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6Al-6V-2Sn Titanium per AMS 6935

The AMS 6935 specification covers 6Al-6V-2Sn titanium alloy in the form of bars, wire, forgings. Specification AMS 6935 also calls for 6Al-6V-2Sn to be Solution Heat Treated and Aged.

6-6-2 Alloy (UNS R56620) is a highly beta-stabilized, two-phase, alpha-beta titanium alloy which is a modification of the Ti6Al-4V system. Because of the higher Beta stabilizing elements (additional Vanadium + Fe and Cu), this alloy has a higher strength potential than Ti-6Al-4V, but at a sacrifice of weldability and toughness. In most cases, the welding of 6-6-2 alloy is not recommended. It can be used in the annealed or solution treated and aged conditions.

Applications of 6Al-6V-2Sn per AMS 6935

The landing gear of an aircraft is the system of struts, wheels, and other components that support the aircraft when it is on the ground. These components must be strong enough to support the weight of the aircraft and withstand the stresses of landing and takeoff. 6Al-6V-2Sn per AMS 6935 is sometimes used for the manufacture of landing gear components due to its high strength and corrosion resistance.

6Al-6V-2Sn per AMS 6935 Round Bar diameters range from 0.125″ to 14.00″ diameter.

AMS 6935, AMS 6935, FIGHTER JET METALS

6Al-6V-2Sn TITANIUM SPECIFICATIONS

GULFSTREAM AEROSPACE SPECIFICATIONS