Cast Alloy

GMR 235

GMR 235 is a precipitation-hardened alloy providing solid creep and oxidation resistance for investment cast turbine nozzles and vanes. Qualified under EMS 73635, it was developed for jet engine hot-section components and has seen sustained use in industrial gas turbines where proven alloy chemistry and established casting practice are valued. Its moderate boron content supports grain boundary strengthening for reliable long-term performance.
Industry Specification
Industries
Aerospace
Power Generation

Nominal Chemistry (wt %)

GMR 235 is a nickel-base cast superalloy for turbine vane and nozzle applications in jet and industrial gas turbine engines.
0.15
Carbon
3
Aluminium
0.06
Boron
15.5
Chromium
Cobalt
Hafnium
5.3
Molybdenum
Niobium / Columbium
Tantalum
2
Titanium
Tungsten
Zirconium
10
Iron
Bal
Nickel

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Military & Defense
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specification
Cast Alloy

GMR 235

GMR 235 is a precipitation-hardened alloy providing solid creep and oxidation resistance for investment cast turbine nozzles and vanes. Qualified under EMS 73635, it was developed for jet engine hot-section components and has seen sustained use in industrial gas turbines where proven alloy chemistry and established casting practice are valued. Its moderate boron content supports grain boundary strengthening for reliable long-term performance.

Keep exploring.

All alloys
Powder Alloy

282

282 is a gamma prime strengthened nickel-base superalloy powder with high creep strength and strong fabricability for additive manufacturing.

Cast Alloy

René N515

René N515 is a reduced-rhenium single crystal nickel-base superalloy for high-pressure turbine blades and nozzle guide vanes.

C50TF130
Cast Alloy

René N500

René N500 is a rhenium-free single crystal nickel-base superalloy for high-pressure turbine blades and nozzle guide vanes.