Method for predicting key performance parameters in transient-state acceleration process of aero-engine based on space reconstruction
A key performance parameter and aero-engine technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of poor generalization ability of the model, insufficient description of aero-engine performance, and large influence of model parameters, etc., to achieve The effect of effective real-time forecasting
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[0053] The specific implementation manners of the present invention will be further described below in conjunction with the accompanying drawings and technical solutions.
[0054] The data used in the present invention are 100 sets of bench test data of a certain type of aero-engine transition state acceleration process provided by a domestic research institute.
[0055] The first step, aero-engine test data preprocessing
[0056] (1) The test data of aero-engine includes the relative speed of compressor inlet PNNC2 g , engine inlet temperature T 2 , engine inlet air pressure P 2 , total compressor outlet pressure P 3 , fuel flow WFB, fan physical speed N f , compressor physical speed N c , the turbine outlet temperature T 5 , the simulated flight height H, and the simulated flight Mach number Ma have a total of 10 sets of parameters;
[0057] (2) Data integration: Read and integrate the txt files of 100 sets of data and store them uniformly to establish a data warehous...
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