Rapid Adhesive Induction Bonding of Pultruded Aerospace Structures

881210

08/01/1988

Event
1988 Conference and Exposition on Future Transportation Technology
Authors Abstract
Content
Joining advanced composite materials is one of the greatest obstacles to proliferating their use in aerospace structures. Another hindrance is the high cost of manufacturing advanced composite structures using conventional methods. The present trend in both the automotive and aerospace industries is lighter weight, energy efficient structures. In the aerospace community, the use of advanced composite structures has the potential for weight reductions of 35 to 40 percent as compared with the use of conventional aluminum alloys. However, this advantage is offset by the higher cost of manufacturing in using conventional composite technology.
This paper identifies pultrusion and induction bonding as potential methods for manufacturing lightweight high-strength advanced composite structures.
Meta TagsDetails
DOI
https://doi.org/10.4271/881210
Pages
12
Citation
Wilson, M., Buckley, J., Fox, R., and Johnson, G., "Rapid Adhesive Induction Bonding of Pultruded Aerospace Structures," SAE Technical Paper 881210, 1988, https://doi.org/10.4271/881210.
Additional Details
Publisher
Published
Aug 1, 1988
Product Code
881210
Content Type
Technical Paper
Language
English