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Modeling and Simulation of Closed-Loop Control Circuit of Aircraft Fuel Metering Valve

  • Xudong ShiEmail author
  • Shaoshuai Yuan
  • Yakun Wang
  • Xu Wang
Conference paper
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 582)

Abstract

The fuel metering valve is an important part of the aircraft fuel system and it controls the supply of metered fuel. In this paper, the closed-loop control principle of fuel metering valve is analyzed and the closed-loop control circuit of certain aero engine fuel metering valve is modeled and simulated by MATLAB/Simulink simulation software. The function of the Engine Electronic Controller (EEC) controls the opening of metering valve is simulated by establishing a model. A new idea is proposed to study the problem of the accessory limit value in the aircraft component maintenance manual through model simulation and the impact of the accessory limit value on the fuel metering valve is obtained.

Keywords

MATLAB/simulink Modeling Simulation Limit value Fuel metering valve Closed-loop control 

Notes

Acknowledgements

The research is supported by the Important and Specific Projects of Civil Aviation Science and Technology Project (Grant No. MHRD20140104). The research is supported by the Innovation Team Cultivation Plan of Colleges and Universities in Tianjin (TD13-5071).

References

  1. 1.
    Yang, Y., Lu, Q.: The research of dynamic modeling and analysis of commercial engine fuel-metering unit. Manuf. Autom. 38(06), 106–110 + 130 (2016)Google Scholar
  2. 2.
    Afiz, I.A., Cunliffe, R., Alukaidey, T.: Mathematical modeling and simulation of a Twin-engine aircraft fuel system using matlab-simulink. Int. J. Control Sci. Eng. 8(1), 1–12 (2018)Google Scholar
  3. 3.
    Zeng, D., Wang, W., Pei, D., Xu, M.: Fuel scavenger contour performance analysis of fuel metering devices. Aero Eng. 36(06), 23–25 + 38 (2010)Google Scholar
  4. 4.
    Yu, L., Zhifeng, Y.E.: AMESim modeling of aero-engine fuel metering device. Mod. Mach. 5, 26–29 (2014)Google Scholar
  5. 5.
    Kang, Y., Zhao, L., Yao, L.: Fault diagnosis and model predictive fault tolerant control for stochastic distribution collaborative systems. IJMIC 30, 30–37 (2018)CrossRefGoogle Scholar
  6. 6.
    Feng, J., Gao, Q., Guan, w., He, Z.: Mathematical modelling and backstepping adaptive sliding mode control for multi-stage hydraulic cylinder. IJMIC 30, 322–332 (2018)CrossRefGoogle Scholar
  7. 7.
    Sharan, A.S., Hiremath, S.S., Venkatesha, C.S., Karunanidhi, S.: Investigation on the critical parameters affecting the working design dynamics of a torque motor employed in an electro-hydraulic servovalve. Simul. Trans. Soc. Model. Simul. Int. 95(1), 31–49 (2019)Google Scholar
  8. 8.
    Mesropyan, A.V., Sharipov, R.R.: Mathematical modeling of transient processes in the jet pipe servo actuator with a dual-mode controller. Ufa Procedia Eng. 150, 168–172 (2016)CrossRefGoogle Scholar
  9. 9.
    Zhang, L., Chen, K., Wu ,W., Zhan, C.: Modeling and dynamic characteristics simulation of three-stage electro-hydraulic servo valve with jet pipe. Hydraul. Pneumatics 6, 66–72 (2018)Google Scholar
  10. 10.
    Ren, H., Li, W., Zhu, T., Wang, Y., Jiang, X.: The simulation modeling research of linear variable differential transformer displacement sensor. J. Astronaut. Metrol. 33(06), 20–25 (2013)Google Scholar

Copyright information

© Springer Nature Singapore Pte Ltd. 2020

Authors and Affiliations

  • Xudong Shi
    • 1
    Email author
  • Shaoshuai Yuan
    • 1
  • Yakun Wang
    • 1
  • Xu Wang
    • 2
  1. 1.College of Electronic Information and AutomationCivil Aviation University of ChinaTianjinChina
  2. 2.Aircraft Maintenance and Engineering Corporation, Beijing (AMECO)BeijingChina

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