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Haynes 230

2.4733
Nickel Alloysni_cr_w
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Nickel-chromium-tungsten alloy — THE combustor can material for gas turbines. Outstanding oxidation resistance to 1149°C for prolonged exposure. Excellent long-term thermal stability (no sigma/mu phase after 16000h at 649-870°C). Lower thermal expansion than most high-temp alloys. Lanthanum addition improves oxide scale adherence. Used for gas turbine combustion cans, transition ducts, furnace retorts, and catalyst grids in nitric acid production.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸UNSUSAUNS N06230N06230REF
🇪🇺ENEuropeNiCr22W14Mo / 2.47332.4733100%
🇺🇸AMSUSAAMS 5878 (sheet) / AMS 5891 (bar)—100%

Sources: ASTM B435, DIN 17744, AMS 5878

Chemical composition comparison (wt%)

Side-by-side: Haynes 230 (UNS) (ASTM B435) vs NiCr22W14Mo / 2.4733 (EN)

ElementHaynes 230 (UNS)NiCr22W14Mo / 2.4733 (EN)Overlap
C0.05–0.1%——
Si0.25–0.75%——
Mn0.3–1%——
Cr20–24%——
Mo1–3%——
Ni———
W13–15%——
Al0.2–0.5%——
B0–0.015%——
Co0–5%——
Fe0–3%——
La0.005–0.05%——

Mechanical properties

Solution Treated

PropertyValueUnit
Tensile Strength≥ 760MPa
Yield Strength≥ 310MPa
Elongation≥ 40%
Elastic Modulus≥ 211GPa
Density≥ 8.97g/cm3

Heat treatment

ProcessTemperatureMediumHolding TimeNotes
solution_treatment1177–1246 °Crapid air or water—Not precipitation-hardenable — solution treated only

Compatibility verdict

Haynes 230 and NiCr22W14Mo / 2.4733: 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.