The invention relates to a wing arrangement (10) comprising a main wing (12) and a slat (14) attached thereto opposite a flow direction (22) in front of the main wing (12). A gap (16) with a flow inlet (18) and a defined flow outlet (20) is formed between the slat (14) and the main wing (12). It is suggested that, in a vertical cross-section viewed along the flow direction (22), a length (D) of a section (32) of the slat (14) extending forwards beyond a length (A) of the main wing (12) opposite the flow direction (22) is at least 20% of a total length (C) of the wing arrangement (10) in the flow direction (22).
FLÜGELANORDNUNG UMFASSEND EINEN HAUPTFLÜGEL UND EINEN ENTGEGEN EINER STRÖMUNGSRICHTUNG VOR DEM HAUPTFLÜGEL DARAN BEFESTIGTEN VORFLÜGEL
WING ARRANGEMENT COMPRISING A MAIN WING AND A SLAT MOUNTED THERETO IN FRONT OF THE MAIN WING AND COUNTER TO A DIRECTION OF FLOW
AGENCEMENT D'AILE COMPRENANT UNE AILE PRINCIPALE ET UN BEC MONTÉ SUR CELLE-CI DEVANT L'AILE PRINCIPALE ET À L'ENCONTRE D'UNE DIRECTION D'ÉCOULEMENT
2024-10-30
Patent
Electronic Resource
German
IPC: | B64C AEROPLANES , Flugzeuge |
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