Aero-engine degradation state fault diagnosis method based on transfer learning
An aero-engine and fault diagnosis technology, applied in computer-aided design, design optimization/simulation, special data processing applications, etc., can solve problems such as inability to train performance, insufficient fault data, etc., to solve insufficient fault data and improve effectiveness Effect
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[0077] This experiment is a simulation experiment, and the engine model used in the experiment is a certain type of turbofan engine model. The main components include fans, compressors (HPC), combustors, high-pressure turbines (HPT), low-pressure turbines (LPT), and micro-nozzles. Its schematic diagram is as follows image 3 As shown, in order to clarify the meaning of the internal parameters of the engine, some sections in the figure are numbered. Section 2 indicates the fan inlet section, section 22 indicates the fan outlet section, section 3 indicates the compressor outlet section, section 42 indicates the high-pressure turbine outlet section, and section 46 indicates the low-pressure turbine outlet section.
[0078] When the performance of the aero-engine degrades or fails, the health parameters of the engine will change. Therefore, the invention simulates the performance degradation and failure of the engine by changing the health parameters of the engine. Performance d...
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