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Turbine Rotor Material Design: Phase II. Final rept.
| 题名： | Turbine Rotor Material Design: Phase II. Final rept. |
| 作者： | McClung-R.C.; Leverant-G.R.; Enright-M.P.; Huyse-L.; Lee-Y.D. |
| 关键词： | *Federal-Aviation-Administration; *Aircraft-engine-industry; *Turbine-rotor-material-design.;Life-management-process; Damage-tolerance; Material-anomalies; Manufacturing-anomalies; High-energy-rotating-components. |
| 摘要： | The Federal Aviation Administration (FAA) is working with the aircraft engine industry to develop an enhanced life management process, based on probabilistic damage tolerance principles, to address the threat of material or manufacturing anomalies in high-energy rotating components, and the process is documented in current and planned versions of FAA Advisory Circular (AC) 33.14. An integrated team of Southwest Research Institute, GE Aviation, Pratt & Whitney, Honeywell, and Rolls-Royce Corporation has developed enhanced predictive tool capability and supplementary material/anomaly behavior characterization and modeling to support and enhance the process and the AC. |
| 报告类型： | 科技报告 |
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