Heterogeneous multilayer heat prevention-heat insulation composite material prefabricating body structure and molding process thereof
A composite material and forming process technology, applied in the directions of lamination, layered products, lamination devices, etc., can solve the problem of poor thermal performance stability, affecting the reliability of the thermal protection system of hypersonic aircraft, and the weight of the thermal protection system being too large, etc. question
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[0033] Prepare the positioning plate 5 and the guide rod 4, the diameter of the guide rod is 1.2mm, punch a hole on the positioning plate 5, the hole diameter is 1.2mm, fix the guide rod 4 on the positioning plate 5, as figure 2 shown.
[0034] image 3 It is a top view of the guide rod 4 distribution, the center distance of the guide sleeves in the y direction is 2 mm, the center distance of the first, second, fourth and fifth rows of guide sleeves in the x direction is 2 mm, and the center distance of the third row of guide sleeves in the x direction is 4 mm.
[0035] The heat-proof structure layer 1 is made of 3K SiC fiber with an area density of 1.79g / cm 3 , the center distance of the guide sleeve in the x and y directions is 2mm, and the fibers follow the guide sleeve according to Figure 4 The method of middle 6 is used for cross-winding, and then laid along the horizontal direction of the guide sleeve to prepare a heat-resistant structural layer 1 with a thickness of...
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