Method for producing a fuselage component for an aircraft, fuselage component for an aircraft and aircraft

摘要

The present invention describes a method for producing a fuselage component (100) for an aircraft (200). According to the invention, stiffening profiles (2; 3) of a plurality of layers (20; 30) lying one above the other in a thickness direction (T) are intersected on a surface (1a) of a surface-extending shell part (1) made of a fiber composite material at a crossing point (5) ), which are each formed by applying filaments (4), each of which has a fiber bundle (F) embedded in a thermoplastic material (P). Stabilizing layers (41; 42) are formed from the filaments (4) in the stiffening profiles (2; 3), within which the filaments (4) extend beyond the crossing point (5). Furthermore, a fuselage component (100) and an aircraft (200) are described which have at least one such fuselage component (100).