Patent ID: 11952817
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B  E | IPC B  E

Claim 0:
1. A fastening system comprising:
a structure holding element which is configured to be fastened to a structural component;
a component holding element which is configured to be fastened to a component that is to be fastened and which is configured to be movable relative to the structure holding element between a first operating position and a second operating position;
a first lever element which is connected to the structure holding element to be rotatable about a first rotation axis and which is connected to the component holding element to be rotatable about a second rotation axis; and
a connection element which is connected to the component holding element to be rotatable about a third rotation axis and which is connected to the structure holding element to be displaceable in translation relative to the structure holding element, such that, when the component holding element is transferred from the first operating position into the second operating position, the second rotation axis is displaced in a plane extending perpendicularly to the second rotation axis.