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Fabricating Composite Hat Stiffened Assemblies Using Flexcauls

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Burrous, D. Wes, author.
Conference Name:
World Aviation Congress & Exposition (1997-10-13 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1997
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
975584
Access Restriction:
Restricted for use by site license

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