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.
Fiber composite component for absorbing energy
2015-07-14
Patent
Elektronische Ressource
Englisch
ENERGY-ABSORBING COMPONENT AND PROCESS FOR PRODUCING AN ENERGY-ABSORBING COMPONENT
Europäisches Patentamt | 2019
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