METHOD FOR PRODUCING A FRAME COMPONENT FOR A DOOR FRAME STRUCTURE OF AN AIRCRAFT, FRAME COMPONENT, AND DOOR FRAME STRUCTURE

摘要

The present invention describes a method for producing a frame component (1) for a door frame structure (100) of an aircraft. Here, a connecting zone (21; 22) is generated on a first and a second assembly surface (20a; 20b) of a connecting component (20) in each case by generating a surface texture on the assembly surfaces (20a; 20b), wherein the connecting component (20) is formed from a metal material. The assembly surfaces (20a; 20b) of the connecting component (20) are placed against a door frame member (10) and against an attachment member (30), wherein the door frame member (10) and the attachment member (30) are each formed from a fibre-reinforced thermoplastics material. Furthermore, the connecting component (20) and the door frame member (10) are welded, and the connecting component (20) and the attachment member (30) are welded. A frame component (1) and a door frame structure (100) are also described.