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一种基于增材制造的紧凑型锯齿隔振器

贾梦 王莛葳 戴宁

南京航空航天大学学报(英文版)2025,Vol.42Issue(z1):121-130,10.
南京航空航天大学学报(英文版)2025,Vol.42Issue(z1):121-130,10.DOI:10.16356/j.1005-1120.2025.S.010

一种基于增材制造的紧凑型锯齿隔振器

Compact Zigzag Vibration Isolator Based on Additive Manufacturing

贾梦 1王莛葳 1戴宁1

作者信息

  • 1. 南京航空航天大学机电学院,南京 210016,中国
  • 折叠

摘要

Abstract

Devices on aircraft are subjected to complex environmental excitations that pose risks to their operational safety.Passive vibration isolation techniques are extensively employed due to their advantage of not requiring additional energy sources.This paper introduces a novel metallic vibration isolator based on zigzag structures.The proposed isolator features a compact design and can be manufactured using additive manufacturing techniques,allowing for the integration of structural and functional elements.Firstly,the vibration response of the single-degree-of-freedom(SDOF)system is analyzed.To achieve effective vibration reduction,it is crucial for the isolator's stiffness to be sufficiently low.Secondly,to obtain a structure with high compliance,the traversal algorithm and the finite element method(FEM)are applied.The results confirm that the zigzag structure is a reliable high-compliance configuration.Thirdly,the parametric geometric model of the zigzag structure is developed and its stiffness is calculated.Quasi-static compression experiments validate the accuracy of the calculations.Finally,a specific engineering example is considered,where a zigzag vibration isolator is designed and fabricated.Vibration experiments demonstrate that the zigzag isolator effectively reduces both the stiffness and the fundamental frequency of the vibration system,achieving a vibration isolation efficiency exceeding 60%.

关键词

振动隔离/被动减振/增材制造/锯齿结构/金属隔振器

Key words

vibration isolation/passive isolators/additive manufacturing/zigzag structures/metallic vibration isolator

分类

机械制造

引用本文复制引用

贾梦,王莛葳,戴宁..一种基于增材制造的紧凑型锯齿隔振器[J].南京航空航天大学学报(英文版),2025,42(z1):121-130,10.

基金项目

This work was supported by the Na-tional Key Research and Development Program of China(Nos.2023YFB4603900,2023YFB4603901)and the Na-tional Natural Science Foundation of China(No.52275255). (Nos.2023YFB4603900,2023YFB4603901)

南京航空航天大学学报(英文版)

1005-1120

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