Comparative Analysis of Next-Gen Single-Crystal Nickel Superalloys for HPT Blades via FEM
DOI:
https://doi.org/10.3849/aimt.02004Keywords:
lightweight alloys, HPT blade, FEA, nickel-based superalloys, strain and deformation analysisAbstract
This study details a structural integrity evaluation of a high-pressure turbine (HPT) blade made up of three nickel-based single-crystal superalloys, specifically CMSX-4, CMSX-8, and CMSX-4 Plus. Finite element analysis was conducted to evaluate stress, strain, deformation, and safety factor under real thermal and mechanical loading. Aerodynamic precision was simulated in blade geometry, discretized using tetrahedral elements, and fixed root and surface pressure was applied. Material information was used from experimental sources. Results showed similar levels of stress for all alloys, but differences in strain and deformation were noted. CMSX-8 registered the lowest deformation and highest safety factor, indicating better mechanical performance and appropriateness as the material of choice for future high-performance turbine blades.
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