Stiffened casing for an aircraft or spacecraft with a...

B - Operations – Transporting – 32 – B

Patent

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Details

B32B 15/14 (2006.01) B32B 15/20 (2006.01) B64C 1/06 (2006.01) B64C 1/12 (2006.01)

Patent

CA 2662141

The present invention provides a casing structure of low weight provided with a laminate stringer of high rigidity. The stringer has the form of a laminate with a plurality of metallic layers (Sl, S3, S5, S7) and at least one synthetic fibre layer (S2, S4, S6), which is produced at least partially from Zylon fibres, provided between two metallic layers (Sl, S3, S5, S7).

La présente invention concerne une structure légère formant carter, comprenant une lisse stratifiée d'une grande rigidité. La lisse a la forme d'un stratifié composé d'une pluralité de couches métalliques (S1, S3, S5, S7), et d'au moins une couche de fibres synthétiques (S2, S4, S6), qui est produite au moins partiellement à partir de fibres de Zylon et qui est placée entre deux couches métalliques (S1, S3, S5, S7).

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