7050 T651 aerospace aircraft aluminum block

7050 T651 aerospace aircraft aluminum block introduction
The main alloying element of 7050 T651 aerospace aircraft aluminum block is zinc. Adding magnesium to the alloy containing 3%-75% zinc can form MgZn2 with remarkable strengthening effect, which makes the heat treatment effect of this alloy far better than aluminum-zinc binary alloy. Mainly used in aerospace, mold processing, mechanical equipment, fixtures, especially for aircraft manufacturing structures and other high-stress structures with high strength and corrosion resistance.


 
7050 T651 aerospace aircraft aluminum block chemical composition:
Aluminum (Al) balance
Chromium (Cr) ≤ 0.04
Zirconium (Zr) 0.08~0.15
Zinc (Zn) 5.7 ~ 6.7
Silicon (Si) ≤ 0.12
Iron (Fe) 0.000 ~ 0.150
Manganese (Mn) ≤ 0.10
Magnesium (Mg) 1.9 ~ 2.6
Titanium (Ti) ≤ 0.06
Copper (Cu) 2.0 to 2.6
 
7050 T651 aerospace aircraft aluminum block mechanical properties
State Tensile strength Yield strength Elongation Hardness (a) Shear strength Fatigue strength (b)
MPa ksi MPa ksi sample thickness
T7651 552 80 ·490 71 11· 135 324 47· 71 10.4
 
7050 T651 aerospace aircraft aluminum block Usage:
7050 T651 aerospace aircraft aluminum block is mainly used in aerospace, mold processing, mechanical equipment, fixtures, especially for aircraft manufacturing structures and other high-stress structures with high strength and corrosion resistance.