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.


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    Title :

    AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH SAME


    Additional title:

    FLUGZEUG-FROSTSCHUTZSYSTEM UND DAMIT AUSGESTATTETES FLUGZEUG
    SYSTÈME ANTIGIVRE POUR AÉRONEF ET AÉRONEF DOTÉ DE CELUI-CI


    Contributors:

    Publication date :

    2019-04-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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