芳纶
蜂巢
超声波传感器
材料科学
凯夫拉
蜂窝结构
刚度(电磁)
复合材料
有限元法
航空航天
复合数
比模量
铝
结构工程
声学
工程类
航空航天工程
物理
纤维
作者
Alena A. Vjuginova,Sergey N. Vjuginov,A. A. Novik
标识
DOI:10.1134/s1063771023601139
摘要
Honeycomb panels made of aluminum and composite materials—aramid, or Kevlar—are widely used in aviation, space, automotive, and other fields due to their unique characteristics: high strength and rigidity, low density, and good thermal insulation properties. However the mechanical processing of products made of honeycomb materials faces several difficulties, and one of the technologies that effectively solves the problems of cutting products made of honeycomb materials is ultrasonic cutting. In this paper, the finite element method is used to study the frequency properties necessary for designing tools for ultrasonic cutting of products made of honeycomb materials with operating frequencies around 20 kHz and various geometric parameters for cutting different variants of honeycomb constructions. The results of analyzing the wave dimensions of specialized ultrasonic triangular and disk-type instruments depending on geometry features are shown, along with the experimental results for a number of developed variants.
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