An aircraft ice protection system (A) is provided for preventing ice accretion on a wing (2) of an aircraft or removing the accreted ice. Bleed air (S2) extracted from a main engine (3) of the aircraft and air (S1') introduced from an air intake (31) installed on an airframe (28) and heated by a heat source (26) of the airframe of the aircraft are selectively supplied to a hot air chamber (32) formed inside the wing (2), thereby carrying out ice protection.
AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH SAME
FLUGZEUG-FROSTSCHUTZSYSTEM UND DAMIT AUSGESTATTETES FLUGZEUG
SYSTÈME ANTIGIVRE POUR AÉRONEF ET AÉRONEF DOTÉ DE CELUI-CI
2019-04-24
Patent
Electronic Resource
English
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