Torsional vibration analysis of helicopter power transmission system by the multi-shaft transfer matrix method
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Torsional vibration analysis of helicopter power transmission system by the multi-shaft transfer matrix method
Vol. 23, Issue 10, (2008)
作者机构:
1. 北京航空航天大学 能源与动力工程学院,北京,100191
2. 重庆大学 机械传动国家重点实验室,重庆,100044
作者简介:
基金信息:
DOI:
CLC:
Published:2008
稿件说明:
移动端阅览
WANG Jian-jun, MAO Zhen-zhong, QING Li-wei, et al. Torsional vibration analysis of helicopter power transmission system by the multi-shaft transfer matrix method[J]. 2008, 23(10).
DOI:
WANG Jian-jun, MAO Zhen-zhong, QING Li-wei, et al. Torsional vibration analysis of helicopter power transmission system by the multi-shaft transfer matrix method[J]. 2008, 23(10).DOI:
Torsional vibration analysis of helicopter power transmission system by the multi-shaft transfer matrix method
The multi-shaft transfer matrix method(TMM) with differential gear mesh and the torsional vibration characteristics of the helicopter power system have been investigated.Firstly
the analytical model for the helicopter power system was built by the transfer matrix method.Next
the 'mesh transfer matrix' for the two-shaft and three-shaft gear pair
and the planetary gear pair were established using transfer matrix method.Then the torsional vibration characteristics of the helicopter power transmission system were obtained using the multi-shaft transfer matrix method.Lastly
the natural frequency and vibration mode properties was discussed