为了解决强背景噪声环境下直升机滚动轴承故障信号微弱,故障特征难以提取的问题,提出一种基于最小熵解卷积(Minimum Entropy Deconvolution,MED)与Teager能量算子(Teager Energy Operator,TEO)的滚动轴承故障特征提取的新方法。根据滚...为了解决强背景噪声环境下直升机滚动轴承故障信号微弱,故障特征难以提取的问题,提出一种基于最小熵解卷积(Minimum Entropy Deconvolution,MED)与Teager能量算子(Teager Energy Operator,TEO)的滚动轴承故障特征提取的新方法。根据滚动轴承故障信号表现为冲击波形的特点和MED降噪对冲击特征敏感的特性,采用MED对故障信号进行降噪处理,同时增强信号中的冲击成分;再结合TEO适合检测信号的瞬时变化,能有效提取故障信号冲击特征的特点,计算降噪信号的Teager能量信号,进行频谱分析提取滚动轴承的故障特征。通过对仿真信号和直升机滚动轴承混合故障信号进行分析,实验结果表明,该方法能有效提取强背景噪声环境中的微弱复合故障特征,具有一定的工程应用价值。展开更多
Three-dimensional unsteady Euler equations are numerically solved to simulate the unsteady flows around forward flight helicopter with coaxial rotors based on unstructured dynamic overset grids. The performances of th...Three-dimensional unsteady Euler equations are numerically solved to simulate the unsteady flows around forward flight helicopter with coaxial rotors based on unstructured dynamic overset grids. The performances of the two coaxial rotors both become worse because of the aerodynamic interaction between them, and the influence of the top rotor on the bottom rotor is greater than that of the bottom rotor on the top rotor. The downwash velocity at the bottom rotor plane is much larger than that at the top rotor plane, and the downwash velocity at the top rotor plane is a little larger than that at an individual rotor plane. The downwash velocity and thrust coefficient both become larger when the collective angle of blades is added. When the spacing between the two coaxial rotors increases, the thrust coefficient of the top rotor increases, but the total thrust coefficient reduces a little, because the decrease of the bottom rotor thrust coefficient is larger than the increase of the top rotor thrust coefficient.展开更多
文摘为了解决强背景噪声环境下直升机滚动轴承故障信号微弱,故障特征难以提取的问题,提出一种基于最小熵解卷积(Minimum Entropy Deconvolution,MED)与Teager能量算子(Teager Energy Operator,TEO)的滚动轴承故障特征提取的新方法。根据滚动轴承故障信号表现为冲击波形的特点和MED降噪对冲击特征敏感的特性,采用MED对故障信号进行降噪处理,同时增强信号中的冲击成分;再结合TEO适合检测信号的瞬时变化,能有效提取故障信号冲击特征的特点,计算降噪信号的Teager能量信号,进行频谱分析提取滚动轴承的故障特征。通过对仿真信号和直升机滚动轴承混合故障信号进行分析,实验结果表明,该方法能有效提取强背景噪声环境中的微弱复合故障特征,具有一定的工程应用价值。
基金China Postdoctoral Science Foundation (20100481368)National Key Laboratory Foundation of China
文摘Three-dimensional unsteady Euler equations are numerically solved to simulate the unsteady flows around forward flight helicopter with coaxial rotors based on unstructured dynamic overset grids. The performances of the two coaxial rotors both become worse because of the aerodynamic interaction between them, and the influence of the top rotor on the bottom rotor is greater than that of the bottom rotor on the top rotor. The downwash velocity at the bottom rotor plane is much larger than that at the top rotor plane, and the downwash velocity at the top rotor plane is a little larger than that at an individual rotor plane. The downwash velocity and thrust coefficient both become larger when the collective angle of blades is added. When the spacing between the two coaxial rotors increases, the thrust coefficient of the top rotor increases, but the total thrust coefficient reduces a little, because the decrease of the bottom rotor thrust coefficient is larger than the increase of the top rotor thrust coefficient.
