Abstract: The invention pertains to a device for 3-dimensionally positioning a coupling component, which forms part of an actuator-driven coupling structure, wherein said device comprises at least a first coupling element that extends in a first longitudinal direction and can be bidirectionally displaced along its first longitudinal direction by means of a first actuator, a second coupling element that extends in a second longitudinal direction and can be bidirectionally displaced along its second longitudinal direction, which extends orthogonal to the first longitudinal direction, by means of a second actuator, and a lever with a longitudinal lever direction that is mounted pivotably about a pivoting axis, which divides the lever into a work arm and a power arm.

Abstract: A loads interface (1), particularly a loads interface (1) of an aircraft door with an edge frame (13), an outer skin (15) and a beam (14). A loads transferring flange (11) is designed to transmit transverse, circumferential and/or longitudinal forces, is provided with at least three flanges (18, 19, 20) for distribution of the loads in the edge frame (13), the outer skin (15) and the beam (14).

Abstract: A loads interface (1), particularly a loads interface (1) of an aircraft door with an edge frame (13), an outer skin (15) and a beam (14). A loads transferring flange (11) is designed to transmit transverse, circumferential and/or longitudinal forces, is provided with at least three flanges (18, 19, 20) for distribution of the loads in the edge frame (13), the outer skin (15) and the beam (14).

Abstract: The present invention concerns an intermediate reinforced composite part composed of an assembly of at least two composite members (1,2,4,5) each comprising reinforcing fibres or fabrics and an impregnation matrix, said assembly comprising a bonding agent (3) ensuring a mechanical bond between said members, characterised in that the bonding agent (3) comprises at least one carbon nanotube (“Bucky Paper”) sheet.