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Journal of Sandwich Structures and Materials
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Article

The manufacturing procedure for aerospace secondary sandwich structure panels

Duncan A Crump1, Janice M Dulieu-Barton1, and John Savage2*

1 School of Engineering Sciences, University of Southampton, Southampton, UK
2 GE Aviation, Hamble-Le-Rice, Hampshite, UK

* To whom correspondence should be addressed. E-mail: John.Savage3{at}ge.com.


  Abstract

This study provides a detailed consideration of five manufacturing options that are used to produce aerospace sandwich panels used in secondary structure. The structural performance of each of the manufacturing options is considered along with a cost analysis. By considering the traditional preimpregnated (prepreg), autoclave-cured process, the sources of cost have been investigated, and it has been shown that by removing a portion of the large labor content and the autoclave cure, in favor of an oven-only cure, it would be possible to make significant savings. Monitoring the time to manufacture representative full-scale sandwich panels using the five manufacturing options has shown that by using a resin film infusion (RFI) oven cure, a 30% reduction in time to production is possible.<?tlsb> To make an initial assessment of the comparative structural performance of laminates produced using the five manufacturing options, this article also presents results of material quality, in-plane and out-of-plane loading tests. The results of these tests show that the laminates produced using RFI are comparable in quality and performance to laminates produced using the current aerospace industry standard prepreg/autoclave process.

First published on June 10, 2009
Journal of Sandwich Structures and Materials 2009, doi:10.1177/1099636209104531
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