The invention relates to a trailing edge system (10) for an aircraft (100). The system (10) comprises a wing structure (12), a trailing edge movable (20) movably coupled to the wing structure (12), and a flexible panel element (30) connected to the wing structure (12) in order to seal a gap (21) between an outer surface (16) of the wing structure (12) and the trailing edge movable (20). An adjustment element (26) is arranged on the trailing edge movable (20) and is arranged relative to the flexible panel element (30) such that the flexible panel element (30) comes into contact with the adjustment element (26) when the trailing edge movable (20) is moved towards the flexible panel element (30). The adjustment element (26) adjusts a movement of the flexible panel element (30) such that the flexible panel element (30) moves along a first surface region (25) of the trailing edge movable (20).
TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM
HINTERKANTENSYSTEM FÜR EIN FLUGZEUG UND VERFAHREN ZUM BETREIBEN EINER VON EINEM HINTERKANTENSYSTEM BEWEGBAREN AUSTRITTSKANTE
SYSTÈME DE BORD DE FUITE POUR UN AÉRONEF ET PROCÉDÉ DE FONCTIONNEMENT D'UN BORD DE FUITE MOBILE D'UN SYSTÈME DE BORD DE FUITE
01.01.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2017
|Europäisches Patentamt | 2017
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