A helicopter engine air intake is provided with an anti-icing grating that offers significant bypass flow in the event of icing. According to the invention, this air intake comprises air intake lips (30, 32), and an anti-icing grating (36) mounted on the external ends (30a, 32a) of the air intake lips (30, 32) and which is interposed in the flow of air entering the air intake (34), at least one air intake lip (30, 32) being formed of thin sheet metal.


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    Titel :

    Helicopter engine air intake with improved bypass flow


    Beteiligte:
    JACTAT PAUL-ETIENNE (Autor:in) / BULOT NICOLAS (Autor:in) / LEBRUSQ PASCAL (Autor:in) / VERGEZ THIERRY (Autor:in)

    Erscheinungsdatum :

    2015-04-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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