| 摘要 |
A device for protecting a front spar structure (12) of a central casing (13) of an aircraft wing and equipment (14) located in said wing. The device comprises a shielding surface (222) extending along the front of a front spar of a central casing (13), from the intersection surface (3) between the wing and the fuselage delimited by the wing root, transversally to this intersection surface (3), up to a first rib of the central casing (13) partially surrounding the equipment (14). The device thus protects the equipment (14) located in the zone between the wing root and the first rib of the central casing (13) of the wing. |
