Automotive/Aerospace Synergism in Computer-Aided Composite Processing

911120

04/01/1991

Event
Aerospace Atlantic Conference & Exposition
Authors Abstract
Content
In-mold dielectric cure monitoring techniques pioneered by the aerospace industry were applied to the manufacturing process of LITEFLEX R springs. Real-time data was collected in-situ and used to interpret the progression of cure in an epoxy/fiberglass composite. This information was used to trigger mold pressurization in an attempt to lower void content and improve part appearance.
A microdielectric sensor placed on the mold surface collected temperature and conductivity data that was converted to a cure percentage scale (cure index). The optimum pressurization point for the epoxy system was at approximately 40% conversion. Although results varied somewhat depending on spring geometry, void contents were reduced to less than 1%. Composite shear strength increased 10-15%. Surface appearance was also significantly improved.
Meta TagsDetails
DOI
https://doi.org/10.4271/911120
Pages
10
Citation
Gentry, J., "Automotive/Aerospace Synergism in Computer-Aided Composite Processing," SAE Technical Paper 911120, 1991, https://doi.org/10.4271/911120.
Additional Details
Publisher
Published
Apr 1, 1991
Product Code
911120
Content Type
Technical Paper
Language
English