| Citation: | CHEN Lei，QIAO Baijie，AO Chunyan，et al.Uncertainty quantification of rotor blade dynamic strain reconstruction based on blade tip timing［J］.Journal of Aerospace Power，2022，37（7）：1456‑1468. doi: 10.13224/j.cnki.jasp.20210275
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Based on the theory of blade non⁃contact dynamic strain reconstruction，research on the uncertainty quantification method of dynamic strain reconstruction was carried out.According to the variance composition theorem，a model of the blade reconstructed dynamic strain uncertainty for quantitative analysis was established.A simulated rotor blade was used as the research object，and the rotation experiment was carried out.The circumferential Fourier Fitting was used to obtain the amplitude of measuring point under different blade tip timing sensor layouts，and the maximum entropy method was adopted to fit the probability density function of the amplitude distribution，which could be used to determine the uncertainty parameters of the blade⁃tip⁃timing vibration measurement.The finite element model of the blade was modified by combining the Kriging proxy model and the resonant frequency of the test.The displacement⁃strain conversion factors of the key measuring points were obtained，and the uncertainty parameters of the conversion factor considering the uncertainty of the resonance speed and measuring point position were obtained.The mean value，standard uncertainty and inclusion interval of the reconstructed dynamic strain were obtained and compared with the measured data of the strain gauge.Results showed that except for the measuring point
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