公开(公告)号：US11952817B2

公开(公告)日：2024-04-09

申请号：US17615067

申请日：2020-07-10

Applicant: Airbus Operations GmbH

Inventor： Philipp Eggert ,  Bogdan-Florin Marculescu

IPC: E05D3/06 ,  B64C1/06 ,  E05D3/12 ,  E05D3/18

CPC classification number: E05D3/125 ,  B64C1/069 ,  E05D3/18 ,  E05Y2201/626 ,  E05Y2201/684 ,  E05Y2900/502

Abstract: A fastening system including a structure holding element fastenable to a structural component. The fastening system includes a component holding element fastenable to a component to be fastened and movable relative to the structure holding element between first and second operating positions. A first lever element is connected to the structure holding element to be rotatable about a first rotation axis and is connected to the component holding element to be rotatable about a second rotation axis. The fastening system includes a connection element, connected to the component holding element to be rotatable about a third rotation axis and connected to the structure holding element to be displaceable in translation relative to the structure holding element, such that the second rotation axis, when the component holding element is transferred from its first into its second operating position, is displaced in a plane extending perpendicularly to the second rotation axis.