FIELD: transport.
SUBSTANCE: invention relates to fuselage design for aircraft or spacecraft. Proposed fuselage consists of skin elements or cylindrical parts from carbon fiber-reinforced. Note here that every said element have outer and inner layers, each being made partially or completely from carbon fiber-reinforced plastic. Composite element of the core is arranged between said outer and inner layers. Fuselage inside has metal carcass 1 jointed with said elements of the skin or cylindrical parts to form a part of Faraday cage.
EFFECT: sufficient intrinsic rigidity, efficient anti-lightning protection.
14 cl, 3 dwg
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