A gas turbine engine includes a thrust reverser including a plurality of blocker doors moveable between a deployed position and a stowed position. A gap is defined between adjacent blocker doors when in the stowed position. A plurality of divots are mounted forward of the plurality of blocker doors to substantially cover the gap between the adjacent blocker doors when in the stowed position.


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    Title :

    DIVOT FOR BLOCKER DOORS OF THRUST REVERSER SYSTEM


    Contributors:

    Publication date :

    2015-07-30


    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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