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Results 1 - 9 of 9 for MIL –T-9047.
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  • Ti5Al2.5Sn is a high strength alloy commonly used in airframe and jet engine applications. It has excellent weldability, stability and high temperature strength. Composition, designations, physical...
  • Ti8Al1Mo1V is a high strength near alpha alloy. It has excellent creep resistance up to 430°C and is used in forged fan and compressor blades. It has the highest tensile modulus and lowest density of...
  • Ti6Al2Sn4Zr2Mo is a near alpha titanium alloy suiable for high temperature use. Its main uses are in gas turbine engines and hot airframe components. Physical and mechanical properties are provided as...
  • Ti 6Al-4V is the most widely used of all the alpha-beta titanium alloys. It may be heat treated for high strength in welded construction at service temperatures through 600°F. Typical applications are...
  • Ti3al2.5V, sometimes called half 6-4 is available in two grades. Grade 18 has a small palladium addition to increase corrosion resistance. These grades offer improved strength over pure grades and...
  • Ti6Al2Sn4Zr6Mo is a heat treatable alpha-beta alloy that combines the high temperature properties of Ti6Al2Sn4Zr2Mo with higher strength. Composition ranges, designations, physical and mechanical...
  • This near alpha alloy is developed primarily for high temperature applications. 6-2-4-2 combines excellent strength and corrosion resistance with considerably good weld and fabrication.
  • Ti3Al8V6Cr4Mo4Zr is a metastable beta titanium alloy. Grade 20 differs from grade 19 in that it has palladium added for corrosion resistance. The composition, mechanical and physical properties are...
  • Ti6Al6V2Sn is heat treatable to higher strengths and larger sections compared to Ti6Al4V. Its main use is in airframes. Composition, physical and mechanical properties and fabrication are all covered.
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