首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >ASSESSMENT OF BEARING HEAT GENERATION PREDICTION BY THE PROGRAM ADORE WITH RESPECT TO EXPERIMENTAL RESULTS AND SHABERTH PREDICTIONS
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ASSESSMENT OF BEARING HEAT GENERATION PREDICTION BY THE PROGRAM ADORE WITH RESPECT TO EXPERIMENTAL RESULTS AND SHABERTH PREDICTIONS

机译:关于实验结果和严格预测的程序内核对产热预测的评估

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This work details the heat generation analysis of a turbine aero-engine main-shaft bearing using the computer program Advanced Dynamics Of Rolling Elements (ADORE). The empirical models used for traction and churning heat generation are detailed. The predictions of ADORE are shown to demonstrate the differing contributions of traction and churning to total heat generation at different load/speed regimes. These results are then compared with experimental results. In addition, the results of ADORE are also compared with results from the well-known bearing analysis program SHABERTH (Shaft Bearing Thermal Analysis). The comparisons showed good agreement between ADORE and the experimental results for loads between 13.35 and 53.40 kN and speeds between 1.8 and 2.2 MDN. The results also showed under prediction of heat generation by SHABERTH in this regime. Limitations of both programs were identified and speculated to include limitations in the empirical models due to the lack of available experimental traction data at high speeds/loads. Finally, recommendations for future research are provided which will likely provide significant improvements in the ability to predict bearing heat generation in turbine aero-engine applications.
机译:这项工作使用计算机程序高级滚动元件动力学(ADORE)详细介绍了涡轮航空发动机主轴轴承的发热分析。详细介绍了用于牵引和搅拌生热的经验模型。 ADORE的预测显示出在不同的负载/速度状态下,牵引力和搅动对总热量产生的不同贡献。然后将这些结果与实验结果进行比较。此外,还将ADORE的结果与著名的轴承分析程序SHABERTH(轴轴承热分析)的结果进行比较。比较表明,在13.35至53.40 kN的载荷以及1.8至2.2 MDN的速度下,ADORE与实验结果之间具有良好的一致性。结果还表明,在这种情况下,SHABERTH预测的热量会产生。两种程序的局限性都被确定并推测为包括经验模型中的局限性,这是由于缺乏在高速度/负荷下可获得的实验牵引力数据所致。最后,提供了用于未来研究的建议,这些建议可能会大大改善预测涡轮航空发动机应用中轴承热量产生的能力。

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