The invention relates to a de-icing system which comprises: - actuators (210) attached to the part (106); and - a device for controlling the actuators (210) in order to vibrate the part (106). The control device is designed for the following, the actuators (210) being divided into a plurality of groups (G1, G2, G3, G4): - to control the actuators (210) of a first one of the groups (G1, G2, G3, G4) in order to establish a resonant frequency of the part (100); then - to control the actuators of a second one of the groups (G1, G2, G3, G4) in order to establish a resonant frequency of the part (106) and, in parallel, to control the actuators (210) of the first group (G1, G2, G3, G4) in order to de-ice the part (106) by vibrating it, using the resonant frequency established with this first group (G1, G2, G3, G4).
DÉGIVRAGE D'UNE PIÈCE D'UN AÉRONEF
DE-ICING OF AN AIRCRAFT PART
ENTEISUNG EINES FLUGZEUGTEILS
2024-04-24
Patent
Elektronische Ressource
Französisch
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