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 |
|||||||||||
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 % |
||
ksi |
MPa |
ksi |
MPa |
|||
Titanium Alloy 6-2-4-2 /6Al-2Sn-4Zr-2Mo |
150 |
1034 |
140~165 |
965~1138 |
10 |
20 |
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