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Ti-6Al-2Sn-4Zr-2Mo-Si (Ti-6242S)

3.7145
Titaniumnear_alpha
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Near-alpha high-temperature titanium alloy with silicon addition for creep resistance. UNS R54620. Rm 940–1110 MPa, Rp0.2 860–1050 MPa, A 13–15%. Density 4.54 g/cm³, E-Modul 114–118 GPa. Excellent creep strength and thermal stability to 540°C. AMS 4919/4975/4976. Applications: gas turbine compressor blades and discs, impellers, afterburner structures, hot airframe skin. Boeing 787, GE/P&W engines.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸UNSUSAR54620%
🇩🇪DINGermanyTiAl6Sn2Zr4Mo2Si3.7145%
🇺🇸AMSUSAAMS 4919/4975/4976%
🇺🇸ATIUSAATI 6-2-4-2%

Sources: SAE/ASTM, DIN, SAE AMS, atimaterials.com

Mechanical properties

Compatibility verdict

Ti-6Al-2Sn-4Zr-2Mo-Si (Ti-6242S) and R54620: null% composition match

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