Preparation method of ceramic-based composite material standard sample with lamination defects
A composite material and delamination defect technology, which is applied in the field of preparation of ceramic matrix composite material delamination defect standard samples, can solve the problems of easy deformation size control of standard samples, etc.
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Embodiment 1
[0027] Example 1: Rectangular delamination defect standard sample.
[0028] (1) Stack 12 layers of 2D [0° / 90°] carbon fiber cloth 1 in sequence;
[0029] (2) Cut a 0.2mm thick PTFE film into a rectangular shape as defect 2. In this embodiment, the placed rectangular defect 2 is 130mm long and 50mm wide;
[0030] (3) Place the PTFE film cut in step (2) on top of the layer of carbon fiber cloth 1 stacked in step (1), and then stack 12 layers of 2D[0° / 90°] carbon fiber cloth in sequence 1;
[0031] (4) Use two porous shaped graphite templates to clamp the above laminated carbon fiber cloth 1 with defects 2, and use relay needle punching to stitch the template and the laminated carbon fiber cloth 1 in the middle. Get a density of 0.6g / cm 3 Carbon fiber preform;
[0032] (5) The obtained carbon fiber preform is deposited by CVD to pyrolyze the C interface layer to obtain a density of 1.6g / cm 3 C / C composite materials; process conditions: deposition temperature 800-900℃, pressure 0.2-0.4kPa...
Embodiment 2
[0037] Example 2: Stepped delamination defect standard sample.
[0038] (1) Stack 12 layers of 2D [0° / 90°] carbon fiber cloth in sequence;
[0039] (2) Cut 0.2mm thick polytetrafluoroethylene film into rectangular shapes of different sizes as defects 2. In this embodiment, the length of the placement defect is 130mm, and the width is 40mm, 50mm, 60mm, 70mm to form a stepped defect. 2.
[0040] (3) Place the defect 2 of the stepped PTFE film cut in step (2) on the layer of carbon fiber cloth 1 stacked in step (1), and then stack 12 layers of 2D[0° / 90 °] Carbon fiber cloth 1;
[0041] (4) Use two porous shaped graphite templates to clamp the above laminated carbon fiber cloth 1 with defects 2, and use relay needle punching to stitch the template and the laminated carbon fiber cloth 1 in the middle. Get a density of 0.6g / cm 3 Carbon fiber preform;
[0042] (5) The obtained carbon fiber preform was deposited by CVD to pyrolyze the C interface layer to obtain a density of 1.6g / cm 3 C / C co...
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