公开(公告)号：US20240327032A1

公开(公告)日：2024-10-03

申请号：US18579593

申请日：2022-07-22

Applicant: LEONARDO S.P.A.

Inventor： Stefano Baglioni ,  Maurizio Ribaudo

IPC: B64F1/16 ,  B64U10/17 ,  B64U70/99

CPC classification number: B64F1/16 ,  B64U10/17 ,  B64U70/99

Abstract: A locking device for an aircraft is described, comprising a body adapted to be fixed to a support surface, a first ring and a second ring rotatable the one with respect to the other with respect to a rotation axis between a first angular position and a second angular position. The first and second ring enclose an area for the landing of the aircraft and are contained within the body. The locking device also comprises a plurality of cables, which connect the first ring to the second ring. The locking device is positionable in an unlocking position, wherein the first and second ring are in the first angular position, the cables are spaced from said area; or in a locking position, wherein the first and second ring are in the second angular position and the cables occupy a region of the area, so as to cooperate in contact with the aircraft to constrain it with respect to the support surface.