摘要
推导了基于经典梁的传递矩阵,用传递矩阵法分析了直升机水平传动轴的稳态不平衡响应。研究了粘弹性减振器的刚度和阻尼对水平传动轴系各元件一阶共振峰值的影响。结果表明,降低支承刚度,轴段的一阶共振峰值减小,支承处的振幅增大;增加支承阻尼,轴系中各元件的一阶共振峰值减小。减振器不仅提高了传动轴系的安全裕度,还减小了轴系的一阶共振峰值。
The transfer matrix is derived according to the classical beam theory. The steady-state unbalance response is analyzed by the transfer matrix method. The effects of the viscoelastic damper' s stiffness and damping on the drive shaft system' s first-order resonance amplitude peak are researched on. The results show that first-order amplitude resonance peak of the shafts reduces with the decrease in the supports' stiffness and its amplitude increases. The amplitude of shaft system decreases with the supports' damping increasing. The damper is used not only to improve the safety margin of the transmission shaft system, but also reduces the first critical speed amplitude.
出处
《机械制造与自动化》
2012年第6期7-11,共5页
Machine Building & Automation
基金
南京航空航天大学直升机专项基金(NP2011026)
江苏省普通高校研究生科研创新计划资助项目(CXZZ11-0199)
关键词
传递矩阵法
传动轴系
稳态不平衡响应
刚度
阻尼
transfer matrix method
drive shaft system
steady-state unbalance response
stiffness
damping