NDLI: Composite part design based on numerical simulation of the manufacturing process

Content Provider	Springer Nature Link
Author	Mouton, Serge Ledoux, Yann Teissandier, Denis Sébastian, Patrick
Copyright Year	2010
Abstract	In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component.
Starting Page	421
Ending Page	431
Page Count	11
File Format	PDF
ISSN	02683768
Journal	The International Journal of Advanced Manufacturing Technology
Volume Number	55
Issue Number	5-8
e-ISSN	14333015
Language	English
Publisher	Springer-Verlag
Publisher Date	2010-12-31
Publisher Place	London
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Resin transfer molding (RTM) Numerical simulations Failure risk Design for manufacturing and assembly (DFMA) Mechanical Engineering Industrial and Production Engineering Production/Logistics/Supply Chain Computer-Aided Engineering (CAD, CAE) and Design
Content Type	Text
Resource Type	Article
Subject	Industrial and Manufacturing Engineering Control and Systems Engineering Mechanical Engineering Computer Science Applications Software

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