三维针刺C/SiC复合材料与30CrSiMoVA对偶的摩擦磨损性能与机理

刘何意 范尚武 殷小玮 袁琦 张立同 成来飞

刘何意, 范尚武, 殷小玮, 袁琦, 张立同, 成来飞. 三维针刺C/SiC复合材料与30CrSiMoVA对偶的摩擦磨损性能与机理[J]. 航空材料学报, 2011, 31(5): 51-57.
引用本文: 刘何意, 范尚武, 殷小玮, 袁琦, 张立同, 成来飞. 三维针刺C/SiC复合材料与30CrSiMoVA对偶的摩擦磨损性能与机理[J]. 航空材料学报, 2011, 31(5): 51-57.
LIU He-yi, FAN Shang-wu, YIN Xiao-wei, YUAN Qi, ZHANG Li-tong, CHENG Lai-fei. Tribological Properties and Wear Mechanisms of the Couple of 3D Needled C/SiC Composite and 30CrSiMoVA[J]. Journal of Aeronautical Materials, 2011, 31(5): 51-57.
Citation: LIU He-yi, FAN Shang-wu, YIN Xiao-wei, YUAN Qi, ZHANG Li-tong, CHENG Lai-fei. Tribological Properties and Wear Mechanisms of the Couple of 3D Needled C/SiC Composite and 30CrSiMoVA[J]. Journal of Aeronautical Materials, 2011, 31(5): 51-57.

三维针刺C/SiC复合材料与30CrSiMoVA对偶的摩擦磨损性能与机理

基金项目: 

凝固技术国家重点实验室自主研究项目(46-QP-2009)

详细信息
    作者简介:

    刘何意(1986- ),男,硕士研究生,(E-mail)heyi_liu@163.com.

  • 中图分类号: TB333

Tribological Properties and Wear Mechanisms of the Couple of 3D Needled C/SiC Composite and 30CrSiMoVA

  • 摘要: 通过MM-1000Ⅱ摩擦试验机,研究了三维针刺C/SiC复合材料与30CrSiMoVA对偶的摩擦磨损性能,并结合SEM,XRD,EDS、热力学计算以及刹车过程温度场有限元模拟,分析了刹车过程中的摩擦磨损机理和物相转变.结果表明:随着初始刹车速率的增加,三维针刺C/S iC复合材料与30CrS iMoVA对偶刹车的平均摩擦系数减小,摩擦面温度升高,三维针刺C/SiC复合材料与30CrSiMoVA线磨损率呈增大趋势.初始刹车速率大于15m/s刹车时,摩擦面最高温度高于560℃,Fe与SiC,Si以及O2发生反应生成Fe3C,Fe3Si,FeO,γ-Fe2O3和α-Fe2O3,以上反应与磨粒磨损、粘着磨损以及疲劳磨损相互促进,加速了材料的磨损.

     

  • [1] BREUER B,DAUSEND U.Advanced Brake Technology[M].USA:SAE International,2003.37-50.
    [2] KRENKEL W,HEIDENREICH B,RENZ R.C/C-SiC composite for advanced friction systems[J].Adv Eng Mater,2002,4(7):427-436.
    [3] VAIDYARAMAN S,PURDY M,WALKER T,et al,C/SiC material evaluation for aircraft brake applications[C]//KRENKEL W,NASLAIN R,SCHNEIDER H.High Temperature Ceramic Matrix Composites.Weinheim:Federal Republic of Germany,2001.802-808.
    [4] KRENKEL W,HENKE T.Design of high performance CMC brake disk[J].Key Eng Mat,1999,164-165:421-424.
    [5] KRENKEL W.C/C-SiC compositer for hot structures and advanced firction systems[J].Ceram Eng Sci Proc,2003,24(4):583-592.
    [6] PAK Z S.Cf/SiC/C composites for fritional application[C]//KRENKEL W,NASLAIN R,and SCHNEIDER H.High Temperature Ceramic Matrix Composites.Weinheim:Federal Republic of Germany,2001.820-825.
    [7] KRENKEL W,BERNDT F.C/C-SiC composites for space applications and advanced friction systems[J].Mat Sci Eng(A),2005,412:177-181.
    [8] 肖鹏,熊翔,张红波,等.C/C-SiC陶瓷制动材料的研究现状与应用[J] 中国有色金属学报,2005,15(5):668-674.
    [9] FAN S,ZHANG L,XU Y,Microstructure and tribological properties of advanced carbon/silicon carbide aircraft brake materials[J].Compos Sci Technol,2008,68:3002-3009.
    [10] CAI Y,FAN S,LIU H,et al.Microstructures and improved wear resistance of 3D needled C/SiC composites with graphite filler[J].Compos Sci Technol,2009,69:2447-2453.
    [11] FAN S,ZHANG L,CHENG L,et al.Effect of braking pressure and braking speed on the tribological properties of C/SiC aircraft brake materials[J].Compos Sci Technol,2010.70:959-965.
    [12] 徐永东,张立同,成来飞,等.三维针刺碳/碳化硅陶瓷基复合材料及其摩擦磨损性能[J].航空材料学报,2007,27(1):28-32.
    [13] 费多尔钦科NM.现代摩擦材料[M].北京:冶金工业出版社,1983:54-57.
    [14] 范尚武.三维针刺C/SiC飞机刹车材料的结构/性能及其试验验证[D].西安:西北工业大学,2009:71-72.
    [15] 张彬.30CrSiMoVA高强度钢性能的研究[J].太钢科技,1994,2:46-49.
    [16] 范尚武,徐永东,楼建军,等.C/SiC刹车材料的制备及摩擦磨损性能[J].无机材料学报,2006,21(4):927-934.
    [17] JACKSON M R,MEHAN R L,HALL E L.Solid State SiC/Ni Alloy Reaction[J].Metall Trans(A),1983,14:355-364.
    [18] PELLEG J.Reactions in the Matrix and Interface of the Fe-SiC Metal Matrix Composite System[J].Mater Sci Eng(A),1999,269:255-261.
    [19] 全永昕.工程摩擦学[M].杭州:浙江大学出版社,1994:43-45.
    [20] GWIDON W,ANDREW W.Engineering tribology[M].Australia:Butterworth Heinemann,2000:543-544.
  • 加载中
计量
  • 文章访问数:  1338
  • HTML全文浏览量:  28
  • PDF下载量:  212
  • 被引次数: 0
出版历程
  • 刊出日期:  2011-10-01

目录

    /

    返回文章
    返回