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Results 1 - 10 of 60 for Compressor blade
  • Supplier Profile
    Damien technologies, founded in 1920, is manufacturing spot welders, arc stick welders, MIG welders and air compressors.Damien is now the uncontested leader in resistance welding, and designed the...
  • Article - 12 Sep 2002
    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...
  • Article - 26 Feb 2001
    Materials such as titanium alloys (Ti6Al4V) and the evolution of turbine blade design are described. Future materials devlopments such as the move to carbon composites are also discussed.
  • Article - 14 Aug 2003
    Ti4Al4Mo2Sn is a high strength forging titanium alloy. Its silicon content improves strength and creep resistance at intermediate temperatures. Other designations, phyical and mechanical properties,...
  • Article - 14 Aug 2003
    Ti5Al2Sn4Mo2Zr4Cr is a near beta titanium alloy. It has properties that are superior to Ti6Al4V. Other designations, phyical and mechanical properties, fabrication details and applications are...
  • Article - 16 Jul 2003
    Electrical Discharge Machining (EDM) is being seen as a novel technique for surface modification. How the process works, problems associated with it, electrode materials, wear and corrosion resistant...
  • Article - 1 Aug 2003
    Investment casting is a process that can be used to manufacture high precision metallic components. Materials suitable for investment casting and its evolution are described. Market history and...
  • Video
    In this video, Prof. Sir Colin Humphreys describes the operation of Rolls-Royce University Technology Centre and how new materials developed in this department are helping to improve turbine...
  • Article - 14 Oct 2014
    The modern jet engine has completely transformed the way we travel, conduct business and connect with the world.
  • Article - 23 Aug 2001
    The use of abradable coatings has enabled increased efficiency gas turbine engines by reducing the clearances between fan and shroud and increasing the operating temperature. They can be applied to...