火箭推进2009，Vol.35Issue(5)：29-33,5.
涡轮泵环形颗粒阻尼器设计
Design of circular particle damper for turbopump
邓长华 1周云端1
作者信息
- 1. 西安航天动力研究所,陕西,西安,710100
- 折叠
摘要
Abstract
A circular particle damper attached to the turbopump of the liquid rocket engine is designed. The models of the turbopump with and without the particle damper are built with finite element method to evaluate the damping effect on the vibration of the turbopump. In the simulation, the equivalent structural damping ratio is used to describe the damping performance of the particle damper. Numerical results show that the particle damper can reduce the vibration of the turbopump significantly, and has less effect on the dynamic characteristics of the turbopump.关键词
颗粒阻尼器/涡轮泵/减振Key words
particle damper/ turbopump/ damping分类
航空航天引用本文复制引用
邓长华,周云端..涡轮泵环形颗粒阻尼器设计[J].火箭推进,2009,35(5):29-33,5.
