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ASSESSMENT OF BEARING HEAT GENERATION PREDICTION BY THE PROGRAM ADORE WITH RESPECT TO EXPERIMENTAL RESULTS AND SHABERTH PREDICTIONS

机译:关于实验结果和雪平预测的程序崇拜轴承发热预测的评估

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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:这项工作详细介绍了涡轮机气动发动机主轴轴承的发热分析,使用电脑节目的滚动元件(宽度)的高级动力学。用于牵引和搅拌热产生的经验模型是详细的。示出了对涂覆的预测,证明了不同负载/速度制度以不同负载/速度制定的牵引和搅拌的不同贡献。然后将这些结果与实验结果进行比较。此外,还将涂层的结果与来自众所周知的轴承分析程序Shaberth(轴承热分析)的结果进行了比较。比较在Adore之间显示出良好的一致性,并且在13.35和53.40kN之间的载荷之间的实验结果和1.8和2.2 MDN之间的速度。该结果还在该制度中通过Shaberth预测了热量产生。鉴定并推测两种程序的局限性,包括在高速/载荷上缺乏可用的实验牵引数据,包括实证模型中的局限性。最后,提供了对未来研究的建议,这可能会提供预测涡轮机气动发动机应用中轴承发热的能力的显着改进。

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