A Performance Degradation Evaluation Method of Turbine Engine Based on Stacked Denoising Autoencoder
Patent Information
- Authority / Receiving Office
- CN Β· China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- HARBIN INST OF TECH
- Publication Date
- 2020-06-16
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Abstract
Description
technical field
[0001] The invention belongs to the technical field of engine performance degradation evaluation, and in particular relates to a method for evaluating turbine engine performance degradation based on a stacked denoising self-encoder. Background technique
[0002] As one of the commonly used and important aircraft components, the turbine engine is of great practical significance to ensure its reliable operation for the stable operation of the aircraft and the reduction of maintenance costs. The health factor of a turbine engine, as a characteristic quantity to evaluate its health level, can represent the degradation state or degree of engine health level. It is obtained by mapping different degradation performance variables during operation. The constructed health factor curve characterizes the engine performance degradation process as a monotonous upward or downward trend. By predicting whether the change of the health factor curve reaches the degradation fail...