摘要
非接触叶尖计时法作为监测旋转叶片振动参数的有效手段,近年来在航空发动机叶片振动监测中得到了广泛使用,然而监测结果中还存在如趋势项等难以定量分析的成分。从叶尖计时原理出发,分析了叶尖计时时域信号中存在的成分,研究了转速非线性变化对叶尖计时测量结果的影响规律,提出了有键相叶尖计时信号中误差辨识与修正方法。建立了融合转速变化及气动阻力引起的趋势项的叶尖计时数字模型,通过数值仿真验证了所提方法的准确性,然后利用航空发动机压气机叶片实验台的叶尖计时数据以及动应力数据进行对比验证,结果表明本文方法计算的叶尖位移趋势项与动应变趋势项的相关系数为0.986,具备良好的一致性。对于降低叶尖计时测量结果的不确定性、实现叶片运行状态的全面监测具有重要的工程应用价值。
As an effective method to monitor the vibration parameters of rotating blades,non-contact blade tip timing method has been widely used in aeroengine blade vibration monitoring in recent years.However,there are still some components that are difficult to be quantitatively analyzed in the measurement results,such as trend term.Based on the principle of blade tip timing,the components in the time domain signal of tip timing are analyzed,the influence of nonlinear change of speed on the measurement results is studied,and the error identification and correction method of once per revolution based tip timing signal is proposed.A tip timing digital model integrating the trend term caused by speed change and aerodynamic resistance is established.The accuracy of the proposed method is verified by numerical simulation,and then compared and verified by using the tip timing data and dynamic stress data of aeroengine compressor blade test-rig.The result shows that the correlation coefficient between tip displacement trend term and dynamic strain trend term calculated by the proposed method is 0.986,which has good consistency.This method has important engineering application value in reducing the uncertainty of blade tip timing measurement results and realizing the comprehensive monitoring of blade operation state.
作者
张旭龙
王维民
李天晴
林昱隆
艾信息
王振国
Xulong ZHANG;Weimin WANG;Tianqing LI;Yulong LIN;Xinxi AI;Zhenguo WANG(Beijing Key Laboratory of Health Monitoring Control and Fault Self?recovery for High?end Machinery,Beijing University of Chemical Technology,Beijing100029,China;Key Lab of Engine Health Monitoring?Control and Networking,Beijing University of Chemical Technology,Beijing100029,China)
出处
《航空学报》
EI
CAS
CSCD
北大核心
2023年第5期305-318,共14页
Acta Aeronautica et Astronautica Sinica
基金
国家重点研发计划(2020YFB2010803)
国家自然科学基金重点项目(92160203)
国家自然科学基金(51775030,91860126)。
关键词
叶尖计时
趋势项
变转速
气动阻力
叶片振动
blade tip timing
trend term
variable speed
aerodynamic resistance
blade vibration
