A foam sandwich structure of a composite launch tube and its integrated molding method
A composite material and sandwich structure technology, applied in the direction of the launch device, can solve the problems of reduced life, non-continuous fibers, cracks in the launch tube, etc., and achieve the effects of improving stress concentration, ensuring fiber continuity, and improving load-carrying capacity
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[0073] Step 1. Forming the inner structural layer of the launching tube, including the ablation-resistant layer and the main bearing layer. The winding adhesive is made of epoxy resin, and the prepreg is carbon fiber / epoxy resin reinforced material. The thickness of the single layer is 0.2mm, the thickness of the inner structure layer is 6mm, and the fiber volume content is 50-70%.
[0074] Forming the inner structure layer of the launch tube, including the ablation-resistant layer and the main bearing layer.
[0075] First, the surface of the mold is coated with an ablation-resistant coating with a coating thickness of 0.6mm, and then cured after coating.
[0076] Forming of the main bearing layer: laying carbon cloth. Lay carbon cloth on the outer surface of the ablation-resistant layer with a thickness of 0.4mm. The subsequent layup is [90 / +45 / 0 / -45]n, the laying thickness range is 8mm, and the fiber volume content is 50%-70%.
[0077] Step 2: The ring rib is formed for ...
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