An aircraft structural component comprising a panel element made of a fiber reinforced composite material and provided with an opening extending fully through the panel element. A reinforcing element made of a fiber reinforced composite material has an opening extending through the reinforcing element from a first surface to a second surface of the reinforcing element. The opening extending through the reinforcing element is aligned with the opening extending through the panel element. A bushing extends through the opening provided in the panel element and the opening provided in the reinforcing element and is adapted to receive an attachment device for attaching a load to the aircraft structural component. A connecting element connects the reinforcing element to the panel element in a region of the panel element adjacent to the opening extending through the panel element by means of a hook and loop connection.
Locally reinforced aircraft structural component
2016-07-12
Patent
Elektronische Ressource
Englisch
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