Connecting arrangement for sandwich shell elements of an aircraft

摘要

Connecting arrangement for the butt connection of two sandwich elements (12) of an aircraft, each consisting of a core layer (14) and two on both sides on the covering layers (16, 18), the joints of the sandwich elements (12) to be connected in each case a z profile (26) with a web portion (28) and two flanks (30, 32), the web portion (28), the core layer (14), further which a profile peaks (30b, 32a) on the outside at one of the covering layers (16b, 18a) is secured and the other profile peaks (30a, 32b) on the inside on the other cover layer (16a, 18b), which is fastened by means of the core layer (14) projects, further comprising the two z - profiles (26) are arranged so as to overlap one another and the in each case lying one on top of the other flanks (30, 32) are connected to one another.