A structural component for reinforcing the fuselage of an aircraft or spacecraft is integrally formed and segmented into surface-like stiffening sections, whereby at least one stiffening section is formed as a rigid mesh section, and at least one stiffening section is formed as a solid section.
STRUCTURAL COMPONENT AND METHOD FOR PRODUCING A STRUCTURAL COMPONENT
12.05.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / B22F Verarbeiten von Metallpulver , WORKING METALLIC POWDER / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64G Raumfahrt , COSMONAUTICS / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL |
Structural component and method for producing structural component
Europäisches Patentamt | 2024
|Structural component and method for producing a structural component
Europäisches Patentamt | 2018
|Structural component and method for producing a structural component
Europäisches Patentamt | 2016
|STRUCTURAL COMPONENT AND METHOD FOR PRODUCING A STRUCTURAL COMPONENT
Europäisches Patentamt | 2025
|Structural component, vehicle and method for producing structural component
Europäisches Patentamt | 2024
|