Patent ID: 8382038
Filing Date: 2013-02-26
Classification: B60P,B64D,Y02T

Abstract:
1. A device comprising a connection rod combined with a fuselage structure of an aircraft for bracing the fuselage structure of an aircraft and for fastening a component on the fuselage structure, said device comprising a central portion and two end portions, wherein a joint is arranged in the region of at least one end portion, the joint being integrated in the fuselage structure or in the component and being pivotable around at least one rotational axis, characterized in that the device has said joint is formed with a barrel nut, wherein the barrel nut is rotatably received in a bearing bore in the component and an end portion is screwed into the barrel nut and the other end portion is screwed to the fuselage structure and that the component is comprised of a vertical support of a lining frame for mounting a plurality of seats; and wherein an inner barrel nut is pivotably received in the barrel nut, wherein the end portion is screwed into the inner barrel nut (− 69 ).