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Waspaloy

2.4654
Nickel Alloysage_hardenable
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Nickel-based gamma-prime strengthened superalloy — THE turbine disc material. Excellent creep-rupture strength up to 650°C (rotating) and 870°C (static). Developed 1950s by Pratt & Whitney. Triple-aged (solution + stabilize + precipitation) for peak properties. Superior to Inconel 718 above 650°C. Used for compressor and rotor discs, shafts, spacers, seals, rings, casings, and fasteners in gas turbine engines.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸UNSUSAUNS N07001N07001REF
🇪🇺ENEuropeNiCr20Co13Mo4Ti3Al / 2.46542.4654100%
🇺🇸AMSUSAAMS 5544 (sheet) / AMS 5706 (bar)—100%

Sources: ASTM B637, EN ISO 9723, AMS 5706

Chemical composition comparison (wt%)

Side-by-side: Waspaloy (UNS) (ASTM B637) vs NiCr20Co13Mo4Ti3Al / 2.4654 (EN)

ElementWaspaloy (UNS)NiCr20Co13Mo4Ti3Al / 2.4654 (EN)Overlap
C0.02–0.1%——
Si0–0.75%——
Mn0–1%——
Cr18–21%——
Mo3.5–5%——
Ni———
Al1.2–1.6%——
Ti2.75–3.25%——
B0.003–0.01%——
Co12–15%——
Fe0–2%——
Zr0.02–0.12%——

Mechanical properties

Aged

PropertyValueUnit
Tensile Strength1170–1310MPa
Yield Strength720–895MPa
Elongation15–25%
Hardness HRC34–44HRC
Elastic Modulus≥ 213GPa
Density≥ 8.19g/cm3

Heat treatment

ProcessTemperatureMediumHolding TimeNotes
solution_treatment996–1010 °Cair or oil2-4 hoursType B per Special Metals for tensile properties
stabilization843–843 °Cair4 hoursIntermediate aging step
precipitation_aging760–760 °Cair16 hoursGamma-prime precipitation

Compatibility verdict

Waspaloy and NiCr20Co13Mo4Ti3Al / 2.4654: 100% composition match

Close equivalents but NOT identical.

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All data is for reference only. Equivalents indicate similarity, not identity. Always verify against the applicable specification for safety-critical applications. materialref.com accepts no liability for decisions based on this data.