A method for mounting a vortex generator on an aerodynamic panel of an aircraft, including, before the step of assembling the vortex generator and the aerodynamic panel, a step of installing at least one shim interposed between the base of the vortex generator and the aerodynamic panel, the shim including a first face, oriented towards the aerodynamic panel during operation, that is shaped like the inner surface of the aerodynamic panel, and a second face, oriented towards the base during operation, that is shaped like the upper face of the arm of the base. This solution makes it possible to manufacture the vortex generator without taking into account the curvature of the aerodynamic panel. An aircraft is provided including at least one vortex generator mounted in this way.
PROCÉDÉ DE MONTAGE D'UN GÉNÉRATEUR DE TOURBILLONS SUR UNE PAROI AÉRODYNAMIQUE COURBE D'UN AÉRONEF ET AÉRONEF COMPRENANT AU MOINS UN GÉNÉRATEUR DE TOURBILLONS AINSI MONTÉ
METHOD FOR MOUNTING A VORTEX GENERATOR ON A CURVED AERODYNAMIC WALL OF AN AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE VORTEX GENERATOR THUS MOUNTED
VERFAHREN ZUR MONTAGE EINES WIRBELGENERATORS AN EINER GEKRÜMMTEN AERODYNAMISCHEN WAND EINES FLUGZEUGS UND FLUGZEUG MIT MINDESTENS EINEM DARAUF MONTIERTEN WIRBELGENERATOR
02.07.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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