TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR MANUFACTURING A TRAILING EDGE SYSTEM

The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12), a trailing edge movable (20) which is movably coupled to the wing structure (12), and a first flexible panel element (30) which seals a gap (21) between an outer surface (16) of the wing structure...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Andreani, Luc, Lorenz, Florian
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12), a trailing edge movable (20) which is movably coupled to the wing structure (12), and a first flexible panel element (30) which seals a gap (21) between an outer surface (16) of the wing structure (12) and the trailing edge movable (20). The first flexible panel element (30) establishes a contact (36) between a first end (33) of the first flexible panel element (30) and a surface of the trailing edge movable (20). The first flexible panel element (30) is deflected by a movement of the trailing edge movable (20) relative to the wing structure (12) when the first end (33) of the first flexible panel element (30) is in contact with the surface of the trailing edge movable (20). The invention also relates to a method for manufacturing a trailing edge system (10).