Titanium alloy

Details Titanium alloy Titanium alloy

C - Chemistry, Metallurgy

22

C

75/53, 148/37.3

C22C 14/00 (2006.01)

Patent

CA 1231560

Abstract Titanium alloy A weldable titanium alloy particularly intended for use at high temperatures and under conditions of high stress in aircraft engines, the alloy having the composition 5.6% aluminum, 4% tin, 4% zirconium, 1% niobium, 0.25% molybdenum, 0.5% silicon, 0.05% carbon, optionally containing 0.2% tungsten and being used in the heat treated condition. The heat treatment would normally comprise a solution treatment above the beta transus, typically at 1 080°C, and an ageing or stress relieving treatment at a temperature of approximately 650°C for approximately 24 hours.

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