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Z-pin增强CMC层间Ⅰ+Ⅱ混合型断裂韧性 被引量:4

Mixed Mode Ⅰ+Ⅱ Interlaminar Fracture Toughness for Z-pin Reinforced CMC
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摘要 提出手工预缝纫方法将3K丝束的T300碳纤维引入预成型体,采用CVI工艺在预成型体和缝线处同时渗透SiC基体,制备了Z-pin增强平纹编织C/SiC陶瓷基复合材料。通过三点弯曲试验测定了Ⅰ+Ⅱ混合型应变能释放率,分析了材料的裂纹扩展行为和Z-pin增强机理。结果表明:随着裂纹扩展长度的增大,Ⅰ+Ⅱ型裂纹扩展阻力不断增大,相同裂纹扩展长度,增加Z-pin植入密度可以提高粘结强度,增大止裂作用。Z-pin增强平纹编织C/SiC陶瓷基复合材料裂纹扩展的耗能途径主要是层间界面剥离、Z-pin弹性剪切和拉伸变形。 A manual pre-stitching method was developed to introduce 3K T300 carbon fiber bundles into preforms.Plain woven ceramic matrix composites(CMCs) reinforced with Z-pins were manufactured by using chemical vapor infiltration(CVI) to infiltrate SiC matrix into plain woven preforms and carbon fiber sutures.Three-point flexure test was used to check mixed mode Ⅰ+Ⅱ strain energy release rates for delamination of Z-pin reinforced plain woven C/SiC ceramic matrix composites.The delamination behaviors and reinforced mechanisms for the material were analyzed.The results show that crack growth resistance of mode Ⅰ+Ⅱ delamination increases with increasing debonding length,and that at the same debonding length,bond strength and arrest action improve with increasing the density of Z-pin.Interlaminar interface debonding,elastic shear deformation and elastic tensile deformation of Z-pins are channels of the energy dissipation during delamination growth of Z-pin reinforced plain woven C/SiC ceramic matrix composites.
出处 《材料科学与工程学报》 CAS CSCD 北大核心 2012年第3期357-360,383,共5页 Journal of Materials Science and Engineering
基金 高等学校博士学科点专项科研基金资助项目(20030699040) 陕西省教育厅专项科研基金资助项目(2010JK628)
关键词 陶瓷基复合材料 断裂韧性 应变能释放率 Z-PIN A manual pre-stitching method was developed to introduce 3K T300 carbon fiber bundles into preforms.Plain woven ceramic matrix composites(CMCs) reinforced with Z-pins were manufactured by using chemical vapor infiltration(CVI) to infiltrate SiC matrix into plain woven preforms and carbon fiber sutures.Three-point flexure test was used to check mixed mode Ⅰ+Ⅱ strain energy release rates for delamination of Z-pin reinforced plain woven C/SiC ceramic matrix composites.The delamination behaviors and reinforced mechanisms for the material were analyzed.The results show that crack growth resistance of mode Ⅰ+Ⅱ delamination increases with increasing debonding length,and that at the same debonding length,bond strength and arrest action improve with increasing the density of Z-pin.Interlaminar interface debonding,elastic shear deformation and elastic tensile deformation of Z-pins are channels of the energy dissipation during delamination growth of Z-pin reinforced plain woven C/SiC ceramic matrix composites.
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参考文献10

  • 1M B Dow, H B Dexter. Development of Stitched, Braided and Woven Composite Structures in the ACT Program and at Langley Research Center ( 1985 to 1997 ) Summary and Bibliography [ R ]. NASA/TP-1997-206234. Hampton, Virginia.
  • 2M Karal. AST Composite Wing Program-Executive Summary [R]. NASA/CR-2001-210650. Hampton, Virginia.
  • 3W B Larry, B Victor. Effectiveness of Z-pins in Preventing Delamination of Co-cured Composite Joints on the Example of A Double Cantilever Test [J]. Composites: Part B, 2006, 37:365-378.
  • 4I S Raju, E H Glaessgen. Effect of Stitching on Debonding in Composite Structure Elements [ R ]. NASA-2001-icces-isr. Hampton, Virginia.
  • 5刘韡,矫桂琼.Z向增强平纹编织C/SiC复合材料层间剪切强度(英文)[J].材料科学与工程学报,2009,27(5):664-667. 被引量:2
  • 6I K Partridge, D D R Cartie. Delamination Resistant Laminates by Z-fiber Pinning I: Manufacture and Fracture Performance[J]. Composites Part A, 2005, 36 (1):55-64.
  • 7D D R Cartie, Manos Troulis, I K Partridge. Delamination of Zpinned Carbon Fibre Reinforced Laminates [J]. Composites Science and Technology, 2006, 66: 855-861.
  • 8刘韡,矫桂琼.Z-pin增强陶瓷基复合材料I型应变能释放率[J].材料科学与工程学报,2009,27(3):381-384. 被引量:4
  • 9X Zhang, L Hounslow, M Grassi. Improvement of low-velocity impact and compression after impact performance by z-fibre pinning [J]. Composites Science and Technology, 2006, 66: 2785-2794.
  • 10A Clarke, E Greenhalgh, C Meeks, C Jones. Enhanced Structural Damage Tolerance of CFRP Primary Structures by Zpins Reinforcement [C]. AIAA-2003-1679. Norfolk, Virginia.

二级参考文献13

  • 1管国阳,矫桂琼,张增光.2D-C/SiC复合材料的宏观拉压特性和失效模式[J].复合材料学报,2005,22(4):81-85. 被引量:53
  • 2刘韡,矫桂琼,管国阳,常岩军.Z-pin增强陶瓷基复合材料拉伸和层间剪切性能[J].复合材料学报,2007,24(1):86-90. 被引量:12
  • 3L. A. Mignery, T-M Tan, C-T Sun. The use of stitch to suppress delamination in laminated composite [S]. Philadelphia, American Society for Testing and Materials, 1985, 371-385.
  • 4G. Freitas, C. Magee, P. Dardzinski, T. Fusco. Fiber insertion process for improved damage tolerance in aircraft laminates [J]. Journal Advanced Material, 1994, 25(4):36-43.
  • 5M. B. Dow, H. B. Dexter. Development of Stitched,Braided and Woven Composite Structures in the ACT Program and at Langley Research Center (1985 to 1997) Summary and Bibliography [R]. NASA TP-97-206234. Hampton, Virginia.
  • 6I. K. Partridge, D. D. R. Cartie Delamination resistant laminates by Z-Fiber pinning: Part I manufacture and fracture performance [J]. Composites: Part A applied science and manufacturing, 2005, 36(1): 55-64.
  • 7Takashi Ishikawa, Toshio Orgasawara. Overview of development activities of spaceplane components using NUSK-CMC (CMC with continuous Si-Ti-C-O fiber)[C]. AIAA-2001-1879. Kyoto, Japan.
  • 8K. A. Dransfield, L. K. Jainb, Y-W Mai. On the effects of stitching in CFRPs-I. Mode I delamination toughness [J]. Composites Science and Technology, 1998, 58: 815-827.
  • 9X-N Sun, L-Y Tong, M. K. D. Wood, Y-W Mai. Effect of stitch distribution on mode I delamination toughness of laminated DCB specimens [J]. Composites Science and Technology, 2004, 64(6): 967-981.
  • 10P. Robinson, S. Das. Mode I DCB testing of composite laminates reinforced with z-direction pins: a simple model for the investigation of data reduction strategies [J]. Engineering Fracture Mechanics, 2004, 71(2): 345-364.

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