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Results 61 - 70 of 569 for Aircraft parts
  • Article - 23 Aug 2001
    Spray formed Ni and Al alloys offer improved performance and reduced costs for some aerospace applications. The process is described and its application to nickel superalloys and aluminium alloys....
  • 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...
  • Article - 16 Aug 2001
    Very expensive laminate, exhibits the best notched izod impact strength and lowest density. Relative advantages, disadvantages and applications are listed together with a table of typical properties.
  • Article - 15 Mar 2001
    Intermetallics possess many remarkable properties, but processing intermetallic components can be difficult. This article looks into the possibility of producing coatings of metal aluminides and the...
  • Article - 7 Mar 2001
    The benefits of PM superalloys over conventional superalloys are explored. It covers the nickel and titanium based superalloys and looks at future developments and directions.
  • Article - 28 Feb 2001
    An outline of the use of halogenated epoxy resins which display hydrophobic characteristics. These adhesives prevent moisture from attacking polymer metal joints and are based on fluoroepoxy resins.
  • Article - 28 Feb 2001
    This article discusses the moisture resistance of adhesive bonding in severe environments.
  • Article - 26 Feb 2001
    Materials evolution (titanium and nickel alloys) and hence property evolution are covered.
  • 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 - 26 Feb 2001
    Developments in advanced materials over the years have contributed to the spectacular progress in the thrust-to-weight ratio of the aero gas turbine.

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