温度,应变速率和条件对AlSi-PES磨损器机械反应的影响
R Lye1, A Pellegrino2, C Bennett1
1Mechanical and Aerospace Systems Research Group, Faculty of Engineering, University of Nottingham, Nottingham, UK.
概括
可磨损层状况显著影响航空发动机压缩机性能. 在各种条件下了解可磨损材料的行为可以改善刀片设计和发动机效率.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 航空发动机压缩机中的可磨损内可以减少叶片尖端的空隙,以提高效率.
- 由于制造和使用中的因素,可磨损性质的变化使性能建模复杂化.
- 不准确的建模导致刀片和空隙的设计不足.
研究的目的:
- 调查可磨损条件对其机械性能的影响.
- 分析可磨损条件对刀片外相互作用反应的影响.
- 在各种条件下描述可磨损材料的故障行为.
主要方法:
- 在近静态和高速负荷下,具有特征的--聚可磨损反应.
- 在各种温度下测试材料,并进行模拟生命周期阶段的预处理.
- 评估了聚相衰老对机械行为的影响.
主要成果:
- 可磨损材料的行为对应变速率,温度和聚阶段条件都很敏感.
- 聚阶段的老化在高速率下增加了高达10%的故障应力,在压缩样本中增加了50%.
- 增加聚结晶性增强了热稳定性和故障应力.
结论:
- 了解可磨损故障行为对于优化压缩机叶片和系统设计至关重要.
- 特定条件的数据弥合了实验摩擦测试和可磨损反应之间的差距.
- 改进的设计可以实现最佳的尖端距离,并提高发动机的整体性能.
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