The present disclosure relates generally to an aerodynamic track fairing assembly (200) used on an engine nacelle (66), the track fairing assembly (200) positionable on the aft section (67) of the engine nacelle, the aerodynamic track fairing assembly (200) including an upper section (202) extending toward an aft end (69) of the aft section (67) of the engine nacelle (66), a bottom section (206) extending toward the aft end (69) of the aft section (67) of the engine nacelle (66), the bottom section (206) affixed to the upper section (202) to form a track cavity (212) therebetween, and a fairing fitting (214) disposed within the track cavity (212) and affixed to the bottom section (206).


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    Title :

    TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE


    Additional title:

    GONDELVERKLEIDUNGSANORDNUNG FÜR EINE TURBINENMOTOR
    ENSEMBLE DE CARÉNAGE POUR UNE NACELLE DE TURBORÉACTEUR


    Contributors:

    Publication date :

    2020-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    Natural laminar flow flight experiments on a turbine engine nacelle fairing

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