US 12,296,975 B2
Aircraft propulsive assembly comprising a nacelle with a t-shaped frame
Lionel Czapla, Toulouse (FR); Christophe Labarthe, Toulouse (FR); and Kotaro Fukasaku, Toulouse (FR)
Assigned to Airbus Operations SAS, Toulouse (FR)
Filed by Airbus Operations SAS, Toulouse (FR)
Filed on Mar. 12, 2024, as Appl. No. 18/602,498.
Prior Publication US 2024/0327023 A1, Oct. 3, 2024
Int. Cl. B64D 37/30 (2006.01); B64D 27/18 (2006.01); B64D 29/02 (2006.01); F02K 1/36 (2006.01)
CPC B64D 37/30 (2013.01) [B64D 27/18 (2013.01); B64D 29/02 (2013.01); F02K 1/36 (2013.01)] 5 Claims
OG exemplary drawing
 
1. A propulsive assembly for an aircraft comprising a wing and a dihydrogen tank, said propulsive assembly comprising:
a nacelle comprising cowls delimiting an internal volume,
a frame that is T-shaped in cross-section, housed in the internal volume, comprising a first wall configured to be fixed against a bottom surface of the wing, and a second wall extending vertically under the first wall by dividing the internal volume into two sub-volumes when the propulsive assembly is mounted on the aircraft,
a consumer device housed in the internal volume and configured to consume dihydrogen,
for each sub-volume, a processing system housed in said sub-volume and intended to process dihydrogen,
for each processing system, a supply line housed in the associated sub-volume and fluidically connected between the processing system and the consumer device, and
for each sub-volume, an input line fluidically connected to the associated processing system, configured to be fluidically connected to the dihydrogen tank, in which said input line extends partly in the associated sub-volume and partly outside of the associated sub-volume by passing through the first wall.