The present disclosure provides an inlet assembly for a nacelle. The inlet assembly may comprise an inlet (200), a lip skin (208) coupled to the inlet (200), the lip skin (208) and the inlet (200) forming a duct (224), and an inner duct skin (214) situated between the inlet (200) and the lip skin (208), the inner duct skin (214) separating the duct (224) by defining a first chamber (240) and a second chamber (242).


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    Title :

    SEGREGATED ANTI-ICE DUCT CHAMBER


    Additional title:

    SEGREGIERTE ANTI-EIS-KANALKAMMER
    CHAMBRE DE CONDUIT ANTI-GIVRE SÉPARÉE


    Contributors:

    Publication date :

    2020-01-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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