Skip to content

Haynes 230

2.4733
nickelni_cr_w
Export PDF€4.90

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

Mechanical properties

Compatibility verdict

Haynes 230 and NiCr22W14Mo / 2.4733: 100% composition match

Related materials

More Nickel materials →

Export this comparison as PDF

Professional datasheet with equivalents, composition, and properties. Ready for your QM documentation.

Download PDF — €4.90

Included with PRO subscription