发明名称 PROCEDE DE MISE EN PLACE DES ELEMENTS D'UN PANNEAU AUTO-RAIDI EN COMPOSITE PREIMPREGNE
摘要 <p>Pre-impregnated carbon fiber layers are superimposed to form a base skin (1). One or more reinforcing layers (9) of carbon fiber prepreg, are located and formed on individual U-section plungers (5). These have rounded edges and their lengths, heights and internal widths correspond with dimensions of the U-shaped stiffeners (2) to be manufactured. Longitudinal edges of the layers are turned down (13) over the height of the plungers, forming rib halves (3a, 3b) of the reinforcing ribs. - The plungers are located side-by-side in inverted-U formation. An approximately triangular section (4) or head, is located between the two descending edges (13) which face each other. The entire assembly is compacted, and then inverted through 180 deg. . It is positioned onto the skin, which is laminated-on as a flat, continuous surface, defined by its external face and the meeting of the components described above. The plungers are then retracted</p>
申请公布号 FR2863197(B1) 申请公布日期 2006.03.03
申请号 FR20030014253 申请日期 2003.12.04
申请人 AIRBUS FRANCE 发明人 NAVAS GEORGES;PETETIN JEAN PAUL;FONTAYNE MICHEL;LAFON PIERRE;HELLARD GUY
分类号 B29C70/30;B29C70/34;B29C70/46;B29D24/00 主分类号 B29C70/30
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