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- W4311543919 abstract "Aero-engine turbine disks are safety-relevant components which are operated under high thermal and mechanical stress conditions. The actual part qualification and certification procedures make use of spin-tests conducted on production-similar disks. While these tests provide, on the one hand, a reliable definition of the critical conditions for real components, on the other hand they represent a relevant cost item for engine manufacturers. The aim of this work is to present two alternative burst speed assessment methods under development based on the Failure Assessment Diagram (FAD) and a global stability criterion, respectively. In the scope of the fracture mechanics assessment, the failure modes hoop-burst and rim-peeling are investigated with semi-circular surface cracks modelled at the critical regions on the turbine disk. The comparison of the predicted critical rotational speed shows good agreement between the assessment methods." @default.
- W4311543919 created "2022-12-27" @default.
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- W4311543919 date "2023-01-01" @default.
- W4311543919 modified "2023-09-25" @default.
- W4311543919 title "Burst speed assessment of aero-engine turbine disk based on failure assessment diagram and global stability criterion" @default.
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- W4311543919 doi "https://doi.org/10.1016/j.engfracmech.2022.109005" @default.
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