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Cr3C2/Ni3Al復合材料耐磨性提高的機制分析

傅麗華 韓偉 趙琳 周孟 李長海 田志凌

傅麗華, 韓偉, 趙琳, 周孟, 李長海, 田志凌. Cr3C2/Ni3Al復合材料耐磨性提高的機制分析[J]. 工程科學學報, 2019, 41(1): 117-123. doi: 10.13374/j.issn2095-9389.2019.01.013
引用本文: 傅麗華, 韓偉, 趙琳, 周孟, 李長海, 田志凌. Cr3C2/Ni3Al復合材料耐磨性提高的機制分析[J]. 工程科學學報, 2019, 41(1): 117-123. doi: 10.13374/j.issn2095-9389.2019.01.013
FU Li-hua, HAN Wei, ZHAO Lin, ZHOU Meng, LI Chang-hai, TIAN Zhi-ling. Wear mechanism of Cr3C2/Ni3Al composites showing excellent wear resistance[J]. Chinese Journal of Engineering, 2019, 41(1): 117-123. doi: 10.13374/j.issn2095-9389.2019.01.013
Citation: FU Li-hua, HAN Wei, ZHAO Lin, ZHOU Meng, LI Chang-hai, TIAN Zhi-ling. Wear mechanism of Cr3C2/Ni3Al composites showing excellent wear resistance[J]. Chinese Journal of Engineering, 2019, 41(1): 117-123. doi: 10.13374/j.issn2095-9389.2019.01.013

Cr3C2/Ni3Al復合材料耐磨性提高的機制分析

doi: 10.13374/j.issn2095-9389.2019.01.013
基金項目: 

國家國際科技合作專項資助項目 2015DFA50970

詳細信息
    通訊作者:

    趙琳, E-mail: hhnds@aliyun.com

  • 中圖分類號: TB333

Wear mechanism of Cr3C2/Ni3Al composites showing excellent wear resistance

More Information
  • 摘要: 為了探討Cr3C2強化相提高Cr3C2/Ni3Al復合材料耐磨性的機制, 本文采用熱等靜壓技術制備了Ni3Al合金和Cr3C2/Ni3Al復合材料, 借助納米壓痕儀對Ni3Al合金和Cr3C2/Ni3Al復合材料中各組成相的力學性能進行了表征, 利用銷-盤式摩擦磨損試驗機研究了熱等靜壓Ni3Al合金和Cr3C2/Ni3Al復合材料的耐磨性能, 并結合掃描電子顯微鏡和納米壓痕儀分析了材料磨損表面形貌和磨損次表面層硬度變化.結果表明, Cr3C2的添加提高了復合材料基體的硬度, Cr3C2/Ni3Al復合材料中各組成相的納米硬度和彈性模量由基體相、擴散相到硬芯相是逐漸增大的, 呈現出梯度變化, 有利于提高Cr3C2/Ni3Al復合材料的耐磨性.在本研究實驗條件下, Ni3Al合金和Cr3C2/Ni3Al復合材料表面的磨損形式主要為磨粒磨損, Cr3C2/Ni3Al復合材料表現出更加優異的耐磨性能.Cr3C2/Ni3Al復合材料耐磨性能的提高主要跟碳化物強化相阻斷磨粒切削、減弱摩擦副間相互作用、減小加工硬化層厚度、磨粒尺寸等因素有關.

     

  • 圖  1  粉末材料微觀形貌:(a) Ni3Al合金粉末;(b) Cr3C2顆粒

    Figure  1.  Morphologies of powder materials: (a) Ni3Al-alloy powders; (b) Cr3C2 particles

    圖  2  Ni3Al合金和Cr3C2/Ni3Al復合材料的微觀組織. (a) Ni3Al合金;(b) Cr3C2/Ni3Al復合材料

    Figure  2.  Microstructure of Ni3Al-alloy and Cr3C2/Ni3Al composites: (a) Ni3Al-alloy; (b) Cr3C2/Ni3Al composites

    圖  3  Ni3Al合金和Cr3C2/Ni3Al復合材料中各組成相納米硬度測試的加載卸載曲線

    Figure  3.  Loading and unloading curves of nanoindentation measurement for different constitution phases in the Ni3Al-alloy and Cr3C2/Ni3Al composites

    圖  4  Ni3Al合金和Cr3C2/Ni3Al復合材料的硬度和磨損量結果

    Figure  4.  Hardness and volume loss of the Ni3Al-alloy and Cr3C2/Ni3Al composites

    圖  5  Ni3Al合金和Cr3C2/Ni3Al復合材料磨損表面形貌. (a) Ni3Al合金;(b) Cr3C2/Ni3Al復合材料

    Figure  5.  Morphologies of the worn surface of the Ni3Al-alloy and Cr3C2/Ni3Al composites: (a) Ni3Al-alloy; (b) Cr3C2/Ni3Al composites

    圖  6  磨損次表面層納米壓痕測試路徑. (a) Ni3Al合金;(b) Cr3C2/Ni3Al復合材料

    Figure  6.  Testing path of nano-hardness measurement on the subsurface layer: (a) Ni3Al-alloy; (b) Cr3C2/Ni3Al composites

    圖  7  Ni3Al合金和Cr3C2/Ni3Al復合材料磨損后加工硬化層納米硬度隨距離的變化趨勢圖

    Figure  7.  Nano-hardness versus surface distance in the work-ardened layer of the Ni3Al-alloy and Cr3C2/Ni3Al composites

    圖  8  磨屑的微觀形貌. (a) Ni3Al合金;(b) Cr3C2/Ni3Al復合材料

    Figure  8.  Microstructure morphologies of the wear debris: (a) Ni3Al-alloy; (b) Cr3C2/Ni3Al composites

    圖  9  Ni3Al合金和Cr3C2/Ni3Al復合材料磨粒磨損的示意圖. (a) Ni3Al合金;(b) Cr3C2/Ni3Al復合材料

    Figure  9.  Diagrammatic sketch of the abrasive wear of the Ni3Al-alloy and Cr3C2/Ni3Al composites: (a) Ni3Al-alloy; (b) Cr3C2/Ni3Al composites

    表  1  Ni3Al合金和Cr3C2/Ni3Al復合材料中各組成相的納米壓痕結果

    Table  1.   Nanoindentation measurement results of different constitution phases in the Ni3Al-alloy and Cr3C2/Ni3Al composites

    材料 相組成 最大深度,h/μm 納米硬度,H/GPa 彈性模量,E/GPa
    Ni3Al合金 第二相 0.315 3.14 160.89
    基材相 0.265 5.32 197.58
    Cr3C2/Ni3Al 復合材料 硬芯相 0.149 18.24 352.60
    擴散相 0.158 16.73 291.76
    基材相 0.240 6.34 211.81
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  • 收稿日期:  2017-12-10
  • 刊出日期:  2019-01-01

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