The invention relates to an aircraft lifting surface comprising an aerodynamic surface (11) with a first electrode (21) embedded at its surface, and a control surface (12) articulated to the aerodynamic surface (11), characterized in that the control surface (12) comprises a second electrode (22) embedded at its surface, and that the first electrode (21) and the second electrode (22) are arranged and adapted to create a plasma (36) in air upon application of a predetermined electrical tension, called ionizing tension, between the first electrode (21) and the second electrode (22).
AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
FLUGZEUGTRAGFLÄCHE UND FLUGZEUG MIT SOLCH EINER TRAGFLÄCHE
SURFACE DE SUSTENTATION D'AÉRONEF ET AÉRONEF COMPRENANT UNE TELLE SURFACE DE SUSTENTATION
2024-11-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
European Patent Office | 2024
|NTIS | 1975
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