Lightweight structure especially for an aircraft and method...

B - Operations – Transporting – 64 – C

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Details

B64C 1/00 (2006.01) B32B 15/08 (2006.01) B64F 5/00 (2006.01)

Patent

CA 2473350

A fiber reinforced strip is adhesively bonded to an outwardly facing surface of a reinforcing frame and to an inwardly facing outer skin surface. Such a strip position reduces crack propagation in a lightweight structure particularly in the outer skin adhesively bonded to the reinforcing frame through the strip. For this purpose the fiber reinforced strip is interposed between the outer skin and the frame and adhesively bonded to the outer skin and to the frame. The strip has reinforcing fibers extending in parallel to each other or the reinforcing fibers are woven into a fabric embedded in a synthetic adhesive bonding material. The embedding of the parallel fibers or of the fiber fabric in the bonding material is performed either prior to the bonding or during the bonding of the strip to the outer skin and to the reinforcing frame.

Une bande renforcée de fibres est collée à une paroi orientée vers l'extérieur d'un cadre de renfort et à une surface de revêtement extérieure orientée vers l'intérieur. Cet emplacement de la bande diminue la propagation des fissures dans une structure légère, en particulier dans le revêtement extérieur collé au cadre de renfort au moyen de la bande. Dans cette fin, la bande renforcée de fibres est intercalée entre le revêtement extérieur et le cadre, et elle est collée au revêtement extérieur et au cadre. Cette bande comprend des fibres de renfort parallèles ou bien ces fibres de renfort sont tissées dans un tissu noyé dans une matière synthétique adhésive. L'enrobage des fibres parallèles ou du tissu de fibres dans la matière de liaison est effectué avant le collage ou durant le collage de la bande au revêtement extérieur et au cadre de renfort.

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