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  2. Titanium alloys - Wikipedia

    en.wikipedia.org/wiki/Titanium_alloys

    Titanium alloy in ingot form. Titanium alloys are alloys that contain a mixture of titanium and other chemical elements. Such alloys have very high tensile strength and toughness (even at extreme temperatures). They are light in weight, have extraordinary corrosion resistance and the ability to withstand extreme temperatures.

  3. Ti-6Al-4V - Wikipedia

    en.wikipedia.org/wiki/Ti-6Al-4V

    Ti-6Al-4V titanium alloy commonly exists in alpha, with hcp crystal structure, (SG : P63/mmc) and beta, with bcc crystal structure, (SG : Im-3m) phases. While mechanical properties are a function of the heat treatment condition of the alloy and can vary based upon properties, typical property ranges for well-processed Ti-6Al-4V are shown below.

  4. Ti-10V-2Fe-3Al - Wikipedia

    en.wikipedia.org/wiki/Ti-10V-2Fe-3Al

    Ti-10V-2Fe-3Al (UNS designation R56410), also known as Ti 10-2-3, is a non-ferrous near-beta titanium alloy featuring an excellent combination of strength, ductility, fracture toughness and high cycle fatigue strength.

  5. Titanium - Wikipedia

    en.wikipedia.org/wiki/Titanium

    Lockheed A-12, first plane made of 93% titanium. Because titanium alloys have high tensile strength to density ratio, [17] high corrosion resistance, [12] fatigue resistance, high crack resistance, [99] and ability to withstand moderately high temperatures without creeping, they are used in aircraft, armor plating, naval ships, spacecraft, and ...

  6. Ti-6Al-7Nb - Wikipedia

    en.wikipedia.org/wiki/Ti-6Al-7Nb

    Ti-6Al-7Nb (UNS designation R56700) is an alpha-beta titanium alloy first synthesized in 1977 containing 6% aluminum and 7% niobium. It features high strength and has similar properties as the cytotoxic vanadium containing alloy Ti-6Al-4V. Ti-6Al-7Nb is used as a material for hip prostheses. [1]

  7. Titanium Beta C - Wikipedia

    en.wikipedia.org/wiki/Titanium_Beta_C

    Titanium Beta C refers to Ti Beta-C, a trademark for an alloy of titanium originally filed by RTI International. [1] It is a metastable "beta alloy" which was originally developed in the 1960s; Ti-3Al-8V-6Cr-4Mo-4Zr, nominally 3% aluminum, 8% vanadium, 6% chromium, 4% molybdenum, 4% zirconium and balance (75%): titanium.

  8. Ti-6Al-2Sn-4Zr-2Mo - Wikipedia

    en.wikipedia.org/wiki/Ti-6Al-2Sn-4Zr-2Mo

    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. It is often used in the aerospace industry for creating high-temperature jet engines and the automotive industry to create high performance automotive valves.

  9. Superalloy - Wikipedia

    en.wikipedia.org/wiki/Superalloy

    Such alloys promise improvements on high-temperature applications, strength-to-weight, fracture toughness, corrosion and radiation resistance, wear resistance, and others. They reported ratio of hardness and density of 1.8–2.6 GPa-cm 3 /g, which surpasses all known alloys, including intermetallic compounds, titanium aluminides, refractory ...