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采用Z-Pin增强体的3D炭/炭复合材料层间断裂行为

韩立军 李铁虎 刘建军 邱海鹏 丁海英

新型炭材料2004,Vol.19Issue(2):97-102,6.
新型炭材料2004,Vol.19Issue(2):97-102,6.

采用Z-Pin增强体的3D炭/炭复合材料层间断裂行为

Interlaminar fracture behavior of 3D C/C composites using z-pins as through-thickness reinforcements

韩立军 1李铁虎 1刘建军 1邱海鹏 2丁海英2

作者信息

  • 1. 西北工业大学,材料科学与工程学院,陕西,西安,710072
  • 2. 北京航空制造工程研究所,北京,100024
  • 折叠

摘要

Abstract

A novel form of preform consisting of plain weave fabric and z-pin through-thickness reinforcements was prepared. The carbon matrix was derived from a combination of isothermal chemical vapor infiltration and high pressure impregnation-carbonization of coal tar pitch. The interlaminar shear strength of the composites was characterized by a short beam interlaminar shear test and a double edge-notched tensile shear test. Hyper pseudoplastic fracture behavior of short beam interlaminar shear of 3D C/C composites was found, which is ascribed to the propagation of microcracks formed between laminations within and between bundles. Z-pins can have effective control over the progress of pseudoplastic fracture. True shear failure, which is characterized by the double edge-notched tensile test, shows non-pseudoplastic fracture progress that is ascribed to shear sliding occurring only within one interlamination. Both short beam interlaminar strength and double edge-notched tensile strength is 40~50 % higher for a z-pin density of 1.5 mm interval than for a z-pin density of 2.5 mm interval. Employing z-pins as through-thickness reinforcements has advantages over a 3D weave.

关键词

层间破坏/3D C/C复合材料/Z-pin/假塑性

Key words

Interlaminar fracture/3D C/C composite/Z-pin/Pseudoplastic

分类

通用工业技术

引用本文复制引用

韩立军,李铁虎,刘建军,邱海鹏,丁海英..采用Z-Pin增强体的3D炭/炭复合材料层间断裂行为[J].新型炭材料,2004,19(2):97-102,6.

基金项目

国防预研基金(51461070103ZS5003) (51461070103ZS5003)

新型炭材料

OA北大核心CSCDCSTPCDSCI

1007-8827

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