The invention relates to an assembly for a nacelle, comprising: a stationary fairing (206); a movable cowl (210) movable between a closed position and an open position and comprising an upper edge (210a) and a lower edge (210b) and a reinforcing rib (232) between the two edges; the fixed fairing (206) comprises an upper reinforcing rib (230a) and a lower reinforcing rib (230b); a hinge (212a-b) including a fixed portion (216) attached to the upper reinforcement rib (230a) of the fixed cowl (206) and a movable portion (214) attached to the reinforcement rib (232) of the movable cowl (210); and at least two locks (220a-b), each lock comprising a first portion (221a) fixed to the lower reinforcing rib (230b) and a second portion (221b) fixed to the reinforcing rib (232) of the movable cowl (210). Such assemblies serve to provide access to the inside of the nacelle while ensuring sufficient rigidity of the fairing.

    本发明涉及一种用于短舱的组件,其包括:固定整流罩(206);可动整流罩(210),能够在关闭位置与打开位置之间运动,并包括上边缘(210a)和下边缘(210b)以及在两个边缘之间的加强肋(232);固定整流罩(206)包括上加强肋(230a)和下加强肋(230b);铰链(212a-b),包括固定部分(216)和可动部分(214),固定部分附接到固定整流罩(206)的上加强肋(230a),可动部分附接到可动整流罩(210)的加强肋(232);以及至少两个锁件(220a-b),每个锁件包括第一部分(221a)和第二部分(221b),第一部分固定到下加强肋(230b),第二部分固定到可动整流罩(210)的加强肋(232)。此类组件用作提供通入短舱内侧的通路,同时确保整流罩保持足够的刚性。


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    Titel :

    Assembly for nacelle of aircraft, nacelle and aircraft comprising such assembly


    Weitere Titelangaben:

    用于飞行器的短舱的组件以及包括该组件的短舱和飞行器


    Beteiligte:
    GASTALDI UGO (Autor:in) / BROCHARD WOLFGANG (Autor:in) / PAUTIS OLIVIER (Autor:in)

    Erscheinungsdatum :

    17.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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