A shell component for an aircraft or spacecraft. The shell component includes a skin panel, a plurality of stringers which are arranged on the skin panel, a former which includes a fiber composite material and is arranged over the stringers so as to cross the stringers, and a former connection structure which includes a ductile material and a plurality of foot portions fixed to the skin panel. The foot portions each transition integrally into a shoulder portion fixed to the former over an associated fixing span, the fixing spans associated with the foot portions extending along the former substantially continuously over the stringers.
Shell component for an aircraft or spacecraft
2015-10-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Method for manufacturing a shell component for an aircraft or spacecraft
European Patent Office | 2018
|European Patent Office | 2016
|METHOD AND APPARATUS FOR MANUFACTURING A SHELL COMPONENT FOR AN AIRCRAFT OR SPACECRAFT
European Patent Office | 2015
|Method and apparatus for manufacturing a shell component for an aircraft or spacecraft
European Patent Office | 2018
|