公开(公告)号：US20220135212A1

公开(公告)日：2022-05-05

申请号：US17647761

申请日：2022-01-12

Applicant: AIRBUS OPERATIONS LIMITED

Inventor： Clive STEADMAN ,  David LIVERSAGE ,  Ben SMITH ,  Ruth PULLAN

IPC: B64C23/06 ,  B64C5/08 ,  B64C3/18

Abstract: An aircraft assembly is disclosed having a wing tip device connected to a wing tip of a wing by a first connector, a second connector, and a third connector. The wing tip device includes a front device spar and a rear device spar. The first connector is associated with the rear device spar. The second connector is spaced apart in a chordwise direction forward of the first connector, and the third connector is spaced apart in a chordwise direction rearward of the first connector. The third connector includes a spigot mounting formation.

公开(公告)号：US20190118930A1

公开(公告)日：2019-04-25

申请号：US16161371

申请日：2018-10-16

Applicant: AIRBUS OPERATIONS LIMITED

Inventor： Clive STEADMAN ,  David LIVERSAGE ,  Ben SMITH ,  Ruth PULLAN

IPC: B64C3/18 ,  B64C23/06

Abstract: An aircraft assembly is disclosed having a wing tip device connected to a wing tip of a wing by a first connector, a second connector, and a third connector. The wing tip device includes a front device spar and a rear device spar. The first connector is associated with the rear device spar. The second connector is spaced apart in a chordwise direction forward of the first connector, and the third connector is spaced apart in a chordwise direction rearward of the first connector. The third connector includes a spigot mounting formation.