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.
METHOD FOR PRODUCING A FRAME COMPONENT FOR A DOOR FRAME STRUCTURE OF AN AIRCRAFT, FRAME COMPONENT, AND DOOR FRAME STRUCTURE
VERFAHREN ZUR HERSTELLUNG EINER RAHMENKOMPONENTE FÜR EINE TÜRRAHMENSTRUKTUR EINES FLUGZEUGS, RAHMENKOMPOENTE UND TÜRRAHMENSTRUKTUR
PROCÉDÉ DE PRODUCTION D'UN COMPOSANT DE CADRE POUR UNE STRUCTURE DE CADRE DE PORTE D'UN AVION, COMPOSANT DE CADRE ET STRUCTURE DE CADRE DE PORTE
2019-05-29
Patent
Elektronische Ressource
Englisch
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Europäisches Patentamt | 2019
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