The present disclosure provides a nacelle rear assembly for turbojet engine including at least one thrust reverser device to redirect air flow circulating from upstream to downstream in a flow path of the turbojet engine and a mast to link the nacelle to a structure of the aircraft. In one form, the nacelle extends longitudinally from forth to back along an axis and includes a cradle fastened on the mast. In one form, the cradle includes a first longeron and a second longeron extending longitudinally on either side of the mast. The first and second longeron each include a sliding guide device for sliding of a movable cowl and of a cascade of the thrust reverser device.
ENSEMBLE ARRIÈRE DE NACELLE POUR TURBORÉACTEUR COMPRENANT UN BERCEAU POUR MÂT
REAR NACELLE ASSEMBLY FOR A TURBOJET COMPRISING A CRADLE FOR A PYLON
HINTERE GONDELANORDNUNG FÜR EIN STRAHLTRIEBWERK MIT EINEM GERÜST FÜR EINEN PYLON
2019-01-09
Patent
Electronic Resource
French
ENSEMBLE ARRIÈRE DE NACELLE POUR TURBORÉACTEUR COMPRENANT UN BERCEAU DE SUSPENSION
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