A method for producing a fuselage portion, in particular for an aircraft or spacecraft, has the following method steps: welding a skin portion containing a thermoplastic material with a former containing a thermoplastic material in the region of a predetermined welding zone; and connecting an attachment element, configured as a crack stopper, to the skin portion and to the former in the region of the welding zone.
METHOD FOR PRODUCING A FUSELAGE PORTION
2017-12-14
Patent
Electronic Resource
English
European Patent Office | 2025
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