Aircraft design for industrial mass production with a modular system of matrix-like CFRP links

摘要

Modular system for the assembly of larger aircraft components with a first component as a basic structural body (20) and other components such as wing, height and vertical stabilizer shells, which are non-positively connected to each other butts via connecting members (1), characterized in that the matrix-like arranged, recesses (23) having basic structural body (20) is an aircraft fuselage (20), wherein the recesses (23) and connecting members (1) penetrating them form a frictional connection, further components are aerodynamic supporting and control surfaces; the links consist of a cavity-like outer cylinder and, in its interior, a microstructure adapted to fit over the first ends (25) of the carbon fiber reinforced composite links (1) which are insertable into the recesses (23) of the aircraft fuselage (20) Ends (25) are formed, and a similar receiving structure on the aerodynamic support and control surfaces for the via the second end of the connecting members (1) insertable connecting members (1) is provided, wherein the connecting members (1) from a cavity-like outer cylinder (3) consist, which has in its interior a microstructure (2) of several nested inner cylinders (4) of different diameters and different wall thicknesses.