ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Identification method of foreign object impact on blade based on blade tip timing
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)
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.
Shuhui WANG , Weimin WANG , Tianqing LI , Jiale WANG , Zhenyu FU , Ya ZHANG . Identification method of foreign object impact on blade based on blade tip timing[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(20) : 430051 -430051 . DOI: 10.7527/S1000-6893.2024.30051
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, 2019, 38(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 Shock, 2019, 38(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 Communication, 2005, 2(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, 2020, 20(6): 2483-2488. |
ZHANG Q B, LEI X B. Analysis of rotor vibration transient response of fan blade impact[J]. Science Technology and Engineering, 2020, 20(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, 2022, 22(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 Engineering, 2022, 22(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, 2023, 44(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 Sinica, 2023, 44(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 Processing, 2020, 144: 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, 2021, 42(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 Sinica, 2021, 42(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, 2020, 41(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 Technology, 2020, 41(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, 2010, 46(23): 61-67. |
TAN J Y, CHEN X F, HE Z J. Stochastic resonance adaptive detection method for shock signal[J]. Journal of Mechanical Engineering, 2010, 46(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 Processing, 2022, 172: 108977. |
15 | XIONG P, TANG B P, DENG L, et al. Multi-block domain adaptation with central moment discrepancy for fault diagnosis[J]. Measurement, 2021, 169: 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 Processing, 2022, 177: 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 Aeronautics, 2020, 33(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 Vibration, 2022, 520: 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 Control, 2021, 40(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 Processing, 2019, 134: 106321. |
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