Component connecting arrangement, particularly for large-area flat components, of aircraft, has plate part with attachment part, where plate part and attachment part are connected with each other in boundary areas

摘要

The component connecting arrangement has a plate part (5) with an attachment part (6), where the plate part and the attachment part are connected with each other in the boundary areas (7) by the interaction of a clinching tool. Multiple clinch seam sections (8a,8b,8c) are inserted along the overlapped boundary areas, where the clinch seam sections run in different directions and are adjacent to each other. Independent claims are also included for the following: (1) a method for machine connection of a plate part with an attachment part for the production of a component connecting arrangement; and (2) an aircraft with a trunk.