Safran Nacelles

Armel Gautier

Patrick Boileau

Olivier Kerbler

Loïc Grall

Ludovic Toupet

Julien Lezerac

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.

Growing community of inventors

Negrepelisse, France

Armel Gautier