烧蚀防热复合材料用压力辅助RTM工艺

马秀萍; 郭亚林; 刘思扬; 吴凡; 霍炳呈

烧蚀防热复合材料用压力辅助RTM工艺

西安航天复合材料研究所, 陕西西安 710025

详细信息

作者简介:
马秀萍,女,1993年生,硕士,研究方向为树脂基复合材料

中图分类号: TB33
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出版历程
- 收稿日期: 2020-07-27
- 刊出日期: 2021-04-24

Pressure-assisted RTM Processing for Ablative Composites

Xi'an Aerospace Composites Research Institute, Xi'an 710025, China

摘要

摘要: 针对目前模压、缠绕等工艺成型烧蚀防热复合材料易造成层间结合差、脱粘、抗烧蚀性能差、易剥蚀等问题，提出了一种新型压力辅助RTM工艺，并对其进行了树脂充模流动模拟，制备了烧蚀防热复合材料，测试了材料的孔隙率、力学性能、烧蚀性能。结果表明：压力辅助RTM工艺具有可行性与优越性，复合材料孔隙率4.64%，层间剪切强度39.3 MPa，线烧蚀率0.017 mm/s，质量烧蚀率0.053 8 g/s。说明压力辅助RTM工艺适合成型烧蚀防热复合材料。
- 压力辅助RTM工艺 /
- 孔隙率 /
- 层间剪切性能 /
- 烧蚀性能
Abstract: The ablative composites made by processing of die molding and tape wrapping have such problems as low interlaminar strength, debonding, poor ablative resistance, and erosion. A new type pressure-assisted RTM processing was presented. Resin filling process was simulated and the ablative composite materials were prepared. The porosity, mechanical property and ablative performance of the composites were tested. The results showed that the pressure-assisted RTM processing was workable and had superiority, and that the porosity, interlaminar shear strength, line ablation rate and mass ablation rate of the composites were 4.64%, 39.3 MPa, 0.017 mm/s and 0.0538 g/s, respectively. The pressure-assisted RTM processing was applicable for moulding ablative composite materials.
- pressure-assisted RTM processing /
- porosity /
- interlaminar shear property /
- ablative performance

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参考文献(6)

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