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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    Titel :

    Divot for blocker doors of thrust reverser system


    Beteiligte:

    Erscheinungsdatum :

    2018-04-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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