材料工程与机械制造

基于叶尖计时的叶片外物打击辨识方法

  • 王树慧 ,
  • 王维民 ,
  • 李天晴 ,
  • 王珈乐 ,
  • 付振宇 ,
  • 张娅
展开
  • 1.北京化工大学 高端机械装备健康监控与自愈化北京市重点实验室,北京 100029
    2.北京化工大学 高端压缩机及系统技术全国重点实验室,北京 100029
.E-mail: wwm@mail.buct.edu.cn

收稿日期: 2023-12-29

  修回日期: 2024-01-23

  录用日期: 2024-02-21

  网络出版日期: 2024-03-11

基金资助

国家自然科学基金重点项目(92160203);联合基金项目(U1808214)

Identification method of foreign object impact on blade based on blade tip timing

  • Shuhui WANG ,
  • Weimin WANG ,
  • Tianqing LI ,
  • Jiale WANG ,
  • Zhenyu FU ,
  • Ya ZHANG
Expand
  • 1.Beijing Key Laboratory of Health Monitoring and Self-recovery for High-end Mechanical Equipment,Beijing University of Chemical Technology,Beijing  100029,China
    2.State Key Laboratory of High-end Compressor and System Technology,Beijing University of Chemical Technology,Beijing  100029,China

Received date: 2023-12-29

  Revised date: 2024-01-23

  Accepted date: 2024-02-21

  Online published: 2024-03-11

Supported by

Key Program of National Natural Science Foundation of China(92160203);Joint Fund Project of China(U1808214)

摘要

外物打击是影响叶片安全运行的重要事件,打击事件的在线辨识有利于巨大灾难事故的提前预警。针对叶片服役过程中振动数据量大,且需要快速、准确地在线辨识打击事件的迫切需求,提出了一种利用峭度与振幅矩联合判据(KAM-BTT)的多工况下叶片外物打击辨识及打击时刻定位方法。基于叶尖计时法,只需要单个传感器即可实现。构建了考虑叶片安装误差、叶片失谐及传感器安装误差的外物打击振动响应模型,并进行了打击模拟,提出了基于叶片模型参数的外物打击辨识参数阈值获取方法。搭建了外物打击实验装置,完成了多转速下的外物打击辨识验证。实验结果表明,提出的打击辨识方法能凭借单传感器在0.047 s内实现打击事件的识别,为在线预警和数据管理提供了研究基础。

本文引用格式

王树慧 , 王维民 , 李天晴 , 王珈乐 , 付振宇 , 张娅 . 基于叶尖计时的叶片外物打击辨识方法[J]. 航空学报, 2024 , 45(20) : 430051 -430051 . DOI: 10.7527/S1000-6893.2024.30051

Abstract

Foreign Object Impact (FOI) is an important event that affects the safe operation of blades, and the online identification of FOI events is conducive to the early warning of huge disasters. To solve the urgent need of a large amount of vibration data during the service of the blade and the need to quickly and accurately identify the FOI event online, a method for the identification of FOI events and the location of the impact moment of the blade under multiple working conditions is proposed, using the joint criterion of Kurtosis and Amplitude Moment (KAM-BTT). This method is based on the blade tip timing method, and requires only a single sensor. In this paper, a foreign object impact vibration response model considering the blade installation error, blade detuning and sensor installation error is constructed, the FOI simulation is carried out, and a method for obtaining the threshold of foreign object impact identification parameters based on the blade model parameters is proposed. The experimental device for FOI was set up, and the verification of FOI identification at multiple speeds was completed. Experimental results show that the KAM-BTT method proposed in this paper can realize the identification of FOI events within 0.047 s with a single sensor, which provides a research basis for online early warning and data management.

