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  1. TIMETAL 6-2-4-2 has an outstanding combination of tensile strength, creep strength, toughness, and high-temperature stability for long-term application at temperatures up to 1000°F (538°C). Its primary application is gas turbine compr essor components such as blades, discs, and impellers.

  2. Ti-6Al-2Sn-4Zr-2Mo (UNS designation R54620), also known as Ti 6-2-4-2, is a near alpha titanium alloy known for its high strength and excellent corrosion resistance.

  3. TIMETAL6-2-4-6 is an alpha-beta alloy capable of being heat treated to higher strengths in greater section sizes than TIMETAL ® 6-4 alloy. The properties of this alloy are influenced by its thermo-mechanical history.

  4. Titanium Ti-6Al-2Sn-4Zr-2Mo (Ti-6-2-4-2), Duplex Annealed. Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy. Material Notes: Alpha Alloy. Silicon is often added to improve creep resistance (See Ti-6242S). Characteristics: Good elevated-temperature performance, good creep strength.

  5. 1 Αυγ 2020 · ATI 6-2-4-2 is a near-alpha, high strength, titanium alloy that exhibits a good combination of tensile strength, creep strength, toughness, and long-term stability at temperatures up to 425 °C (800 °F). Silicon up to 0.1% frequently is added to improve the creep resistance of the alloy.

  6. Alpha Alloy. Silicon is often added to improve creep resistance (See Ti-6242S). Applications: High-temp jet engines. Blades, discs, spacers, seals. High performance automotive valves. References for this datasheet.

  7. Titanium Ti-6Al-2Sn-4Zr-2Mo (Ti-6-2-4-2), Sheet. Unspecified heat treatment. Alpha Alloy. Silicon is often added to improve creep resistance (See Ti-6242S). Applications: High-temp jet engines. Blades, discs, spacers, seals. High performance automotive valves.

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