Development and testing of a discrete coil magnetostrictive actuator

被引:0
|
作者
Wang, Yanwen [1 ]
Zhu, Yuchuan [1 ]
Chen, Long [1 ]
Ling, Jie [1 ]
Zhang, Mingming [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Mech & Elect Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
discrete coil; magnetostrictive actuator; servo amplifier; experimental validation; ACTIVE CONTROL; DESIGN; COMBUSTOR; SYSTEMS; MODEL;
D O I
10.1088/1361-665X/ad6382
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Active combustion control (ACC) technology is an effective measure for suppressing the combustion oscillation of aero-engines. The magnetostrictive actuator is the most suitable choice for the ACC actuator due to its excellent high-frequency characteristics and high-temperature resistance. In order for the magnetostrictive actuator to produce high-frequency displacement, the constant current driver must have sufficient power, which results in a larger mass of the driver. A solution is to use multi-channel and low-power constant current driver. Therefore, the coil of the magnetostrictive actuator is axially dispersed and driven by two four-channel servo amplifiers. The driver's mass is significantly reduced while maintaining the same electromagnetic conversion effect. In addition, an analytical model of a discrete coil magnetostrictive actuator is established, and a series of experiments are conducted. The maximum hysteresis error of output displacement at 200 Hz is reduced by 15.2%. Furthermore, under PID closed-loop control, the root mean square (RMS) error is less than 2% when tracking a 10 Hz sinusoidal displacement with coil switching drive.
引用
收藏
页数:14
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