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Analysis of structure characteristics of a flying probe tester

Chuji Chen (Hans CNC Technology Co. Ltd, Shenzheng City, People's Republic of China)
Hongyan Shi (Shenzhen University, Guangdong, People's Republic of China)
Fumin Song (Hans CNC Technology Co. Ltd, Shenzheng City, People's Republic of China)

Circuit World

ISSN: 0305-6120

Article publication date: 1 February 2013

169

Abstract

Purpose

The purpose of this paper is to present a method for evaluating the structural dynamic characteristics of a flying probe tester.

Design/methodology/approach

The dynamic characteristics of a flying probe tester framework were analyzed based on a finite element analysis method. First, modal analysis was carried out to characterize the modal parameters of the structure. Second, the harmonic response was analyzed according to the modal analysis and the response curve of the structural system was studied. Finally, transient analysis was conducted to obtain the transient response of the structures at the beginning of the vibration.

Findings

The natural frequency and the response frequency of a natural granite structure was the highest and the transient vibration displacement amplitude was the smallest compared with cast iron and artificial stone structures.

Originality/value

A comprehensive understanding of the dynamic characteristics of the framework of a flying probe tester with three different materials has been achieved. The results of the analyses provide a reference for the framework design of a flying probe tester.

Keywords

Citation

Chen, C., Shi, H. and Song, F. (2013), "Analysis of structure characteristics of a flying probe tester", Circuit World, Vol. 39 No. 1, pp. 31-41. https://doi.org/10.1108/03056121311298927

Publisher

:

Emerald Group Publishing Limited

Copyright © 2013, Emerald Group Publishing Limited

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