Jet Engine Turbine Mechanical Properties Prediction by Using Progressive Numerical Methods
Open Access
Abstract
The propulsion system for an aircraft is one of its most crucial systems; therefore, its reliable work must be ensured during all operational conditions and regimes. Modern materials, techniques and methods are used to ensure this goal; however, there is still room for improvement of this complex system. The proposed manuscript describes a progressive approach for the mechanical properties prediction of the turbine section during jet engine operation using an artificial neural network, and it illustrates its application on a small experimental jet engine. The mechanical properties are predicted based on the measured temperature, pressure and rpm during the jet engine operation, and targets for the artificial neural network are finite element analyses results. The artificial neural network (ANN) is trained using training data from the experimental measurements (temperatures, pressure and rpm) and the results from finite element analyses of the small experimental engine turbine section proposed in the paper. The predicted mechanical stress by ANN achieved high accuracy in comparison to the finite element analyses results, with an error of 1.38% for predicted mechanical stress and correlation coefficients higher than 0.99. Mechanical stress and deformation prediction of the turbine section is a time-consuming process when the finite element method is employed; however, the method with artificial neural network application presented in this paper decreased the solving time significantly. Mechanical structural analyses performed in ANSYS software using finite element modeling take around 30–40 min for one load step. In contrast, the artificial neural network presented in this paper predicts the stress and deformation for one load step in less than 0.00000044 s.Keywords
Funding Information
- Agentúra na Podporu Výskumu a Vývoja (APVV-20-0546, OPII-VA/DP/2021/9.3-01, 313011BWP9)
- Agentúra na Podporu Výskumu a Vývoja (APVV-20-0546, OPII-VA/DP/2021/9.3-01, 313011BWP9)
- Research of an intelligent management logistics system with a focus on monitoring the hygienic safety of the logistics chain (APVV-20-0546, OPII-VA/DP/2021/9.3-01, 313011BWP9)
This publication has 37 references indexed in Scilit:
- Surrogate-based optimization with improved support vector regression for non-circular vent hole on aero-engine turbine diskAerospace Science and Technology, 2020
- Machinability of Rene 65 SuperalloyMaterials, 2019
- Robust Control of Small Turbojet EnginesMachines, 2019
- Adaptive Degradation Prognostic Reasoning by Particle Filter with a Neural Network Degradation Model for Turbofan Jet EngineData, 2018
- Intelligent Situational Control of Small Turbojet EnginesInternational Journal of Aerospace Engineering, 2018
- Failure analysis of an un-cooled turbine blade in an aero gas turbine engineEngineering Failure Analysis, 2017
- An Artificial Neural Network for Analyzing Overall Uniformity in Outdoor Lighting SystemsEnergies, 2017
- Experimental-numerical investigation for predicting erosion in the first stage of an axial compressorPowder Technology, 2017
- Attitude-independent 3-axis Accelerometer Calibration Based on Adaptive Neural networkProcedia Engineering, 2014
- Thermal fatigue failure of fuel spray bars of a jet engine afterburnerEngineering Failure Analysis, 2011