| 摘要 |
An aircraft structural component (10) comprises a panel element (12) made of a fibre reinforced composite material and being provided with an opening (18) extending through the panel element (12), a reinforcing element (24) made of a fibre reinforced composite material and being provided with an opening (18) extending through the reinforcing element (24), the two openings being aligned. A bushing (36) extending through the opening (18) provided in the panel element (12) and the opening (30) provided in the reinforcing element (24) and being adapted to receive an attachment device for attaching a load to the aircraft structural component (10), and a connecting element (48) which connects the reinforcing element (24) to the panel element (12) in a region of the panel element (12) adjacent to the opening () extending through the panel element (12) by means of a hook and loop connection. |
