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FIBER COMPOSITE COMPONENT FOR ENERGY ABSORPTION IN THE EVENT OF A CRASH FOR AN AIRCRAFT OR SPACECRAFT, FUSELAGE STRUCTURAL SECTION OF AN AIRCRAFT OR SPACECRAFT, AND AIRCRAFT OR SPACECRAFT
FIBER COMPOSITE COMPONENT FOR ENERGY ABSORPTION IN THE EVENT OF A CRASH FOR AN AIRCRAFT OR SPACECRAFT, FUSELAGE STRUCTURAL SECTION OF AN AIRCRAFT OR SPACECRAFT, AND AIRCRAFT OR SPACECRAFT
In the case of a fiber composite component for energy absorption in the event of a crash for an aircraft or spacecraft, the fiber composite component is formed as a laminate construction made of CFRP layers and at least one integrated metal foil portion which is corrosion-resistant with respect to the CFRP layers. A fuselage structure portion of an aircraft or spacecraft is formed using at least one fiber composite component of this type. An aircraft or spacecraft comprises a fuselage structure portion of this type.
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