公开(公告)号：US11465774B2

公开(公告)日：2022-10-11

申请号：US16377834

申请日：2019-04-08

Applicant: Airbus Operations SAS ,  Airbus SAS

Inventor： Christian Gulli ,  Patrick Roussel ,  Patrick Hubert

IPC: B64F1/10 ,  B60D1/18 ,  B64F1/22

Abstract: To avoid the intervention of an operator on a direction control device with which an aircraft towing system is equipped, this system comprises a first towing sling comprising a front end connected to a towing vehicle, and a rear end connected to a first main landing gear, a second towing sling comprising a front end connected to the vehicle, and a rear end connected to a second main landing gear. The direction control device is connected to a front landing gear, and arranged between the first and second slings. The direction control device comprising a lateral direction control member having a first lateral end mounted on the first sling, and a second lateral end mounted on the second sling.