The invention relates to an aerodynamic profiled body for an aircraft, in particular a winglet, comprising a front profiled element having a profile front edge, a rear profiled element having a profile rear edge, and an adjusting unit, which connects the front profiled element to the rear profiled element and by means of which the rear profiled element can be moved in relation to the front profiled element, wherein the adjusting unit has a front mounting device connected to the front profiled element, a rear mounting device connected to the rear profiled element, and a force-transmitting device, which connects the front mounting device and the rear mounting device to each other.
AERODYNAMISCHER PROFILKÖRPER FÜR EIN FLUGZEUG
AERODYNAMIC PROFILED BODY FOR AN AIRCRAFT
CORPS À PROFIL AÉRODYNAMIQUE POUR AÉRONEF
01.01.2020
Patent
Elektronische Ressource
Deutsch
IPC: | B64C AEROPLANES , Flugzeuge |
Strömungskörper, Tragfläche, Flugzeug und Verfahren zum Ausgleichen aerodynamischer Lasten
Europäisches Patentamt | 2015
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