A nacelle-to-pylon fairing (20) formed over at least a portion of an inter-region between a nacelle (16) and a pylon (18) of an aircraft may include a longitudinal axis, a lateral axis and a transverse axis, an upper end incorporated to the pylon at a fairing-to-pylon interface (72), and a lower end incorporated to the nacelle at a failing-to-nacelle interface (70), wherein the fairing (20) defines a surface between the upper end and the lower end.


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    Title :

    NACELLE-TO-PYLON FAIRING


    Additional title:

    GONDEL-MAST-VERKLEIDUNG
    CARÉNAGE NACELLE-MÂT


    Contributors:

    Publication date :

    2015-11-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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