Research on the Real-Time Model of Aero-Engine Actuator

Author:

Li Hua Cong1,Zhang Hong An1,Han Xiao Bao1,Fu Jiang Feng1

Affiliation:

1. Northwestern Polytechnical University

Abstract

Since the solving process of hydraulic dynamic simulation is complex and computational ineffectiveness,the aero-engine actuators real-time modeling is presented in this paper. Combined with the precise model, the convergence of the model and flow coefficient is analyzed. The real-time model operates a number of solving processes in one 20ms simulation cycle and the convergence of fix-step algorithm is guaranteed by adjusting the relevant parameters. The simulation shows that the real-time model can improve the computational efficiency with satisfactory real-time performance and precision.

Publisher

Trans Tech Publications, Ltd.

Reference7 articles.

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3. Montazeri-Gh M, Nasiri M, Rajabi M, et al. Actuator-based hardware-in-the-loop testing of a jet engine fuel control unit in flight conditions[J]. Simulation Modelling Practice and Theory, 2012, 21(1): 65-77.

4. KONG Fan-e, CHEN Zhong-ji. Real-Time simulation of Flight Control System Based on RTW and VxWorks[J][J]. Journal of System Simulation, 2007, 19(11): 2455-2457.

5. PENG Kai, FAN Ding, BU Zheng-peng. Failure analysis and parameter optimization for fuel distributor for aeroengine[J]. Journal of propulsion technology, 2011, 32(2): 276-281.

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