| 摘要 |
A rib element for aircraft and 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.
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