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).
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
2025-01-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2025
|European Patent Office | 2017
|European Patent Office | 2017
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