Patent ID: 11878809
Assignee: AIRBUS OPERATIONS S.L.
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 0:
1. An aircraft propulsion assembly comprising:
a first engine and a second engine that are adjacent and a nacelle in which said first and second engines are installed,
wherein the nacelle comprises a common air inlet lip for the first engine and the second engine, the air flow being divided between the first engine and the second engine by a median lip which extends, at least partly, set back from said common air inlet lip,
wherein the common air inlet lip comprises, directly in line with the median lip, a bottom lobe and a top lobe extending forward of the nacelle,
wherein the first engine comprises a first fan and the second engine comprises a second fan, the first fan and the second fan extending in one and the same plane, and
wherein a circle in which the first fan is inscribed in rotation is separated by at most thirty centimeters, from a circle in which the second fan is inscribed in rotation.