2A10 Aircraft Aerospace Aluminum Alloy Wire

• Color: Silver
• Application: Transportation Tools, Door & Window, Decorations
• Certification: ISO9001, ASTM, JIS, GB, EN
• Technique: Extruded
• Grade: 2000 Series
• Temper: O - H112
• Model NO.: 2A10
• Surface Treatment: Enameled Wire
• 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

 

 

 

2A10 aircraft aerospace aluminum alloy Wire

 

The shear strength of wire for 2A10 aircraft aerospace aluminum alloy Wire is high. It has enough riveting rivet in annealing, rigid quenching, aging and hot state. After riveting with quenching and aging, the riveting process is not limited by time after heat treatment. The weldability of aluminum plate 2A10 is the same as that of 2A11, and the corrosion stability of the rivet is the same as that of 2A01 and 2A11. When the heating is over 100 ºC, the tendency of intergranular corrosion is produced.
 

Alloy	Alloy Series	Main Features
2A10	Al-Cu-Mg	Heat treatment reinforced alloy, Al-Cu-Mn series of natural failure aircraft structure special rivet alloy, used in the manufacture of high strength rivets. The plasticity of the alloy at ambient temperature, the cold can be made into all kinds of rivets, good can weld, solder alloy used in gas welding, argon arc welding and the weld in the process of formation of hot crack tendency.

 

High Temperature Shear Strength of 2A10 T6 Aircraft Aerospace Aluminum Alloy Wire with Diameter 8mm
Stabilization Treatment		Temperature/ºC	Time t/min	Shear Strength t/Mpa
Temperature /ºC	Time t/h
-	-	20	30	247
-	-	100		225
-	-	125		200
-	-	150		193
-	-	175		183
-	-	185		180
-	-	190		178
-	-	200		177
-	-	210		163
-	-	220		150
-	-	250		125
125	100	125		228
150	100	150		219
175	100	175		177
190	100	190		161
200	100	200		152
220	100	220		126
225	100	225		113
250	100	250		89
300	100	300		63

 

Axial tensile fatigue behavior of 2A10 alloy riveted structure with diameter 4mm at room temperature
Type	Sample State	Rivet Diameter d/mm	K	R	Rmax/Mpa	F/(Week.min^-1)	N/week
Rivet	Solid solution heat treatment at 515 ºC + artificial aging 75 ºC, 24h	4	0.6	0.1	751	83	1.04×10^5
							1.82×10^5
							1.55×10^5
			0.7		876		8.5×10^5
							1.11×10^5
							9.3×10^5
	Solid solution heat treatment 515ºC+artificial aging  75ºC, 24h+Stabilization Treatment 150ºC/75h+175ºC/5h		0.6		751	111	2.03×10^5
							1.75×10^5
							1.74×10^5

Shear Strength of 2A10 T6 Aircraft Aerospace Aluminum Alloy Wire with Diameter 4mm

Stabilization Treatment

Shear Strength t/Mpa

Temperature /ºC

Time  t/h

-

100
 

255

125

254

150

246

175

215

190

221

200

211

220

193

225

179

250

161

300

143