Design of a particle damper and experimental study on vibration damping of the pipeline

被引:32
作者
Jin, Gen [1 ,2 ]
Zhao, Zihao [1 ]
Liu, Binbin [3 ]
Cun, Wenyuan [2 ]
Zhao, Zhengda [2 ]
Hou, Minli [2 ]
Chen, Guo [1 ,4 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Civil Aviat, 29 Jiangjun Rd, Nanjing 210016, Jiangsu, Peoples R China
[2] Chengdu Aircraft Ind Grp Co Ltd, Chengdu, Peoples R China
[3] Avic Harbin Aircraft Ind Grp Co Ltd, Harbin, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, Coll Gen Aviat & Flight, Nanjing, Peoples R China
基金
中国国家自然科学基金;
关键词
Aircraft; pipeline; vibration reduction; particle damper; filling rat; SYSTEM;
D O I
10.1177/16878140211044923
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this work, we designed a particle damper which can be conveniently clamped on to a pipeline without affecting the existing structure, showing a promising application in vibration reduction of real aircraft. Based on the designed particle damper, the impact of particle filling rate on the vibration reduction effect, the effect of EDEM simulation on the energy consumption of particles in the vibration process of the damper, and the result of actual vibration reduction test of particle damper installed on hydraulic pipeline were investigated. It is found that the vibration of the pipeline decreases first and then increases with the increase of particle filling rate. The particle filling rate corresponding to the maximum particle energy consumption rate is consistent with that of the minimum pipeline vibration acceleration during the test, that is, from 94.9% to 97.9%. The simulation results are in good agreement with the test results. Moreover, the vibration of the hydraulic pipeline and actual aircraft pipeline are both obviously suppressed after the installation of the particle damper. These results fully demonstrate the effectiveness and practicability of the aircraft pipeline particle damper.
引用
收藏
页数:14
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