公开(公告)号：US20250074612A1

公开(公告)日：2025-03-06

申请号：US18820521

申请日：2024-08-30

Applicant: Airbus Operations SAS

Inventor： Kotaro FUKASAKU ,  Lionel CZAPLA ,  Rémi AMARGIER ,  Alain RAZAFINDRABE ,  Thomas SPIGOLON

IPC: B64D27/40

Abstract: An aircraft comprising at least one engine mounting system which connects a propulsion unit and a wing and which comprises a primary structure, engine mounts connecting the primary structure and the propulsion unit, as well as at least first, second and third wing mounts connecting the primary structure and the wing structure, the first and second wing mounts being offset height-wise with respect to one another, the third wing mount being offset in the longitudinal direction toward the rear with respect to the first and second wing mounts.