A method for producing a frame component for a door frame structure of an aircraft. A connecting zone is generated on a first and a second assembly surface of a connecting component in each case by generating a surface texture on the assembly surfaces, wherein the connecting component is formed from a metal material. The assembly surfaces of the connecting component are placed against a door frame member and against an attachment member, wherein the door frame member and the attachment member are each formed from a fiber-reinforced thermoplastics material. Furthermore, the connecting component and the door frame member are welded, and the connecting component and the attachment member are welded. A frame component and a door frame structure are also described.
METHOD FOR PRODUCING A FRAME COMPONENT FOR A DOOR FRAME STRUCTURE OF AN AIRCRAFT, FRAME COMPONENT, AND DOOR FRAME STRUCTURE
2019-06-06
Patent
Electronic Resource
English
European Patent Office | 2019
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