System for the manufacturing of carbon fibre structures and relevant manufacturing process, suitable for aeronautic applications

摘要

Equipment and method for the manufacturing of integral monolithic structures, adopting reinforcing fibre layers impregnated with thermosetting resins, consisting of: the equipment base (4), which determines the shape of the structure; the cover (8) of said equipment; two side supports (6), enclosed by an outer bag (16) made of nylon or similar material and by as many supporting elements (7) as the number of bays required; breathing material (17); a sheet of parting film (18); sealing mastic (15); vacuum application valves (14); a tubular parting film (10); tubular bags (11).;The invention simplifies a manufacturing process, particularly important in the aeronautical field and wherever there is a need for very low weight, high structural efficiency and high quality standards.