Systems and methods are provided for an inductive coil anti-icing and noise absorption system. In certain versions, the inductive coil anti-icing and noise absorption system may include an inductive coil and a skin. The inductive coil may generate electromagnetic fields and may electromagnetically couple with the skin. The skin, upon electromagnetically coupling with the inductive coil, may increase in temperature and the increase in temperature may melt or prevent the formation of ice on the skin. The skin or a portion of the skin may be porous and may allow incorporation of a sound absorbing liner. The sound absorbing liner may attenuate noise generated by the aircraft (e.g., noise generated by the aircraft engine). Certain versions may include a plurality of inductive coils and a plurality of skins.
SYNERGETIC NOISE ABSORPTION AND ANTI-ICING FOR AIRCRAFTS
SYNERGISTISCHE GERÄUSCHABSORPTION UND ENTEISUNG FÜR FLUGZEUGE
ABSORPTION DE BRUIT SYNERGIQUE ET ANTIGIVRAGE POUR AÉRONEFS
2020-01-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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