期刊文献+

碳布缝合预制体孔隙与热解碳沉积时变相依的多尺度研究 被引量:5

Multi-Scale Relationship of Pores in Carbon Cloth Stitched Preform and Deposition of Pyrocarbon
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摘要 以甲烷为前驱体,碳布缝合织物为预制体,采用等温化学气相渗透(ICVI)工艺,在1 368 K温度和1 s滞留时间下制备了C/C复合材料。采用压汞仪表征不同致密化时间下预制体的孔隙分布,采用偏光显微镜观察热解碳的结构。结果表明:预制体的孔隙分布呈现多峰分布,热解碳的沉积速率与[A/V]值成反比,热解碳的结构与预制体的比表面积相关,沉积初期比表面积较大时,得到的热解碳织构为各相同性和低织构热解碳,随着沉积的进行,比表面积逐渐减小,在纤维束的边沿等部位出现了高织构热解碳。 Isothermal chemical vapor infiltration(ICVI) was used to study carbon cloth stitched preform densifi- cation process,methane was the precursor, at the temperature of 1 368 K and residence time of 1 s. Carbon cloth stitched preform porosity distribution under different time was characterized by mercury porosimetry, and the pyrocar- bon structure was observed by PLM. It is found that the porosity presented multipeek shape, and pyrocarbon deposition rate and [A/V] value showed a inverse correlation throughout the whole study process. The texture of the pyrocarbon had a relationship with the specific surface area. Isotropic and low textured pyrocarbon was first got at the initial of in- filtration, then high textured pyrocarbon was discovered at larger size pores like the edge of the bundle.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2015年第5期36-39,43,共5页 Aerospace Materials & Technology
关键词 碳布缝合预制体 等温化学气相渗透(ICVI) 孔隙变化 [A/V] 热解碳结构 Carbon cloth stitched perform,Chemical vapor infiltration(CVI),Porosity variation, [A/V] ,Pyrocarbon srueture
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参考文献15

  • 1Becker A, HtiTtinger K. Chemistry and kinetics of chemical vapor deposition of pyrocarbon--II pyrocarbon deposition from ethylene, acetylene and 1, 3-butadiene in the low tempera- ture regime[J]. Carbon, 1998, 36(3) : 177-199.
  • 2Becker A, HtlTtinger K. Chemistry and kinetics of chemical vapor deposition of pyrocarbon-V influence of reactor volume/deposition surface area ratio[J]. Carbon, 1998, 36(3) : 225 -232.
  • 3ZHANG W, HtiTtinger K. Densification of a 2D carbon fiber preform by isothermal, isobaric CVI: kinetics and carbon microstrueture[J]. Carbon, 2003, 41 (12) : 2325-2337.
  • 4Guellali m, Oberacker R, HOFFMANN M, et al. Tex- tures of pyrolytic carbon formed in the chemical vapor infiltration of capillm'ies[J]. Carbon,2003,41 ( 1 ) :97-104.
  • 5Beatty, CARLSEN F, COOK J. Pyrolytic-carbon coat- ings on ceramic fuel particles[J]. NUCL APPL, 1965,1 (6) :560 -566.
  • 6SAVAGE G. Carbon-carbon composites [M]. Springer, 1993.
  • 7李新涛,赵高文,许正辉,杨文彬,杨晓光.缝合结构C/C复合材料的制备及组织[J].宇航材料工艺,2011,41(1):58-60. 被引量:2
  • 8白瑞成,李贺军,付业伟,王兰英,卢锦花.预制体孔隙结构对炭/炭复合材料ICVI制备工艺的影响[J].炭素技术,2005,24(3):24-27. 被引量:9
  • 9ANTES J, HU Z, ZHANG W, et al. Chemistry and ki- netics of chemical vapour deposition of pyrocarbon : VII. Confirma- tion of the influence of the substrate surface area/reactor volumeratio[J]. Carbon,1999,37 (12):2031-2039.
  • 10HUZJ, H | FINGER KJ. Mechanisms of carbon deposition--a kinetic approach [J]. Carbon, 2002,40 (4) : 624 - 628.

二级参考文献16

  • 1严柳芳,陈南梁,罗永康.缝合技术在复合材料上的应用及发展[J].产业用纺织品,2007,25(2):1-5. 被引量:18
  • 2Alex V,Patrick T.Advamced structural concept development using stitched composites.NASA,2008-2329.
  • 3Lomov S V,Belov E B,BischoffT,et al.Carbon composites based on muhiaxial multiply stitched preforms[J].Composites:Part A,2002;33,1171-1183.
  • 4Savage G.Carbon/carbon composites[M].Campman &Hall,London,1993:179.
  • 5Fitzer E.The future of carbon-carbon composites[J].Carbon,1987,25(2):163-190.
  • 6THOMAS C R, In:Thomas C R, ed. Essential of carbon-carbon composites [M]. Royal Society of Chemistry Cambridge, 1993.1.
  • 7OBERLIN A. Pyrocarbona[J]. Carbon, 2002, 40:7-24.
  • 8ZHANG W G, HUUTTINGER K J. Chemical vapor deposition of carbon from methane at various pressures, partial pressures and substrate surface/reactor volume ratios[J].Journal of Materials Science, 2001, 36:3503-3510.
  • 9HU Z J, HUTTINGER K J. Influence of pressure, temperature and surface area/volume ratio on the texture of pyrolytlc carbon deposited from methane[J]. Carbon, 2003,41:749-758.
  • 10HU Z J, HUTTINGER K J. Influence of the surface area/volume ratio on the chemistry of carbon deposition frommethane[J]. Carbon,2003, 41:1501-1508.

共引文献9

同被引文献42

  • 1郑茂繁,江豪成,张天平,顾左.离子推进器C/C复合材料栅极研究[J].航天器环境工程,2010,27(6):756-759. 被引量:6
  • 2潘叶金.钼、钨及其合金[J].中国钼业,2001,25(2):44-47. 被引量:13
  • 3李娟,顾佐,江豪成,聂文虎.氙离子火箭发动机补偿栅极设计[J].真空与低温,2005,11(1):29-33. 被引量:6
  • 4李翠云,李辅安.碳/碳复合材料的应用研究进展[J].化工新型材料,2006,34(3):18-20. 被引量:61
  • 5杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:995
  • 6CHOURY J J. Carbon/Carbon Materials for Nozzles of Solid Propellant Rocket Motors[J]. AIAA/SAE 12th Pro- pulsion Conference, 1976: 26--29.
  • 7ZHANG Wei-gang. Chemical Vapor Infiltration: From Hydrocarbon Gas to Solid Carbon[M]. Beijing: Science Press, 2007.
  • 8PIERSON H O, Lieberman M L. The Chemical Vapor Deposition of Carbon on Carbon Fiber[J]. Carbon, 1975, 13(1): 159--166.
  • 9LI Ai-jun, ZHANG Shou-yang, REZNIK Boris, et al. Chemistry and Kinetics of Chemical Vapor Deposition of Pyrolytic Carbon from Ethanol[J]. Proceedings of the Combustion Institute, 2011, 33(2): 1843-1850.
  • 10YANG Min, SUN Jin-liang, REN Mu-su. Nanohardness and Elastic Modulus of Pyrocarbon[J]. Journal of Shang- hai University(Natural Science Edition), 2008, 14(5): 541 -545.

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