Home | Products | AD730 – Nickel alloys

AD730 Nickel alloys

  • Aerospace
  • Defense
  • Energy
  • Tooling

Spécifications

  • EU
    NiCr16Co9Fr4Mo3W3Ti3Al2

Typical composition

  • Ni
    Base
  • Cr
    16
  • Mo
    3
  • Ti
    4
  • Co
    9
  • Al
    2
  • Nb
    1
  • W
    3
  • Fe
    4

Applications

• Aero Engines and Land Turbines : engines disk, buckets, fasteners, blades
• Specialities : hot parts for turbo shafts in motorsport
• Hot Tooling

Mechanical properties

• Good high temperature fatigue creep resistance
• High microstructural stability up to 750°C
• Better oxydation resistance than Waspaloy or 720 Alloy

Mechanical features

  • Heat treatment
    H + V
  • UTS (N/mm²)
    1580
  • A (%)
    20
  • Solution treated : H
    Annealed : R
  • Thermo-mechanical treatment : TM
    Quenched and tempered : T+RV
  • Sub-zero treatment : F
    Solution treated and aged : T+RV
AD730 superalloy 2024
Download (PDF, 6 MB)

See also

PER3

  • Aerospace
  • Energy
Nickel alloys
  • Aero engine
  • Disks
  • High temperature
  • Land turbine
Spécifications
  • Common name : WASPALOY
  • EU : NiCr20Co13Mo4Ti3Al
  • USA : UNS:N07001
Heat treatment
  • H + V
Read more

PER72

  • Aerospace
  • Energy
Nickel alloys
  • Aero engine
  • Disks
  • Impellers
  • Land turbine
Spécifications
  • Common name : UDIMET 720
  • EU : NiCr18Co15TiMoAl
Heat treatment
  • H + V
Read more
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