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采用磁流变阻尼器的直升机"地面共振"分析
引用本文:王唯,夏品奇.采用磁流变阻尼器的直升机"地面共振"分析[J].南京航空航天大学学报,2003,35(3):264-267.
作者姓名:王唯  夏品奇
作者单位:南京航空航天大学直升机旋翼动力学国家重点实验室,南京,210016
基金项目:航空自然科学基金(01A52006)资助项目.
摘    要:针对磁流变阻尼器的非线性特性,采用能量法得到了磁流变阻尼器的等效线性阻尼。建立了机体平面二自由度和刚性桨叶的“地面共振”分析模型,得出了直升机“地面共振”的稳定性区域。通过分析计算可以得出,磁流变阻尼器能在不同情况下提供“地面共振”所要求的阻尼,达到抑制“地面共振”的目的。

关 键 词:磁流变阻尼器  直升机  地面共振  非线性特性  振动控制
文章编号:1005-2615(2003)03-0264-04
修稿时间:2002年10月14

Ground Resonance Analysis of Helicopter with Magnetorheological Lag Damper
WANG Wei,XIA Pin qi.Ground Resonance Analysis of Helicopter with Magnetorheological Lag Damper[J].Journal of Nanjing University of Aeronautics & Astronautics,2003,35(3):264-267.
Authors:WANG Wei  XIA Pin qi
Abstract:Magnetorheological (MR) damper is the more promising semi active devices for vibration control of structures. External energy required by the adjustable fluid damper is minuscule while speed of its response is on the order of milliseconds. Based on the excellent performance, using the MR damper as the lag damper of rotor can adaptively control the helicopter ground resonance. Due to no linear pro perties of the MR damper, the equivalently linearized damping coefficient is calculated by using the energy method. Through setting an analytical model with couple of rotor and fuselage of helicopter, the stability area of the helicopter ground resonance is obtained. The calculated areas show that the MR lag damper can supply the required damping to control the ground resonance at the different rotating speeds.
Keywords:helicopters  ground resonance  magnetorheological lag damper
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