Ti-6Al-2Sn-4Zr-2Mo
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Ti-6Al-2Sn-4Zr-2Mo - 1

Ti-6Al-2Sn-4Zr-2Mo is near α titanium alloy with high creeping resistance, which is working at 470℃-550℃ and mainly used for manufacture of discs and blades of high pressure compressor of aero-engine. This alloy was successfully developed in 1974 by foreign and was done a lot of basic and applied research and development. At present, Ti-6242 alloy has been successfully used for aero-engine of F414, F119 and TRENT800 aircrafts. Residual Each Total ≤0.1 ≤0.30 Mechanical Properties Room temperature

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Ti-6Al-2Sn-4Zr-2Mo - 2

Ultrasonic Test as per AMS 2628 Ultrasonic Hole Depth Data Recording Signal-to-Noise Ratio Note 1: Depth less than 4 inches Note 2: Depth 4 inches and over

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