公开(公告)号：US20210284338A1

公开(公告)日：2021-09-16

申请号：US17197813

申请日：2021-03-10

Applicant: Airbus Operations S.L.

Inventor： Diego GARCIA MARTIN ,  Raul Carlos LLAMAS SANDIN

IPC: B64C39/00 ,  B64C39/08 ,  B64C25/04 ,  B64C3/56 ,  B64C25/10 ,  B64C7/00 ,  B64D27/02

Abstract: An asymmetric aircraft configuration having a first and a second wing, the first wing having a span larger than the second wing. A first engine is mounted on the first wing, and a second engine mounted on the rear end of the aircraft with its centerline aligned with the aircraft longitudinal axis. The rear end of the aircraft has a T tail, and the second engine is configured to ingest and consume air forming a boundary layer during the flight. A main landing gear assembly includes a first landing gear attached to the first wing, and a second landing gear attached to an area of the fuselage close to the second wing.