Hull of an aircraft or spacecraft in CFRP metal. Hybrid construction with a metal frame

摘要

Rigid fuselage (10) of an aircraft or spacecraft with fuselage elements in CFRP construction, the fuselage elements each having an outer skin and an inner skin, each made entirely of a CFRP material or of a laminate with at least one layer of a CFRP material and at least one layer are formed from a GRP material and / or an AFK material, a composite core element being provided between the outer skin and the inner skin, the composite core element having a honeycomb structure and made of at least one organic material or a fiber-reinforced plastic or wax paper and the fuselage (10) having a metal frame (1) inside which is connected to the fuselage elements, the metal frame (1) having annular metal frames (2, 3, 4, 5) which are connected to one another in the longitudinal direction via metal elements (6) are connected to form a Faraday cage, the metal frames (2, 3, 4, 5) and the metal elements ( 6) are made of aluminum, steel and / or titanium.