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整机瞬态动力特性计算及稳定性分析
ANALYSIS OF TRANSIENT DYNAMIC CHARACTERISTICS AND STABILITY OF AEROENGINE
【摘要】 采用子结构传递矩阵—模态综合法研究了航空发动机整机的瞬态动力特性及稳定性。分析了各种因素(突加不平衡大小及位置、转速、油膜间隙等)对瞬态响应和稳定性的影响规律,得到一些有价值的结论。
【Abstract】 Transient dynamic characteristics and stability of a rotor-support-casing system in an aeroengine are analyzed by means of substructure transfer matrix-modal synthetic method.The effects of various sudden unbalance levels,radial oil film clearances of damper and different rotor speeds on the transient response of the entire engine system are investigated and some valuable conclusions have been drawn.The substructure transfer matrix-modal synthetic method discussed in the paper is available in theory and practice.
- 【文献出处】 航空动力学报 ,JOURNAL OF AEROSPACE POWER , 编辑部邮箱 ,1996年01期
- 【分类号】V231
- 【被引频次】2
- 【下载频次】105