| 摘要 |
The invention relates to a rib element for aircraft and to a composite flange for use in aircraft. The rib element (24) and the composite flange (14), manufactured from a composite material, comprise at least two elongated flanges (15, 16, 26) interconnected with one another in a corner (17) provided with a rounded inner corner (18) and a rounded outer corner (19). The corner is reinforced by at least one reinforcing component (20) which covers at least a part of the inner corner. |
