Method and device for making parts of a composite material, in particular sections of an aircraft fuselage

The invention claims a method for producing a composite material made of the hollow component especially claims such as airframe component method and device of the hollow component comprises outer skin and can be the reinforcing element. The method comprises set with fibre laying head a plurality of articulated arm extends into the shape of the negative mould in the step of said negative mould through the longitudinal notch opening the longitudinally cut used for containing said several joint of the arm supporting mechanism and using the laying head a fibre coating the negative mould of the internal surface so as to form the composite material the outer skin of the following steps by using a joint arm movable coating head and along the longitudinally cut relatively translational articulated arm of said supporting mechanism.