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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Main Authors: Qianjing Chen, Jinquan Huang, Muxuan Pan, Feng Lu
Format: Article
Language:English
Published: MDPI AG 2019-10-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/12/19/3791
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spelling 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
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