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Technology update

Evolution of PM nickel base superalloy processes and products

Pages 10-13 | Published online: 19 Jul 2013

REFERENCES

  • R. Couturier et aL: 'Process devel-opment and mechanical properties of alloy U 720LI for high temperature turbine disk', in ‘Superalloys 2004’; 2004, Warrendale, PA, TMS.
  • P.Kantzoset :‘Effect ofpowder cleanliness on the fatigue behaviour of powder metallurgy Ni-disk alloy Udimet 720’, in 'Superalloys2004';2004,Warrendale, PA, TMS.
  • A.Pineau: ‘Superalloysdisksdurability and damage tolerance in relation to inclusions’, Proc. Conf. on 'High temperature materials for powerengineering',Liege,Belgium, September 1990; 1900, Dordrecht, Kluwer Academic Publishers.
  • ‘Fatigue crack growth resistant nickel-base article and alloy and method for making’, US Patent 4,957,567, 18 September1990.
  • D. R. Chang et aL: ‘Superalloy powder processing, properties and turbine disk applications; in 'Super-alloys 1984’; 1984, Warrendale, PA, TMS.
  • G.Garibov: ‘Improvement inperformance characteristics of as-hipped PM superalloy disks, Proc. Int. Conf. on 'Hot isostatic pressing’, Paris, France, May 2005, FIAP.
  • V. Y. Koshelev et aL: ‘Study of the effect of powder size on low-fatigue-resistance of EP741-NP type superalloy’, Proc. Int. Conf. on ‘Hot isostatic pressing’, Paris, France, May 2005, FIAP.

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