METHOD OF MANUFCTURING A CURVED STRUCTURAL ELEMENT MADE OF COMPOSITE MATERIAL AND HAVING A COMPLEX, OPEN CROSS-SECTION
Abstract
A method of manufacturing a curved structural element made of composite material and having a complex, open cross-section is described, in which the structural element is formed by the assembly of components made of composite material. First of all a plurality of flat, fresh components (10, 20, 30; 110, 120, 130) are prepared, each component being constituted by a flat layer of curved fibres previously infused with resin, combined with a pre-impregnated layer with straight fibres. Hot-forming of the flat, raw components is then performed. The hot-formed, fresh components are then assembled in accordance with a predetermined sequence on a polymerization tool. The tool comprises a shaped, inflatable device (42; 42'; 42") astride which a C-shaped raw component is deposited. Finally, the fresh components assembled on the tool are subjected to a polymerization cycle in an autoclave. The inflatable device is inflated by means of the pressure produced in the autoclave in order to apply a predetermined pressure from the inside of the C-shaped fresh component.
Classe Tecnologica
B - Performing operations, transporting
Patent Office
United States Patent and Trademark Office
Numero Deposito
US2011259508
Anno Deposito
2007
Anno Concessione
2011
Inventori Pugliesi
- De Vita Vincenzo
- Iagulli Gianni
Tutti gli inventori
- Sabato Inserra Imparato
- Vincenzo De Vita
- Gianni Iagulli
- Luca Di Tommaso
Titolari pugliesi
- Non ci sono titolari pugliesi
Tutti i titolari
- Alenia Aeronautica S.p.a.
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