The present invention pertains to a structural component (1) for reinforcing the fuselage (6) of an aircraft or spacecraft, wherein the structural component (1) is integrally formed and segmented into surface-like stiffening sections, whereby at least one stiffening section is formed as a rigid mesh section (2), and at least one stiffening section is formed as a solid section (3). The present invention further pertains to a method for producing a structural component of this type.
Structural component and method for producing a structural component
Strukturkomponente und Verfahren zur Herstellung einer Strukturkomponente
Composant structurel et procédé de fabrication associé
11.05.2016
Patent
Elektronische Ressource
Englisch
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