公开(公告)号：US20200324871A1

公开(公告)日：2020-10-15

申请号：US16843399

申请日：2020-04-08

Applicant: Airbus Operations Ltd.

Inventor： Henry EDWARDS ,  Miguel PENA-HERRERO

IPC: B64C3/00 ,  B64C3/16 ,  B64C3/34 ,  B64C25/14 ,  B64D27/02 ,  B64C7/00 ,  B64C3/40 ,  B64D33/02

Abstract: An aircraft wing with a root, a tip, an inboard wing part, an outboard wing part, and a junction between the inboard wing part and the outboard wing part. The inboard wing part has anhedral and is swept back so that it extends downwardly and aft away from the root towards the junction. The outboard wing part has dihedral and is swept forward so that it extends upwardly and forward away from the junction towards the tip. An engine and landing gear are mounted at the junction. An aircraft with a pair of such wings has a W-shaped profile viewed from above, and an inverted gull-wing profile viewed from the front.