AIRCRAFT PROPULSION ASSEMBLY COMPRISING A NACELLE WITH A T-SHAPED FRAME

The invention relates to a propulsive assembly (150) comprising a nacelle delimiting an interior volume (154), a T-shaped chassis (160) comprising a first wall (160a) fixed to the wing and a second vertical wall (160b) dividing the interior volume (154) into two sub-volumes (154a-b), a dihydrogen consuming device (162) for each sub-volume (154a-b), a dihydrogen treatment system (166), a supply line (168) connected between the treatment system (166) and the consuming device (162), and a supply line (164a-b) connected between the treatment system (166) and a dihydrogen tank. With such an arrangement, the distribution of dihydrogen is doubled and a failure on one side of the second wall will not impact the other side.