Abstract: An attachment arrangement for attaching a component to the fuselage of an aircraft. The attachment arrangement comprises an elongated stringer that can be connected to the aircraft fuselage, and a fitting that can be connected to the component. The stringer comprises a multitude of recesses that are formed one behind the other in the direction of longitudinal extension of the stringer. The fitting comprises at least one engagement element that is adapted for positive-locking engagement in the recesses of the stringer. The stringer and/or the fitting can comprise CFC. The fittings can also comprise various other plastics or metal. Weight savings are achieved while at the same time providing stable and variably-positionable attachment. Furthermore, a method for constructing a stringer for an attachment arrangement is proposed, in which method, by providing reinforcement fibers adjacent to the recesses, a carbon scrim is locally reinforced around the recesses.

Abstract: An attachment structure is provided by which interior equipment components of an aircraft passenger cabin can conveniently be affixed. The attachment structure includes, but is not limited to at least one system support that above the cabin floor extends at least along the spacing of two frame elements. The system support has a longitudinal extension along which it comprises a plurality of attachment means, evenly spaced apart from each other, for affixing interior equipment components, wherein the spacing of the attachment means is smaller than the spacing of the frame elements.

Abstract: A test structure for dynamic seat tests comprises a load cell, a seat rail with a bar and a upper chord, a load transfer device, which comes into contact with opposite sides of the bar of the seat rail and is fixed to the load cell and an integrated floor plate which is fixed to the upper chord of the seat rail and to the load transfer device.

Abstract: Proposed is an attachment arrangement (1) for attaching a component to the fuselage (3) of an aircraft, and an aircraft comprising such an attachment arrangement. The attachment arrangement (1) comprises an elongated stringer (5) that can be connected to the aircraft fuselage, and a fitting (11) that can be connected to the component. The stringer comprises a multitude of recesses (9) that are formed one behind the other in the direction of longitudinal extension of the stringer. The fitting comprises at least one engagement element (13) that is adapted for positive-locking engagement in the recesses (9) of the stringer (5). The stringer and/or the fitting can comprise CFC. The fittings can also comprise various other plastics or metal. Weight savings are achieved while at the same time providing stable and variably-positionable attachment.

Abstract: A test structure for dynamic seat tests comprises a load cell, a seat rail with a bar and a upper chord, a load transfer device, which comes into contact with opposite sides of the bar of the seat rail and is fixed to the load cell and an integrated floor plate which is fixed to the upper chord of the seat rail and to the load transfer device.

Abstract: An attachment structure is provided by which interior equipment components of an aircraft passenger cabin can conveniently be affixed. The attachment structure includes, but is not limited to at least one system support that above the cabin floor extends at least along the spacing of two frame elements. The system support has a longitudinal extension along which it comprises a plurality of attachment means, evenly spaced apart from each other, for affixing interior equipment components, wherein the spacing of the attachment means is smaller than the spacing of the frame elements.