NiBRh is a nickel-based alloy incorporating rhodium, belonging to the family of high-performance superalloys designed for extreme thermal and mechanical environments. This material is primarily used in aerospace propulsion systems, particularly in gas turbine engines where it serves critical functions in high-temperature sections that demand exceptional strength, oxidation resistance, and creep resistance. Engineers select NiBRh-type compositions for applications where conventional nickel alloys reach their performance limits, as the rhodium addition enhances high-temperature stability and resistance to thermal fatigue, making it valuable in jet engines, industrial power generation turbines, and specialized chemical processing equipment operating under severe conditions.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Bulk Modulus(K) | 26.46 | GPa | — | ||
Poisson's Ratio(ν) | 0.4400 | - | — | ||
Shear Modulus(G) | -2.570 | GPa | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.784 | kg/m³ | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Band Gap(Eg) | 0.000 | eV | — | ||
Magnetic Moment(μB) | 0.000 | µB | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Energy Above Hull(ΔEhull) | 0.000 | eV/atom | — | ||
Formation Energy(ΔHf) | -0.2307 | eV/atom | — |