TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM

TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM

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

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ANDREANI, Luc, LORENZ, Florian, BLANC, Sébastien
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surface (27) of the trailing edge movable (20). A first spacer element (26) is disposed on the upper surface (27) of the trailing edge movable (20) and extends at least over a first portion of the upper surface (27) of the trailing edge movable (20). The first spacer element (26) is configured to maintain a spacing between a first end (33) of the flexible panel element (30) and the upper surface (27) of the trailing edge movable (20) when the trailing edge movable (20) is in the extended position (60).