Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type

In some microelectronic products, one or several components can be idealized as simply supported beam type and viewed as vulnerable elements or critical component due to the fact that they are destroyed easily under impact loadings. The composite cushioning structure made of expanded polyethylene (E...

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Main Authors: Fu-de Lu, De Gao
Format: Article
Language:English
Published: SAGE Publishing 2014-04-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1155/2014/159576
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spelling doaj-d7fd901a2e364b57a99b4925571d11132020-11-25T03:24:08ZengSAGE PublishingAdvances in Mechanical Engineering1687-81322014-04-01610.1155/2014/15957610.1155_2014/159576Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam TypeFu-de Lu0De Gao1 Zhejiang Provincial Key Lab of Part Rolling Technology, Ningbo 315100, China Zhejiang Provincial Key Lab of Part Rolling Technology, Ningbo 315100, ChinaIn some microelectronic products, one or several components can be idealized as simply supported beam type and viewed as vulnerable elements or critical component due to the fact that they are destroyed easily under impact loadings. The composite cushioning structure made of expanded polyethylene (EPE), and expanded polystyrene (EPS) was utilized to protect the vulnerable elements against impact loadings during transportation. The vibration equations of composite cushioning system were deducted and virtual mass method was applied to predict impact behavior of critical component. Numerical results indicate that virtual mass method is appropriate for computing impact response of composite cushioning system with vulnerable element of simply supported beam type, which is affirmed by the fact that the impact responses of structure element in terms of velocity- and displacement-time curves are almost unchanged when virtual mass is smaller than a certain value. The results in this paper make it possible for installation of packaging optimization design.https://doi.org/10.1155/2014/159576
collection DOAJ
language English
format Article
sources DOAJ
author Fu-de Lu
De Gao
spellingShingle Fu-de Lu
De Gao
Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
Advances in Mechanical Engineering
author_facet Fu-de Lu
De Gao
author_sort Fu-de Lu
title Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
title_short Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
title_full Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
title_fullStr Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
title_full_unstemmed Impact Responses of Composite Cushioning System considering Critical Component with Simply Supported Beam Type
title_sort impact responses of composite cushioning system considering critical component with simply supported beam type
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8132
publishDate 2014-04-01
description In some microelectronic products, one or several components can be idealized as simply supported beam type and viewed as vulnerable elements or critical component due to the fact that they are destroyed easily under impact loadings. The composite cushioning structure made of expanded polyethylene (EPE), and expanded polystyrene (EPS) was utilized to protect the vulnerable elements against impact loadings during transportation. The vibration equations of composite cushioning system were deducted and virtual mass method was applied to predict impact behavior of critical component. Numerical results indicate that virtual mass method is appropriate for computing impact response of composite cushioning system with vulnerable element of simply supported beam type, which is affirmed by the fact that the impact responses of structure element in terms of velocity- and displacement-time curves are almost unchanged when virtual mass is smaller than a certain value. The results in this paper make it possible for installation of packaging optimization design.
url https://doi.org/10.1155/2014/159576
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