Paper Title:
Power Flow Method for Determination of Product Shock Fragility
  Abstract

One of necessary prerequisites to design cushioned package is the determination of product shock fragility, which is so far obtained by means of destructive method on shock testing machines. This paper presents a non-destructive method--power flow method to predict the product fragility. The transport package system was first divided into two subsystems to simplify analysis. The energy of critical component of the product was then calculated by applying a power flow equilibrium equation. And finally, the parameters of the transport package system, such as the input power, the internal loss factor and the coupling loss factor, were discussed.

  Info
Periodical
Chapter
Chapter 6: Engineering Mechanics and Application
Edited by
Di Zheng, Yiqiang Wang, Yi-Min Deng, Aibing Yu and Weihua Li
Pages
1167-1172
DOI
10.4028/www.scientific.net/AMM.101-102.1167
Citation
X. F. Kuang, Z. W. Wang, "Power Flow Method for Determination of Product Shock Fragility", Applied Mechanics and Materials, Vols. 101-102, pp. 1167-1172, 2012
Online since
September 2011
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: P.X. Yi, Shi Yuan Liu, Y.M. Hu, W. Liu
Abstract:As an important means to improve the reliability of complex manufacturing systems and to ensure that they can function better, condition...
863
Authors: Ying Ze Wang
Abstract:This paper is concerned with an analysis of the dynamic characteristics of the high performance launcher—rarefaction wave gun(RAVEN) by...
44
Authors: Wei Zhou, Li Hong Lin, Xiao An Chen
Abstract:Electromechanical coupling effect must be considered in the dynamic analysis of permanent magnet AC servo-driven precision gear transmission...
1375
Authors: Ji Lin
Chapter 3: Electrotechnics and Electrical Machines
Abstract:This paper concerns the power transmissions between two flexible subsystems (i.e., with short-wavelength deformations) coupled by a stiff...
915
Authors: Guo Jun Zhang, Yun Ju Yan
Chapter 4: Mechanics, Thermal and Dynamics Systems, Vibration, Noise, Applied Mechanics and Numerical Simulation Applications
Abstract:The SEA model of hypersonic aircraft is established based on statistical energy analysis (SEA) theory. Three parameters of the SEA model are...
810