A nacelle (212) is provided comprising, a thrust reverser (216) comprising a translating sleeve (208; 604) configured to translate between a stowed position and a deployed position, the translating sleeve (208; 604) comprising a slat cutout (210; 610) for clearance, and a slat clearance door (204; 602) disposed at least partially in the slat cutout (210; 610) in response to the thrust reverser (216) being in the stowed position, wherein the slat clearance door (204; 602) is configured to move in response to the thrust reverser (216) being in the deployed position to expose a portion of the slat cutout (210; 610) to accept a portion of a deployed forward wing slat (206; 606).


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    Title :

    SLAT-THRUST REVERSER CLEARANCE


    Additional title:

    SCHUBUMKEHRER MIT VORFLÜGELFREIRAUM
    INVERSEUR DE POUSSÉE COMPRENANT UNE DÉCOUPE D'ÉVITEMENT DU BEC MOBILE D'UNE AILE


    Contributors:

    Publication date :

    2018-09-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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