Aeroengine Performance Modeling Method Based on Self-tuning Wiener Model
An aero-engine and Wiener model technology, applied in neural learning methods, biological neural network models, design optimization/simulation, etc., can solve the problems affecting the dynamic performance of the model, low efficiency of the Wiener model structure parameters and output weights, etc. The effect of reducing computational time, accurate dynamic performance estimation, generalization ability and efficiency improvement
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[0059] The technical solution of the present invention will be described in further detail below in conjunction with the accompanying drawings and corresponding embodiments:
[0060] The main components of a turbofan engine include intake, fan, compressor, combustion chamber, high-pressure turbine, low-pressure turbine, external duct, mixing chamber, tail nozzle, etc. The engine speed is an important parameter representing the working state of the turbofan engine. The time constant value of the self-tuning Wiener model is affected by the operating point parameters of the engine system and some other parameters.
[0061] The construction flowchart of the self-adjusting Wiener model in the embodiment is as follows figure 1 As shown, the turbofan engine component-level model (GGTS, referred to as the turbofan engine component-level model) provides test and training data for the performance model, and the quasi-amplitude modulated pseudo-random binary signal (QAPRBS) is used as th...
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