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

Claim 9:
10. 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, and
wherein the median lip has a curvature in the median plane such that the median lip joins said bottom lobe and top lobe by forming a circular arc.