A system for suction of the boundary layer of a wing and protection against icing of this wing includes a wall including micro-perforations and delimiting a leading edge extended by a pressure-side wall and by a suction-side wall. The system also includes a perforated tube running along the leading edge, an exhaust duction for sucking air from this tube in order to suck the boundary layer successively via the micro-perforations of the wall and via the perforations of the tube, and a supply duct for blowing hot air into this perforated tube during a phase of protection against icing, this hot air being discharged successively via the perforations of the tube and via the micro-perforations of the wall.
SYSTÈME D'ASPIRATION DE COUCHE LIMITE ET DE PROTECTION CONTRE LE GIVRE D'UNE SURFACE PORTANTE D'AÉRONEF
SYSTEM FOR SUCTION OF THE BOUNDARY LAYER AND PROTECTION AGAINST ICING OF AN AIRCRAFT BEARING SURFACE
SYSTEM ZUM ABSAUGEN DER GRENZSCHICHT UND ZUM SCHUTZ VOR VEREISUNG EINER FLUGZEUGTRAGFLÄCHE
2022-11-23
Patent
Electronic Resource
French
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