The invention relates to a method of manufacturing a stiffened panel (10) comprising a skin (11) and at least one substantially elongate stiffener (12) said stiffener comprising a longitudinal groove (13) forming a cavity (15), said panel comprising at least one means (19) for storing and releasing electrical energy which means is placed inside the cavity, said method involving a step of filling the groove (13) with at least one means (19) of storing and releasing electrical energy; and a step of covering said means with the skin (11) so that the groove of the stiffener and the skin together form the cavity (15). The invention also relates to a stiffened ring (10) derived from such a method.
Stiffened panel and method of manufacturing same
2015-07-01
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |