Abstract
In order to realize the rapid response control for turboshaft engine during the process of variable rotor speed, the linear quadratic Gaussian with loop transfer recovery (LQG/LTR) control method for turboshaft engine based on torsional vibration suppression is proposed. Firstly, the two-speed dual clutch transmission model is applied to realize the variable rotor speed of helicopter. Then, based on the state variable model of turboshaft engine, the proper LQG/LTR controller is available. In order to eliminate the limitation of low-order torsional vibration on the bandwidth of LQG/LTR controller, a frequency-domain analysis method for the effect of torsional vibration suppression on LQG/LTR controller performance is developed. Finally, the numerical simulation is conducted to verify the LQG/LTR control for turboshaft engine with variable rotor speed based on torsional vibration suppression. The results show that the bandwidth of the LQG/LTR control loop can increase by 2–3 times under torsional vibration suppression. Meanwhile, when the rotor speed varies continuously by 40%, the overshoot and sag of the power turbine speed can decrease to less than 2% through LQG/LTR controller based on torsional vibration suppression, which achieves the rapid response control of the turboshaft engine.
Highlights
With the wide application of helicopter in various fields, the problems of short flying range, high noise, and limited flight altitude are more obvious
The results showed that this method can significantly improve the sensitivity of turboshaft engine to load and reduce the sag of power turbine speed effectively
In order to compensate for the lack of research on linear quadratic Gaussian with loop transfer recovery (LQG/LTR) control method for turboshaft engine with variable rotor speed based on the torsional vibration suppression, the two-speed dual-clutch transmission model is introduced based on the integrated helicopter/engine model firstly
Summary
With the wide application of helicopter in various fields, the problems of short flying range, high noise, and limited flight altitude are more obvious. It is necessary to develop high-quality control methods for the turboshaft engine with the variable rotor speed based on the torsional vibration suppression.
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