Aero-engine service life prediction method based on label-free, unbalanced and initial value uncertain data
An aero-engine and data-determining technology, applied in electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as unbalanced initial value, lack of prior knowledge, and imbalance
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[0048] In this embodiment, the civil turbine engine life cycle data set released by NASA's predictive failure prediction research is used, and the FD001 data set is selected. This data set simulates the end-of-life situation of aero-engines caused by the performance degradation of high-pressure compressors of aero-engines. The data set includes training data, test data and RUL of test data. The data set includes 21 sensor measurement variables, including multi-source data types such as temperature, pressure, and rotational speed. The specific sensor symbols, descriptions, and units are shown in Table 1. Furthermore, the dataset contains noise and the initial health state of each engine sample is uncertain.
[0049] Table 1 Description of aero-engine sensor variables
[0050]
[0051]
[0052] The overall process of this method is as follows figure 1 As shown, the specific implementation steps are as follows:
[0053] Step 1. Feature selection of aero-engine multi-sour...
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