Study on the Dynamic Modeling of the Turbofan Engine

Authors

  • Ri CholUk  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Zhang ZhunHyok  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Kim JaeHun  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Yun HoYong  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Kim KumChol  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Han JongMin  School of Mechanical Technology, KimChaek University of Technology, Pyongyang 950003, Democratic People’s Republic of Korea
  • Zhang Ryong  KimIlSung University, Pyongyang 999093, Democratic People’s Republic of Korea

Keywords:

Turbofan Engine, Mathematical Model, Part Calculation, Dynamic Model

Abstract

The external conditions and internal parameters of aero-engine work vary widely, and there are strict requirements of aerodynamic and strength limitation, so certain control strategies must be adopted to meet the operating requirements of the engine. Engine mathematical model is the core of engine simulation technology, the basis of analyzing engine characteristics, studying its control law, and designing and analyzing the control system. It is also an important condition for the research of integrated flight/propulsion control system. Based on the analysis of the characteristics of turbofan engine components and the thermodynamic calculation process, a component level nonlinear mathematical model of the engine with variable specific heat is established. This model can be used to calculate the steady and dynamic processes of turbofan engines under different control laws. It can also be used as the research object of multivariable control. In this paper, based on mentioning the theoretical basis for making a dynamic model of a turbofan engine, an assumption was made to create a dynamic model. Next, a geometrical structure diagram of a turbofan engine was created to create a dynamic model and the principle of the modeling method was explained. Also, based on the calculation of the characteristics of the turbofan engine and the calculation of the parts, the dynamic equation of the turbofan engine was prepared. The mathematical model of turbofan engine established in this paper has certain practicability and can be used as the basis of engine control research.

References

  1. Shidfar A, Garshasbi M. Mathematical Modeling and Numerical Investigation of Heat Flux at the External Surface of Cylinder of an Internal Combustion Engine J. Biodegradation, 2007, 25(4):515-527.
  2. Campanella A J. Cabin noise mathematical modeling for single engine aircraft J. Journal of the Acoustical Society of America, 1983, 73(S1).
  3. Preetham B S, Anderson M, Richards C. Mathematical modeling of a four-stroke resonant engine for micro and mesoscale applications J. Journal of Applied Physics, 2014, 116(21):422-520.
  4. JK Lytle. The Numerical Propulsion System Simulation: An Advanced Engineering Analysis Tool for Airbreathing Engines J. 2001.
  5. Liu Y, Frederick D K, Decastro J A, et al. User's Guide for the Commercial Modular Aero-Propulsion System Simulation (C-MAPSS): Version 2. 2012.
  6. Chin J C, Csank J T. Tool for the Integrated Dynamic Numerical Propulsion System Simulation (NPSS)/Turbine Engine Closed-Loop Transient Analysis (TTECTrA) User's Guide. , 2016.
  7. Yakinthos K, D Missirlis, Palikaras A, et al. Optimization of the design of recuperative heat exchangers in the exhaust nozzle of an aero engine J. Applied Mathematical Modelling, 2007, 31(11):2524-2541.
  8. Wang B, Zhao H, Ye Z. A Co-modeling Method Based on Component Features for Mechatronic Devices in Aero-engines J. International Journal of Turbo & Jet-Engines, 2016, 34.
  9. Sherbaum V, Erenburg V. Numerical Modeling of Unsteady Oil Film Motion Characteristics in Bearing Chambers: International Journal of Turbo & Jet-Engines J. International Journal of Turbo & Jet-Engines, 2014.
  10. Fei C , Liu H , Li S , et al. Dynamic parametric modeling-based model updating strategy of aeroengine casingsJ. Chinese Journal of Aeronautics, 2021.
  11. Sheng H, Zhang T, Jiang W. Full-Range Mathematical Modeling of Turboshaft Engine in Aerospace J. International Journal of Turbo and Jet Engines, 2015.
  12. Visser W, Kogenhop O, Oostveen M. A Generic Approach for Gas Turbine Adaptive Modeling J. Journal of Engineering for Gas Turbines and Power, 2006.
  13. Mink G, Behbahani A. The AFRL ICF Generic Gas Turbine Engine ModelC// Aiaa/asme/sae/asee Joint Propulsion Conference & Exhibit. 2013.
  14. Visser W P J. Generic Analysis Methods for Gas Turbine Engine Performance: The development of the gas turbine simulation program GSP J. 2015.

IInternational Journal of Scientific Research in Mechanical and Materials Engineering

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Published

2021-04-30

Issue

Volume 5, Issue 2, March-April-2021

Section

Research Articles

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Copyright (c) IJSRMME

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This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
Ri CholUk, Zhang ZhunHyok, Kim JaeHun, Yun HoYong, Kim KumChol, Han JongMin, Zhang Ryong, " Study on the Dynamic Modeling of the Turbofan Engine, IInternational Journal of Scientific Research in Mechanical and Materials Engineering(IJSRMME), ISSN : 2456-3307, Volume 5, Issue 2, pp.27-38, March-April-2021.