A wing assembly and method for operating the wing assembly, the assembly having a main wing and high-lift body movably coupled to the leading edge of the main wing, the coupling achieved by a driving device, an adjusting lever arrangement having a first main wing lever coupled to the main wing formed between a first adjusting lever pivot joint and the high-lift body as well as a second main wing lever coupled to the main wing so as to form an effective lever arm between a second adjusting lever pivot joint and a first adjusting lever pivot joint, and at least one adjusting lever non-rotatably coupled to the high-lift body, the high-lift body being movable between an initial position and a maximally adjusted position with respect to the initial position, at least one guide mechanism aiding movement of the high-lift body.
AIRFOIL WITH A MAIN WING AND A HIGH-LIFT BODY AND METHOD FOR REALIZING ADJUSTING MOVEMENTS OF A HIGH-LIFT BODY RELATIVE TO A MAIN WING
PROFIL MIT HAUPTFLÜGEL UND HOCHAUFTRIEBSKÖRPER UND VERFAHREN ZUR AUSFÜHRUNG VON STELLBEWEGUNGEN EINES HOCHAUFTRIEBSKÖRPERS IN BEZUG AUF EINEN HAUPTFLÜGEL
PROFIL AÉRODYNAMIQUE À AILE PRINCIPALE ET CORPS HYPERSUSTENTÉ, ET PROCÉDÉ D'EXÉCUTION DE MOUVEMENTS DE RÉGLAGE D'UN CORPS HYPERSUSTENTÉ PAR RAPPORT À UNE AILE PRINCIPALE
2015-10-21
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2016
|WING ASSEMBLY WITH A MAIN WING AND A HIGH-LIFT SYSTEM
Europäisches Patentamt | 2023
|High-Lift Airfoil for Small UAV Wing
British Library Conference Proceedings | 2012
|