A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine
Nonlinear component level model (NCLM) is a widely used model for aeroengines. However, it requires iterative calculation and is, therefore, time-consuming, which restricts its real-time application. This study aims at developing a simplified real-time modeling approach for turbofan engines. A mecha...
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doaj-adcb7778c5d74b7fb2cb899a1c7f95b42020-11-25T00:46:04ZengMDPI AGEnergies1996-10732019-10-011219379110.3390/en12193791en12193791A Novel Real-Time Mechanism Modeling Approach for Turbofan EngineQianjing Chen0Jinquan Huang1Muxuan Pan2Feng Lu3Jiangsu Province Key Laboratory Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaJiangsu Province Key Laboratory Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaJiangsu Province Key Laboratory Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaJiangsu Province Key Laboratory Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaNonlinear component level model (NCLM) is a widely used model for aeroengines. However, it requires iterative calculation and is, therefore, time-consuming, which restricts its real-time application. This study aims at developing a simplified real-time modeling approach for turbofan engines. A mechanism modeling approach is proposed based on linear models to avoid the iterative calculation in NCLM so as to effectively reduce the computational complexity. Linear local models, of which the outputs are the solution of the balance equations in NCLM, are established at the ground operating points and are combined into a linear parameter varying (LPV) state-space model. Then, the model is extended throughout the full flight envelope in a polytopic expression and is integrated with the flow path calculation to obtain satisfactory real-time performance. In order to ensure the accuracy of the integrated model, the upper bound of convergence residual of the iteration is strictly set and consideration on the interpolation method is taken. The simulation results demonstrate that the integrated model requires much less computational resources than the NCLM does. Meanwhile, it maintains an acceptable accuracy performance and, therefore, is suitable for real-time application.https://www.mdpi.com/1996-1073/12/19/3791turbofan enginenonlinear component level modellinear parameter varying modelreal-time model |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Qianjing Chen Jinquan Huang Muxuan Pan Feng Lu |
spellingShingle |
Qianjing Chen Jinquan Huang Muxuan Pan Feng Lu A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine Energies turbofan engine nonlinear component level model linear parameter varying model real-time model |
author_facet |
Qianjing Chen Jinquan Huang Muxuan Pan Feng Lu |
author_sort |
Qianjing Chen |
title |
A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine |
title_short |
A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine |
title_full |
A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine |
title_fullStr |
A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine |
title_full_unstemmed |
A Novel Real-Time Mechanism Modeling Approach for Turbofan Engine |
title_sort |
novel real-time mechanism modeling approach for turbofan engine |
publisher |
MDPI AG |
series |
Energies |
issn |
1996-1073 |
publishDate |
2019-10-01 |
description |
Nonlinear component level model (NCLM) is a widely used model for aeroengines. However, it requires iterative calculation and is, therefore, time-consuming, which restricts its real-time application. This study aims at developing a simplified real-time modeling approach for turbofan engines. A mechanism modeling approach is proposed based on linear models to avoid the iterative calculation in NCLM so as to effectively reduce the computational complexity. Linear local models, of which the outputs are the solution of the balance equations in NCLM, are established at the ground operating points and are combined into a linear parameter varying (LPV) state-space model. Then, the model is extended throughout the full flight envelope in a polytopic expression and is integrated with the flow path calculation to obtain satisfactory real-time performance. In order to ensure the accuracy of the integrated model, the upper bound of convergence residual of the iteration is strictly set and consideration on the interpolation method is taken. The simulation results demonstrate that the integrated model requires much less computational resources than the NCLM does. Meanwhile, it maintains an acceptable accuracy performance and, therefore, is suitable for real-time application. |
topic |
turbofan engine nonlinear component level model linear parameter varying model real-time model |
url |
https://www.mdpi.com/1996-1073/12/19/3791 |
work_keys_str_mv |
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