参考文献

1 冯振宇, 霍雨佳, 裴惠, 等. 明胶鸟弹撞击力传感器试验及数值建模方法研究[J]. 振动与冲击201938(12): 206-212.
  FENG Z Y, HUO Y J, PEI H, et al. An experiment and numerical modeling method of gelatin bird striking on force sensors[J]. Journal of Vibration and Shock201938(12): 206-212 (in Chinese).
2 VOIGT P, VOIGT M, MAILACH R, et al. A novel methodology for detecting foreign object damage on compressor blading[C]∥ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. 2019.
3 TURSO J A, LITT J S. A foreign damage event detector data fusion system for turbofan engines[J]. Journal of Aerospace Computing, Information, and Communication20052(7): 291-308.
4 CHANA K S, CARDWELL D N. The use of eddy current sensor based blade tip timing for FOD detection[C]∥ASME Turbo Expo: Power for Land, Sea, & Air. 2008.
5 CARDWELL D N, CHANA K S, Russhard P. The use of eddy current sensors for the measurement of rotor blade tip timing: sensor development and engine testing[C]∥ASME Turbo Expo 2008: Power for Land, Sea, and Air. 2008.
6 张强波, 雷晓波. 风扇叶片外物撞击瞬间转子振动响应分析[J]. 科学技术与工程202020(6): 2483-2488.
  ZHANG Q B, LEI X B. Analysis of rotor vibration transient response of fan blade impact[J]. Science Technology and Engineering202020(6): 2483-2488 (in Chinese).
7 陶冶, 张帅. 基于叶片应变测量的航空发动机风扇外物撞击监测识别[J]. 科学技术与工程202222(3): 1286-1291.
  TAO Y, ZHANG S. Foreign object impact monitoring and identification of aero engine fan based on blade strain measurement[J]. Science Technology and Engineering202222(3): 1286-1291 (in Chinese).
8 欧阳涛. 基于叶尖定时的旋转叶片振动检测及参数辨识技术[D]. 天津: 天津大学, 2011.
  OUYANG T. Rotating blade vibration detection and parameters identification technique using blade tip-timing[D]. Tianjin: Tianjin University, 2011 (in Chinese).
9 张旭龙, 王维民, 李天晴, 等. 变转速工况下叶尖计时信号趋势项解析及验证[J]. 航空学报202344(5): 426980.
  ZHANG X L, WANG W M, LI T Q, et al. Analysis and verification of trend term of blade tip timing signal under variable speed working condition[J]. Acta Aeronautic et Astronautica Sinica202344(5): 426980 (in Chinese).
10 WANG W M, HU D F, LI Q H, et al. An improved non-contact dynamic stress measurement method for turbomachinery rotating blades based on fundamental mistuning model[J]. Mechanical Systems and Signal Processing2020144: 106851.
11 张帅, 张强波, 张霞妹. 基于方差分析的航空发动机风扇叶片外物撞击识别[J]. 航空学报202142(5): 524196.
  ZHANG S, ZHANG Q B, ZHANG X M. Identification of foreign object impact on aero-engine fan blades with varience analysis[J]. Acta Aeronautic et Astronautica Sinica202142(5): 524196 (in Chinese).
12 张帅, 雷晓波, 张霞妹, 等. 基于统计特征的航空发动机风扇外物撞击检测[J]. 推进技术202041(10): 2325-2331.
  ZHANG S, LEI X B, ZHANG X M, et al. Foreign object impact detection of aero-engine fan based on statistical characteristics[J]. Journal of Propulsion Technology202041(10): 2325-2331 (in Chinese).
13 谭继勇, 陈雪峰, 何正嘉. 冲击信号的随机共振自适应检测方法[J]. 机械工程学报201046(23): 61-67.
  TAN J Y, CHEN X F, HE Z J. Stochastic resonance adaptive detection method for shock signal[J]. Journal of Mechanical Engineering201046(23): 61-67 (in Chinese).
14 ZHAO N Y, ZHANG J J, MA W S, et al. Variational time-domain decomposition of reciprocating machine multi-impact vibration signals[J]. Mechanical Systems and Signal Processing2022172: 108977.
15 XIONG P, TANG B P, DENG L, et al. Multi-block domain adaptation with central moment discrepancy for fault diagnosis[J]. Measurement2021169: 108516.
16 WANG W M, CHEN K, ZHANG X L, et al. A novel method to improve the precision of BTT under rapid speed fluctuation conditions[J]. Mechanical Systems and Signal Processing2022177: 109203.
17 WANG W M, ZHANG X L, HU D F, et al. A novel none once per revolution blade tip timing based blade vibration parameters identification method[J]. Chinese Journal of Aeronautics202033(7): 1953-1968.
18 NIU G Y, DUAN F J, LIU Z B, et al. Identification of the excitation source’s circumferential position for rotating blades based on vibration phase[J]. Journal of Sound and Vibration2022520: 116628.
19 REN S Q, XIANG X R, ZHAO Q J, et al. Research on an active control method of rotor blade synchronous vibration based on additional secondary excitation forces[J]. Journal of Low-Frequency Noise, Vibration and Active Control202140(4): 2077-2093.
20 CHEN K, WANG W M, ZHANG X L, et al. New step to improve the accuracy of the blade tip timing method without once per revolution[J]. Mechanical Systems and Signal Processing2019134: 106321.
文章导航

/