| 摘要 |
Device for transferring in an stiffened skin of an aircraft component made of a composite material the load of an stringer (16) to the skin (11) in a stringer run-out zone, the stringer (16) being configured by a web (31) and a foot (33), comprising two brackets (40, 40′) configured as unitary parts by webs (41, 41′) to be joined to each side of the stringer web (31) in said run-out zone and feet (43, 43′) having a first section (45, 45′) to be joined to each side of the stringer foot (33) in said run-out zone and a second section (47, 47′) to be joined to the skin (11). An aircraft component made of a composite material using said device in the stringer run-outs |
