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...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
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). |
---|