The invention relates to a preparation method of an ultra-light multi-feature
skin-free skeleton type
composite material shell. The preparation method comprises the following steps of automatically winding linear
trajectory planning by arranging an end socket guiding and positioning device capable of freely moving, achieving accurate groove entering
numerical control automatic winding of 'non-geodesic line '
equidistant spiral ribs and annular rib hot melting prepreg filaments and alternate proceeding of framework ribs and multi-
feature structure laying are. Aiming at a multi-feature
skin-free skeleton type structure, uniform and effective connection of side wall flanges, end frames and skeleton ribs is realized through balanced interactive
coupling layering structure design, accurate calculation of a skeleton rib hot-melt prepreg
filament winding cycle number, balanced interactive
coupling rib winding-end frame-opening reinforcing area layering structure, rib scattering and the like, and the overall rigidity and stability of the product are ensured. By optimizing the design of a framework rib R-angle mold, a pre-compaction control technology and a reasonable curing process, the problems of poor rib size precision, rib defects and product quality defects caused by the problem of multi-
feature structure curing pressurization interference due to edge overflow of a
skin-free framework rib are solved, high-quality and high-dimensional-precision integrated forming of the ultra-light multi-feature skin-free framework
composite material shell is achieved, the weight is reduced by 30% or above compared with a traditional
skin structure, and the requirement for light weight of
spaceflight models is met.