Improved composite structure for aircraft

Details Improved composite structure for aircraft Improved composite structure for aircraft

B - Operations, Transporting

64

C

B64C 1/06 (2006.01)

Patent

CA 2575332

Une structure (2) d'aéronef (1) comporte des parois transversales (3- 8) reliées à des parois longitudinales (9-12) ; les parois (3-12, 18, 18B) comportent chacune deux enveloppes (19) en matériau composite disposées de part et d'autre d'un agencement (20) intermédiaire ; la structure comporte une barre (21) de section cruciforme reliant une paroi transversale à une paroi longitudinale.

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