方位(导航)
转子(电动)
控制理论(社会学)
瞬态(计算机编程)
刚度
固有频率
阻尼器
直升机旋翼
瞬态响应
振动
频率响应
工程类
机械
结构工程
计算机科学
物理
声学
机械工程
操作系统
控制(管理)
电气工程
人工智能
作者
Oscar C. De Santiago,Luis San Andrés
摘要
A simple procedure, with potential as a field resource, for identification of bearing support parameter from recorded transient rotor responses due to impact loads follows. The method is applied to a test rotor supported on a pair of mechanically complex bearing supports, each comprising a tilting pad bearing in series with an integral squeeze film damper. Identification of frequency dependent bearing force coefficients is good at a rotor speed of 2,000 rpm. Stiffness coefficients are best identified in the low frequency range (below 25 Hz) while damping coefficients are best identified in the vicinity of the first natural frequency (48 Hz) of the rotor bearing system. The procedure shows that using multiple-impact frequency averaged rotor responses reduces the variability in the identified parameters. The identification of frequency-dependent force coefficients at a constant rotor speed is useful to assess rotor-bearing system stability.
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