A structural component has a main body formed of a fibre composite material, a plurality of first reinforcement parts and a plurality of second reinforcement parts, wherein the main body is formed as a domed body having a peripheral edge and a vertex, wherein the first reinforcement parts are connected to the main body and in each case have a concave curvature course in relation to a first plane, and wherein the second reinforcement parts are connected to the main body and also have a concave curvature course in each case in relation to a second plane.
Componente estructural, procedimiento para la fabricación de un componente estructural, fuselaje de presión para un vehículo con componente estructural
2018-03-05
Patent
Electronic Resource
Spanish
IPC: | B64C AEROPLANES , Flugzeuge |
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