Thermal Expansion Molding Process for Aircraft Composite Structures

800612

04/01/1980

Event
Turbine Powered Executive Aircraft Meeting
Authors Abstract
Content
Thermal expansion molding is a low-cost manufacturing method for fabricating fiber-reinforced-resin composite structures. In its simplest form, the tooling is self-pressurized by thermal expansion of solid “rubber” blocks inside a closed hard mold box. To provide closer control of molding pressure, hollow rubber blocks may be pressurized from an external source. A procedure for sizing castable rubber tools is explained, and several examples of integrally molded complex structures are shown.
Meta TagsDetails
DOI
https://doi.org/10.4271/800612
Pages
16
Citation
Cremens, W., "Thermal Expansion Molding Process for Aircraft Composite Structures," SAE Technical Paper 800612, 1980, https://doi.org/10.4271/800612.
Additional Details
Publisher
Published
Apr 1, 1980
Product Code
800612
Content Type
Technical Paper
Language
English