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针刺预制体参数对C/C复合材料力学性能的影响

郑金煌 李贺军 崔红 张晓虎 邓海亮

固体火箭技术2017,Vol.40Issue(2):221-227,7.
固体火箭技术2017,Vol.40Issue(2):221-227,7.DOI:10.7673/j.issn.1006-2793.2017.02.016

针刺预制体参数对C/C复合材料力学性能的影响

Effect of needle-punched preform parameters on the mechanical properties of carbon/carbon composites

郑金煌 1李贺军 1崔红 2张晓虎 2邓海亮2

作者信息

  • 1. 西北工业大学凝固技术国家重点实验室,西安710072
  • 2. 西安航天复合材料研究所,西安710025
  • 折叠

摘要

Abstract

Carbon fiber preforms were prepared and then densified to produce carbon/carbon composites using needle-punching and chemical vapor infiltration technique,respectively.The effects of the preform manufacturing parameters,including the needlepunched density and its depth,and the mass-to-area (M/A) ratio of short-cut fiber felt,on the mechanical properties of the composites were investigated.The relation between the mechanical properties of the composites and the bulk density of the preforms was also discussed.Results show that the tensile strength of the composites increase and thereafter decrease as the needle-punched density increased from 20 to 50 pin/cm2,while the interlaminar shear strength of the composites tends to increase.The tensile and interlaminar shear strengths exhibit an increasing tendency with the increase of needle-punched depth from 10 to 16 mm,whereas they reduce as the M/A ratio of short-cut fiber felt is increased from 100 to 300 g/m2.Both the tensile and interlaminar shear strengths are dominated by the preform density when only one parameter of the needle-punched density and its depth,and the M/A ratio was varied.The preform density could be employed as a key macro-parameter to predict the mechanical properties of the composites.

关键词

C/C复合材料/针刺参数/针刺预制体/力学性能

Key words

carbon/carbon composites/preform/needle-punched parameters/mechanical properties

分类

航空航天

引用本文复制引用

郑金煌,李贺军,崔红,张晓虎,邓海亮..针刺预制体参数对C/C复合材料力学性能的影响[J].固体火箭技术,2017,40(2):221-227,7.

基金项目

National Natural Science Foundation of China (51202233) (51202233)

Equipment Advanced Research Foundation of China (9140A12060514HT43190) (9140A12060514HT43190)

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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