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STIFFENED CASING FOR AN AIRCRAFT OR SPACECRAFT WITH A LAMINATE STRINGER OF HIGH RIGIDITY AND CORRESPONDING LAMINATE STRINGER
STIFFENED CASING FOR AN AIRCRAFT OR SPACECRAFT WITH A LAMINATE STRINGER OF HIGH RIGIDITY AND CORRESPONDING LAMINATE STRINGER
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机译:具有高刚度叠层绞合器和相应叠层绞合器的飞机或太空船的加筋壳体
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摘要
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).
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