Abstract:
The present invention provides an interconnection, in particular in the field of aerospace. The interconnection has a T-stringer, an Ω-stringer and a connecting arrangement. The connecting arrangement connects base sections of the T-stringer and of the Ω-stringer to one another. This provides a coupling of an Ω-stringer to a T-stringer which is comparatively insensitive with respect to tolerances relating to the orientation of the Ω-stringer in relation to the T-stringer.
Abstract:
The invention relates to an interconnection, including: a T-stringer which has a web portion and two foot portions; a Ω-stringer which has a comb portion and two foot portions; and a connection arrangement which joins together the foot portions of the T-stringer and of the Ω-stringer, wherein the connection arrangement joins together the T-stringer and the Ω-stringer, wherein the connection arrangement has a first and a second connection element, the connection elements connecting a first foot portion of the T-stringer to a first foot portion of the Ω-stringer, respectively, wherein the connection elements together have a substantially H-shaped outline, and wherein at least one angle bracket, in particular for connecting a former to the Ω-stringer and the T-stringer, is connected to the widening foot portions of the first and second connection elements.