Titanium 6-6-2 (6Al-6V-2Sn) is a heat treatable, high strength titanium alloy with higher strength and section hardenability that 6Al-4V. but with lower toughness and ductility and limited weldability. 6-6-2 is typically used in airframe component applications.
Standard Specification:
AMS 4971 bars, rings, forgings (annealed, heat treatable)
AMS 4978 bars, rings, forgings (annealed)
AMS 4979 bars, rings, forgings (annealed & precipitation heat treated)
AMS 6935 bars, forgings (solution treated & aged)
AMS 6936 bars, forgings (annealed)
AMS-T-9047 6Al-6V-2Sn bar;
MIL-T-9047 6Al-6V-2Sn bar;
Standard |
Werkstoff No. |
UNS |
AMS Titanium Alloy 6-6-2 /6Al-6V-2Sn |
3.7174 |
R56620 |
Technical Data Sheet
Chemical Composition |
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Weight % |
Ti |
Al |
V |
Sn |
C |
Fe |
N |
O |
H |
Other |
|
AMS Titanium Alloy 6-6-2 /6Al-6V-2Sn |
Balance |
5.0~6.0 |
5.0~6.0 |
1.5~2.5 |
0.05 |
0.35~1.0 |
0.04 |
0.2 |
0.0150 |
0.3Total Max. |
Typical Mechanical Properties (Tensile Requirements)
Material |
Tensile Strength, min |
Yield Strength (0.2% Offset) min or range |
Elongation in 4D,min% |
Reduction of Area % |
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ksi |
MPa |
ksi |
MPa |
|||
Titanium Alloy 6-2-4-2 /6Al-2Sn-4Zr-2Mo |
150 |
1034 |
140~165 |
965~1138 |
10 |
20 |
Titanium and Copper Clad Bar, which is a layer of titanium coated with a certain thickness on the copper rod, is the main component of the metal anode. It combines the excellent conductivity of coppe
Standard Titanium Grade Condition of Delivery Tolerance Dimensions
Standard Titanium Grade Condition of Delivery Tolerance Dimensions
Titanium Ti5Al2.5Sn (Grade 6) is a high strength alloy which is most commonly used in airframe and jet engine applications. Titanium Ti5Al2.5Sn (Grade 6) has good weldability, stability and strength