摘要
介绍了用整体传递矩阵法计算航空发动机多转子相互耦合系统的固有频率特性。该方法克服了传统子结构传递矩阵法不易编制通用计算软件的缺点。同时，用有限元法对支承机匣刚度进行了计算。并以某航空发动机转子系统为例验证了方法的有效性。
The natural frequency characteristics are analysed by the whole Transfer Matrix method for turboengine coupling multi-rotors system. The method prevents the difficulties in developing a com- mon program of the traditional sub-system transfer matrix method. Furthermore, the supporting shell stiffness is calculated by the Finite Element method. The rotor system of an aeroengine is taken as an example to verify the effectiveness of the stated method.
出处
《哈尔滨工业大学学报》
EI
CAS
CSCD
北大核心
1998年第1期32-35,共4页
Journal of Harbin Institute of Technology
基金
航天工业总公司"九五"攻关项目
关键词
整体传递矩阵
临界转速
航空发动机
转子
Whole transfer matrix method
supporting shell stiffness
coupling matrix
natural fre- quency
main mode
