	1.6	191.0	229.0	209.5
	2.0	-	-	211.0
	2.5	207.0	211.0	208.3
T4	2.6	-	-	210.0
	3.0	209.0	220.0	214.0
	3.5	218.0	221.0	220.4
	4.0	208.0	212.0	210.8
	5.0	203.0	210.0	207.1
	6.0	-	-	205.0
T6	2.5	214.0	219.0	216.5
	3.0	-	-	218.0

 

Mechanical properties of 2A01 T4 alloy wire with diameter 8mm at different temperatures
Temperatures /ºC	Rm/Mpa	Rp0.2/Mpa	A10/%	Z/%
20	294	167	24	50
100	255	-	24	63
150	226	-	22	66
200	186	-	26	69

 

High temperature shear strength of 2A01-T4 alloy wire with diameter 8mm
Temperatue /ºC	Shear Strength/MPa	Temperatue /ºC	Shear Strength/MPa
200	206	200	137
100	177	250	108
150	167	300	59