共 3 条
Spatial transformation of general sampling-aliasing frequency region for rotating-blade parameter identification with emphasis on single-probe blade tip-timing measurement
被引:10
|作者:
Cao, Jiahui
[1
]
Yang, Zhibo
[1
]
Teng, Guangrong
[2
]
Tian, Shaohua
[2
]
Ye, Guoyong
[3
]
Chen, Xuefeng
[1
]
机构:
[1] Xi An Jiao Tong Univ, Sch Mech Engn, Xian 710049, Peoples R China
[2] Sichuan Gas Turbine Estab Aero Engine Corp China, Mianyang 621000, Peoples R China
[3] Zhengzhou Univ Light Ind, Coll Mech & Elect Engn, Zhengzhou 450002, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Blade-tip timing (BTT);
Extended time-frequency analysis;
Image-feature recognition;
Parameter extraction;
Sampling-aliasing frequency map;
Spatial transformation;
Vibration analysis;
VIBRATION;
SIGNALS;
D O I:
10.1016/j.cja.2022.10.002
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
Blade-health monitoring is intensely required for turbomachinery because of the high fail-ure risk of rotating blades. Blade-Tip Timing (BTT) is considered as the most promising technique for operational blade-vibration monitoring, which obtains the parameters that characterize the blade condition from recorded signals. However, its application is hindered by severe undersampling and stringent probe layouts. An inappropriate probe layout can make most of the existing methods inva-lid or inaccurate. Additionally, a general conflict arises between the allowed and required layouts because of arrangement restrictions. For the sake of economy and safety, parameter identification based on fewer probes has been preferred by users. In this work, a spatial-transformation-based method for parameter identification is proposed based on a single-probe BTT measurement. To present the general Sampling-Aliasing Frequency (SAFE) map definition, the traditional time-fre-quency analysis methods are extended to a time-sampling frequency. Then, a SAFE map is projected onto a parameter space using spatial transformation to extract the slope and intercept parameters, which can be physically interpreted as an engine order and a natural frequency using coordinate transformation. Finally, the effectiveness and robustness of the proposed method are ver-ified by simulations and experiments under uniformly and nonuniformly variable speed conditions. (c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
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页码:220 / 240
页数:21
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