Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung

摘要

The lightweight structure consists of at least one skin metal sheet (1) and stiffening elements (2), which are arranged longitudinally and/or vertically on the metal sheet and which are connected to the metal sheet using the feet (3) of the stiffening elements. The link (4) of the stiffening element consists of two legs (5,6) on the side that is turned to the metal sheet. Both legs are connected to the metal sheet using two separate joining areas (7,8). An Independent claim is also provided for a method for manufacturing lightweight structure components.