Fabricating Composite Hat Stiffened Assemblies Using Flexcauls

975584

10/01/1997

Event
World Aviation Congress & Exposition
Authors Abstract
Content
Hat stiffened composite assemblies provide aircraft with a high strength to weight ratio structure. They are however, time consuming and difficult to produce. A new tooling method has been developed that looks promising for fabricating this type of assembly. This new method incorporates a flexible caul (flexcaul) and inflatable mandrels and can be incorporated with the existing bond mold. This method improves the shape and location of the hats while reducing the fabrication time
Meta TagsDetails
DOI
https://doi.org/10.4271/975584
Pages
7
Citation
Burrous, D., "Fabricating Composite Hat Stiffened Assemblies Using Flexcauls," SAE Technical Paper 975584, 1997, https://doi.org/10.4271/975584.
Additional Details
Publisher
Published
Oct 1, 1997
Product Code
975584
Content Type
Technical Paper
Language
English